List of reports with prices

MISSING IMAGE

Material Information

Title:
List of reports with prices
Physical Description:
v. : ; 19 cm.
Language:
English
Creator:
United States -- National Advisory Committee for Aeronautics
Publisher:
G.P.O.
Place of Publication:
Washington, D.C
Publication Date:
Frequency:
irregular

Subjects

Subjects / Keywords:
Aeronautics -- Bibliography -- Periodicals   ( lcsh )
Government publications -- Bibliography -- Periodicals -- United States   ( lcsh )
Genre:
bibliography   ( marcgt )
federal government publication   ( marcgt )

Notes

Dates or Sequential Designation:
May 1, 1926-
General Note:
Title from cover.
Statement of Responsibility:
National Advisory Committee for Aeronautics.

Record Information

Source Institution:
University of Florida
Rights Management:
All applicable rights reserved by the source institution and holding location.
Resource Identifier:
aleph - 030814821
oclc - 10739617
Classification:
lcc - Z5063 .U64
ddc - 016.62913 U62
System ID:
AA00022345:00005

Table of Contents
    Front Cover
        Front Cover 1
        Front Cover 2
    Title Page
        Page i
        Page ii
    Introduction
        Page iii
        Page iv
    Index
        Page v
        Page vi
    Annual reports and bibliographies
        Page 1
        Page 2
    Technical reports
        Page 3
        Page 4
        Page 5
        Page 6
        Page 7
        Page 8
        Page 9
        Page 10
        Page 11
        Page 12
        Page 13
        Page 14
        Page 15
        Page 16
        Page 17
        Page 18
        Page 19
        Page 20
        Page 21
        Page 22
        Page 23
        Page 24
        Page 25
        Page 26
        Page 27
        Page 28
        Page 29
        Page 30
        Page 31
        Page 32
        Page 33
        Page 34
        Page 35
        Page 36
        Page 37
        Page 38
        Page 39
        Page 40
        Page 41
        Page 42
    Back Cover
        Back Cover 1
        Back Cover 2
Full Text
















:' ~~.. ".:.. .. .::" :.






.. .. .. '. : .
M E 1, ", In














46i.
'J 4 ... ..














Spp
SA I.'... "
I p : ...



. . : "
. .. -o w n .". e ,..: :,,
m m an ." .." ; # L .," ,. .. .., ,. .. .. ./ ." .

't i e -..:4.4 .. . . .: .




















































~0
4' 1
*I ~


S44


( I


a


4. 4,
C.
I.


u ^
nItn


2 ,,~ 44


jt I j i i*i' : ii.


1~~ ~ ~ 4 1.M, %^ .
i ~ ~ ~ ~ ~ i A' ; **. A^'


-A-m
*1* 'Ia.. t> ***










MN A:


I. '0
. " .. ... ...." : . .
,, 1 .. '. .. . . .. : "~.
.... * '< : .: "::'. ::; :: h t '8 ': ":i,








.. 4.. . . . N . ..
.. '. a .. , *. : .... *..
. 1 *. :. : ' -' ,.
i i' i,** $l i* ,,i .... ,i ii^







4. .'4 *'* I j'- : ^^^^^ ^
/.'.. . ... >,.

; .. '' .' :" :' p';, ..: ,
. j..
::" ,.. i : ? 2." : -,. \ ..: [ t d



{ i.: i,. i:, i i IL
aP : I I "
.. .1 ' .. ,:i "


*1. I
V
.4 4

/~ Ir~ *,


iN4..


'.








NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS





LIST OF REPORTS
WITH PRICES



EDITION JUNE, 1932


UNITED STATES
GOVERNMENT PRINTING .OFFICE
WASHINGTON : 1932



















Digitized by the Internet Archive
in 2013













http://archive.org/detail Is/listofrepo1932unit















NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


NOTE


This is a list of the Reports of the National Advisory Com-
mittee for Aeronautics prepared as of June, 1932, arranged
by subjects.
Unless otherwise indicated, all reports may be obtained at
the prices stated from the Superintendent of Documents, Gov-
ernment Printing Office, Washington, D. C. (See "Instruc-
tions for the Purchase of Government Publications" below.)

INSTRUCTIONS FOR THE PURCHASE OF GOVERNMENT
PUBLICATIONS
Reports may be purchased on application to the Superin-
tendent of Documents, Government Printing Office, Washington,
D. C., which should be accompanied by remittance in the form
of coupons, postal money order, express order, or certified
check. If currency is sent, it will be at sender's risk. Foreign
orders should be accompanied by international money order
or draft on an American bank. Postage stamps, foreign money,
defaced or smooth coins, will not be accepted.
All reports marked as out of print are available for reference
or loan upon application to the Office of Aeronautical
Intelligence, National Advisory Committee for Aeronautics,
Washington, D. C.
(lit




















INDEX
Page
Annual reports ------------------------------------ 1
Bibliographies ------------------------------------ 1
Technical reports ---------------------------------- 3
Aerodynamics --------------------------------- 3
Airfoils and wing sections----------------------- 5
Airplanes-Full-scale experiments---------------- 9
Airplanes-Model experiments ------------------ 12
Airships----------- -------------------------- 14
Engines and accessories----------------------- 16
Fuels -------------------------------------- 25
Gases--------------------------------------- 26
Helicopters ----------------------------------- 26
Hydrodynamics-------------------------------- 26
Instruments ---------------------------------- 27
Materials------------------------------------- 30
Meteorology---------------------------------- 32
Miscellaneous ---------------------------------33
Nomenclature--------------------------------- 33
Parachutes -----------------------------------34
Propellers------------------------------------- 34
Seaplanes----_------------------------------ 37
Stability and control --------------------------- 38
Strength of construction ------------------------ 39
Wind tunnels and laboratories------------------- 41
(v)












NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


ANNUAL REPORTS


First 1-------
Second- ----
Third-------
Fourth 1 ----
Fifth -------
Sixth1
Seventh. .
Eighth I-
Ninth I------
Tenth1------
Eleventh-.
Twelfth 'I.
Thirteenth '_
Fourteenth_---
Fifteenth- -.
Sixteenth -
Seventeenth -


Year

1915
1916
1917
1918
1919
1920
1921
1922
1923
1924
1925
1926
1927
1928
1929
1930
1931


With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With
With


Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports
Reports


Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.


1-7------
8-12.--..--
13-23-----
24-50-----
51-82-----
83-110----
111-132..-
133-158 ---
159-185---
18f%-209---
210-232---
233-256---
257-282..-
283-308---
309-336---
337-364___
365-400--


Price


$Si. 25
1.50


2. 25





1. 25
2. 35
3. 00
3. 00


SOut of print. Available for reference or loan in the Office of Aeronautical Intel.
ligence, National Advisory Committee for Aeronautics, and in the libraries of large
cities.
NoTE.-Beginning with the sixteenth, the annual reports are to be bound in buck-
ram only.
BIBLIOGRAPHIES


Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography


Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics


(1909-1916)--------------
(1917-1919)
(1920-1921)-------------
(1922)----------------
(1923)-------------------
(1924)-- -----------
(1925)-------------------
(1926)-------------------
(1927)-------------------
(1928)-------------------
(1929) ..-----------------. i
(1930) .------..----. -
(1)


$2.




*












TECHNICAL REPORTS


AERODYNAMICS


No.

1 12

20


3 78

3 79

3 83


97

114

116

139

144

3151

185

3197


Price


$0.05


Title

Experimental Researches on the Resistance of
Air. By L. Marchis. (Second Annual, 1916).
Aerodynamic Coefficients and Transformation
Tables. By Joseph S. Ames. (Third Annual,
1917)------------------------------------
The Limiting Velocity in Falling from a Great
Height. By Edwin Bidwell Wilson. (Fifth
Annual, 1919)---------------------------
Bomb Trajectories. By Edwin Bidwell Wilson.
(Fifth Annual, 1919)----------------------
Wind Tunnel Studies in Aerodynamic Phe-
nomena at High Speed. By F. W. Caldwell
and E. N. Fales. (Sixth Annual, 1920)-----
General Theory of the Steady Motion of an
Airplane. By George de Bothezat. (Sixth
Annual, 1920)----------------------------
Some New Aerodynamical Relations. By Max
M. Munk. (Seventh Annual, 1921) --------
Applications of Modern Hydrodynamics to
Aeronautics. By L. Prandtl. (Seventh An-
nual, 1921) -------- -- -----
Influence of Model Surface and Air Flow Tex-
ture on Resistance of Aerodynamic Bodies.
By A. F. Zahm. (Eighth Annual, 1922)----....-
The Decay of a Simple Eddy. By H. Bateman.
(Eighth Annual, 1922)---------------------
General Biplane Theory. By Max M. Munk.
(Eighth Annual, 1922)---------_-- .- _---- -
The Resistance of Spheres in Wind Tunnels
and in Air. By David L. Bacon and Elliott
G. Reid. (Ninth Annual, 1923) ------------
A New Relation Between the Induced Yawing
Moments and the Rolling Moments of an
Airfoil in Straight Motion. By Max M.
Munk. (Tenth Annual. 1924)--------------


.10

.05

.05


. 10


I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.
(3)


.15









AERODYNAMICS-Continued

No. Title Price

213 A R6sume ot the Advances in Theoretical
Aeronautics Made by Max M. Munk. By
Joseph S. Ames. (Eleventh Annual, 1925)--....-- $0. 15
S247 Pressure of Air on Coming to Rest from Various
Speeds. ByA.F.Zahm. (Twelfth Annual, 1926)------
"253 Flow and Drag Formulas for Simple Quadrics.
By A. F. Zahm. (Twelfth Annual, 1926)----------
287 Theories of Flow Similitude. By A. F. Zahm.
(Thirteenth Annual, 1927)----------------- .05
289 Forces on Elliptic Cylinders in Uniform Air
Stream. By A. F. Zahm, R. H. Smith, and
F. A. Louden. (Fourteenth Annual, 1928)-- .05
311 Aerodynamic Theory and Test of Strut
Forms-1I. By R. H. Smith. (Fifteenth
Annual, 1929)--------------------------- 10
316 Tables for Pressure of Air on Coming to Rest
from Various Speeds. By A. F. Zahm and
F. A. Louden. (Fifteenth Annual, 1929)____ .05
323 Flow and Force Equations for a Body Revolv-
ing in a Fluid. By A. F. Zahm. (Fifteenth
Annual, 1929)----------------------------- .20
335 Aerodynamic Theory and Test of Strut Forms.
Part II. By R. H. Smith. (Fifteenth Annual,
1929)------------------------------ .20
349 A Proof of the Theoreim Regarding the Distribu-
tion of Lift over the Span for Minimumn In-
duced Drag. By W. F. Durand. (Sixteenth
Annual, 1930)---------------------------- 10
361 Experimental Determination of Jet Boundary
Corrections for Airfoil Tests in Four Open
Wind Tunnel Jets of Different Shapes. By
Montgomery Knight and Thomas A. Harris.
(Sixteenth Annual, 1930)------------------ .20
362 An Extended Theory of Thin Airfoils and Its I
Application to the Biplane Problem. Bv y
Clark B. Millikan. (Sixteenth Annual, 1930)_ 20
395 A New Principle of Sound Frequency Analysis.
By Theodore Theodorsen. (Seventeenth An-
nual, 1931) --..---------------------------- 15
I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.







AERODYNAMNI ICS-Continued


No. Title Price

411 Theory of Wing Sections of Arbitrary Shape.
By Theodore Theodorsen. (Eighteenth An-
nual, 1932)------------------------------- $0. 10
Relation Between Aeronautic Research and Air-
craft Design. By Joseph S. Ames. (Appen-
dix to Administrative Report, 1923)--------- 15

AIRFOILS AND WING SECTIONS

4 18 Aerofoils and Aerofoil Structural Combinations.
By Edgar S. Gorrell and H. S. Martin.
(Third Annual, 1917)--------------------------
3 28 An Introduction to the Study of the Laws of Air
Resistance of Aerofoils. By George de
Bothezat. (Fourth Annual, 19S18)
3 75 The Aerodynamic Properties of Thick Aerofoils
SSuitable for Internal Bracing. By F. H.
Norton. (Fifth Annual, 1919) ---- ---- ------
S77 Thle Parker Variable Camber Wing. By H. F.
SParker. (Fifth Annual, 1919)---..-------------- --
1 93 Aerodynamic Characteristics of Airfoils. By
SNational Advisory Committee for Aero-
nautics. (Sixth Annual, 1920)-----------------
3 111 The Variation of Airfoil Lift and Drag Coeffi-
cients with Changes in Size and Speed. By
W. S. Diehl. (Seventh Annual, 1921)-----------
3 121 The Minimum Induced Drag of Airfoils. By
Max M. Munk. (Seventh Annual, 1921)-------
124 Aerodynamic Characteristics of Airfoils-II.
By the National Advisory Committee for
S Aeronautics. (Seventh Annual, 1921) ------ $0.30
3 142 General Theory of Thin Wing Sections. By
Max M. Munk. (Eighth Annual, 1922) --------
S150 Pressure Distribution over Thick Aerofoils-
Model Tests. By F. H. Norton and D. L.
Bacon. (Eighth Annual. 1922)-----------------
1 Out of print. Annual volume available for reference or loan in the office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and
in the libraries of large cities.
3 Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.
4 Not issued as a separate report. The annual volume containing this report is
still available.







6

AIRFOILS AND WING SECTIONS-Continued

No. Title Price

3152 The Aerodynamic Properties of Thick Aero-
foils-II. Bv F. H. Norton and D. L.
Bacon. (Eighth Annual, 1922)----------------
s 169 The Effect of Airfoil Thickness and Plan Form
on Lateral Control. By H. I. Hoot. (Ninth
Annual, 1923)
'182 Aerodynamic Charactersitics of Airfoils-III.
By National Advisory Committee for Aero-
nautics. (Ninth Annual, 1923).....
3 191 Elements of the Wing Section Theory and of the
Wing Theory. By Max M. Munk. (Tenth
Annual, 1924)-----------------------------
200 Some Problems on the Lift and Rolling Mo-
ments of Airplane Wings. By Jas. B. Scar-
borough. (Tenth Annual, 1924) ------------ $0.10
3201 The Effects of Shielding the Tips of Airfoils.
By Elliott G. Reid. (Tenth Annual, 1924)-----
207 Aerodynamic Characteristics of Airfoils at High
Speeds. By L. J. Briggs, G. F. Hull, and
H. L. Dryden. (Tenth Annual, 1924)----.- 10
217 Preliminary Wing Model Tests in the Variable
Density Wind Tunnel of the National Advi-
sory Committee for Aeronautics. By Max M.
Munk. (Eleventh Annual, 1925)----------- .10
s221 Model Tests with a Systematic Series of 27
Wing Sections at Full Reynolds Number.
By Max M. Munk and Elton W. Miller.
(Eleventh Annual, 1925)---- -------------
229 Pressure Distribution over Thick, Tapered Air-
foils, N. A. C. A. 81, U. S. A. 27 C Modified
and U. S. A. 35. By Elliott G. Reid.
(Eleventh Annual, 1925)------------------- .10
'233 The Aerodynamic Characteristics of Seven Fre-
quently Used Wing Sections at Full Reynolds
Number. Bv Max M. Munk and Elton W.
Miller. (Twelfth Annual, 1926)------------
'244 Aerodynamic Characteristics of Airfoils-IV.
By National Advisory Committee for Aero-
nautics (Twelfth Annual. 1926)-------,
2 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.









AIRFOILS AND WING SECTIONS-Continued

No. Title Price

255 Pressure Distribution over Airfoils at High
Speeds. By L. J. Briggs and H. L. Dryden.
(Twelfth Annual, 1927)-------------------- $0. 15
267 Drag of Wings with End Plates. By Paul E.
Hemke. (Thirteenth Annual, 1927)--------- .10
271 Pressure Distribution Tests on PW-9 Wing
Models Showing Effects of Biplane Interfer-
ence. By A. J. Fairbanks. (Thirteenth
Annual, 1927)---------------------------- 10
278 Lift, Drag, and Elevator Hinge Moments of
Handley-Page Control Surfaces. By R. H.
SSmith. (Thirteenth Annual, 1927)---------- 10
285 A Study of Wing Flutter. By A. F. Zahm and
R. M. Bear. (Fourteenth Annual, 1928)---- .15
286 Aerodynamic Characteristics of Airfoils-V.
By National Advisory Committee for Aero-
nautics. (Fourteenth Annual, 1928)-------- .25
288 Pressure Distribution over a Rectangular Mono-
plane Wing Model up to 90 Angle of Attack.
By Montgomery Knight and Oscar Loeser, jr.
(Fourteenth Annual, 1928) ----------------- 10
309 Joint Report on Standardization Tests on
N. P. L. R. A. F. 15 Airfoil Model. By
Walter S. Diehl. (Fifteenth Annual, 1929)-- 10
312 The Prediction of Airfoil Characteristics. Bv
George J. Higgins. (Fifteenth Annual, 1929)_ 10
315 Aerodynamic Characteristics of Airfoils-VI.
By National Advisory Committee for Aero-
nautics. (Fifteenth Annual, 1929)---------- .20
317 Wing Tunnel Tests on a Series of Wing Models
Through a Large Angle of Attack Range. Part
I, Force Tests. By Montgomery Knight and
Carl J. Wenzinger. (Fifteenth Annual, 1929)_ .25
319 Aerodynamic Characteristics of Twenty-four
Airfoils at High Speeds. By L. J. Briggs
and H. L. Dryden. (Fifteenth Annual, 1929)_ 15
331 Collection of Wind Tunnel Data on Commonly
Used Wing Sections. By F. A. Louden. (Fif-
teenth Annual, 1929)---------------------- .20
336 Tests of Large Airfoils in the Propeller Research
Tunnel, including Two with Corrugated Sur-
faces. By Donald H. Wood. (Fifteenth An-
nual, 1929)------------------------------ .10









AIRFOILS AND WING SEcriONs-Continued

No. Title Price

352 Large-Scale Aerodynamic Characteristics of Air-
foils as Tested in the Variable-Density Wind
Tunnel. By Eastman N. Jacobs and Ray-
mond F. Anderson. (Sixteenth Annual, 1930) $0. 20
353 Airfoil Pressure Distribution Investigation in the
Variable-Densitv Wind Tunnel. By Eastman
N. Jacobs, John Stack, and Robert M. Pinker-
ton. (Sixteenth Annual, 1930) --.-------- .15
360 Pressure Distribution over a Symmetrical Airfoil
Section with Trailing Edge Flap. By East-
man N. Jacobs and Robert M. Pinkerton.
(Sixteenth Annual, 1930)------------ 15
365 Aerodynamic Characteristics of Circular-Arc
Airfoils at High Speeds. By L. J. Briggs and
H. L. Dryden. (Seventeenth Annual, 1931)J .10
367 Pressure Distribution over a Thick, Tapered, and
Twisted Monoplane Wing Model. N. A. C. A.
81-J. By Carl J. Wenzinger. (Seventeenth
Annual, 1931)------------------------- 10
370 Effect of Variation of Chord and Span of Ailerons
on Hinge Moments at Several Angles of Pitch.
By H. B. Monish. (Seventeenth Annual,
1931)--------------------------------- 10
383 On the Theory of Wing Sections with Particular
Reference to the Pressure Distribution. By
Theodore Theodorsen. (Seventeenth Annual,
1931)------------------------------------ .10
385 WinNd Tunnel Tests on Airfoil Boundary Layer
Control Using a Backward-Opening Slot. By
Millard J. Bamber. (Seventeenth Annual,
1931)--------------------------------- .20
386 Maneuverability Investigation of an F6C-4
Fighter Airplane. By C. Hf. Dearborn and H.
W. Kirschbaumni. (Seventeenth Annual, 1931). .20
391 ThIe Aerodynamic Characteristics of Eight Very
Thick Airfoils from Tests in the Variable Den-
sity WVind Tunnel. By Eastman N. Jacobs.
(Seventeenth Annual, 1931)------ ---- 10
400 The Aerodynamic Characteristics of a Slotted
Clark Y Wing as Affected by the Auxiliary
Airfoil Position. By Carl J.1. Wenzinger and
Joseph A. Shortal. (Seventeenth Annual,
1931) ------------------------------------.I







AIRFOILS AND WING SECTIONS-Continued


No. Title Price

407 The Characteristics of a Clark Y Wing Model
Equipped with Several Forms of Low-Drag
Fixed Slots. By Fred E. Weick and Carl J.
Wenzinger. (Eighteenth Annual, 1932).___ $0. 10

AIRPLANES-FULL-SCALE EXPERIMENTS

3 69 A Study of Airplane Ranges and Useful Loads.
By J. C. Coffin. (Fifth Annual, 1919)-------------
3 70 Preliminary Report on Free Flight Tests. By
Edward P. Warner and F. H. Norton. (Fifth
Annual, 1919)---------------------------------
3 105 Angles of Attack and Air Speeds during Maneu-
vers. By Edward P. Warner and F. H.
Norton. (Sixth Annual, 1920)--------- ----
3118 The Pressure Distribution over the Horizontal
Tail Surfaces of an Airplane. By F. H. Nor-
ton. (Seventh Annual, 1921) -------------- ------
3 148 The Pressure Distribution over the Horizontal
Tail Surfaces of an Airplane-III. By F. H.
Norton and W. G. Brown. (Eighth Annual,
1922)---------------------------------------
3 149 Pressure Distribution over the Rudder and Fin
of an Airplane in Flight. By F. H. Norton I
and W. G. Brown. (Eighth Annual, 1922)------
3154 A Study of Taking Off and Landing an Airplane.
By. T. Carroll. (Eighth Annual, 1922) ----
3155 A Study of Airplane Maneuvers with Special
Reference to Angular Velocities. By H. J.
E. Reid. (Eighth Annual, 1922)------------ -----
162 Complete Study of the Longitudinal Oscillation
of a VE-7 Airplane. By F. H. Norton and
W. G. Brown. (Ninth Annual, 1923)------- $0.05
163 i The Vertical, Longitudinal, and Lateral Accelera-
Stions Experienced by an S-5A Airplane while
I Maneuvering. By F. H. Norton and T.
SCarroll. (Ninth Annual, 1923)------------ .05
167 The Measurement of the Damping in Roll on a
JN4H in Flight. By F. H. Norton. (Ninth
Annual, 1923)----------------------------- .05
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.









AIRPLANES-FULL-SCALE EXPERIMENTS-Continued
No. Title Price

3 170 A Study of Longitudinal Dynamic Stability in
Flight. By F. H. Norton. (Ninth Annual,
1923)------------------------------------------
173 Reliable Formulhe for Estimating Airplane
Performance and the Effects of the Changes in
WVeight, WVing Area, or Power. By Walter
S. Diehl. (Ninth Annual, 1923)------------ $0.05
174 The Small Angular Oscillations of Airplanes in
Steady Flight. By F. H. Norton. (Ninth
Annual, 1923) --------------------------- .05
3192 Charts for Graphical Estimation of Airplane
Performance. By Walter S. Diehl. (Tenth
Annual, 1924)--------- ----------------
3 193 Pressure Distribution Over the Wings of an
MB-3 Airplane in Flight. By F. H. Norton.
(Tenth Annual, 1924)__
- 194 Investigation of Slip Stream Velocity. By J. W. I
Crowley, jr. (Tenth Annual, 1924)-------------
203 Accelerations in Flight. By J. H. Doolittle.
(Tenth Annual, 1924)-- -------- 10
219 Some Aspects of the Comparison of Model and
Full-Scale Tests. By D. W. Taylor. (Elev-
enth Annial, 1925)---------------------- 10
228 A Study of the Effect of a Diving Start, on Air-
plane Speed. By Walter S. Diehl. (Eleventh
Ani ial, 1925) ----------------- ----------- .05
234 Three Methods of Calculating Range and En-
1draiKice of Airplanes. By Walter S. Diehl.
(Twelfth Annual, 19)26) -------------------- 10
238 The Effect of Flight Path Inclination on Airplane
Veloc(ity. Bv Walter S. Diehl. (Twelfth
A al, 1926)------------------------- .05
2-19 A Cnomparison of the Take-off and Landing
ICharacteristics of a Numnber of Service Air-
1plalnes. By Thomlas Carroll. (Twelfth An-
iiiial, 1921)- ------------------------------
257 Pressutre D)istribution over a Wing and Tail
Rib of a VE--7 and of a TS Airplane in Flight.
Bv J. W. (Crowlk'y, jr. (Thirteenth Annual,
1927)------ .------------------------------. 15
265 A Fiull-Scale Investigation of Groutnd Effect.
Bv% Elliott G. Reid. (Th irteenth Annual,
1'27) ---------------..-----------------: 05
S(Jutof ( if int .."vilahle as a separate report for reference or loan in tile Office
of Aeroniauial Intlelligence, National Advisory Committee for Aeronautics.









AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

No. Title Price

297 The Reduction of Observed Airplane Perform-
ance to Standard Conditions. By Walter S.
Diehl. (Fourteenth Annual, 1928)--------- $0. 15
304 An Investigation of the Aerodynamic Charac-
teristics of an Airplane Equipped with Several
Different Sets of Wings. By J. W. Crowley,
jr., and M. W. Green. (Fourteenth Annual,
1928)----------------------------------- .10
307 The Pressure Distribution over the Horizontal
and Vertical Tail Surfaces of the F6C-4 Pur-
suit Airplane in Violent Maneuvers. By R.
V. Rhode. (Fourteenth Annual, 1928)------ 10
364 Pressure Distribution over the Wings and Tail
Surfaces of a PW-9 Pursuit Airplane in Flight.
By Richard V. Rhode. (Sixteenth Annual,
1930) ----------------------------------- .60
366 Dynamic and Flight Tests on Rubber-Cord and
Oleo-Rubber-Disk Landing Gears for an
F6C4 Airplane. By Wm. C. Peck. (Seven-
teenth Annual, 1931)---------------------- 10
368 A New Chart for Estimating the Absolute Ceil-
ing of an Airplane. By Walter S. Diehl.
(Seventeenth Annual, 1931)---------------- 10
369 Maneuverability Investigation of the F6C3
Airplane with Special Flight Instruments.
By C. H. Dearborn and H. W. Kirchbaum.
(Seventeenth Annual, 1931)---------------- 15
377 A Method of Flight Measurement of Spins. By
Hartley A. Soule and Nathan F. Scudder.
(Seventeenth Annual, 1931)---------------- .10
380 Pressure Distribution over the Fuselage of a I
PW-9 Airplane in Flight. By R. V. Rhode
and E. E. Lundquist. (Seventeenth Annual,
1931)----------------------------------- .20
381 Static, Drop and Flight Tests on Musselman
Type Airwheels. By Wm. C. Peck and
Albert P. Beard. (Seventeenth Annual,
1931)----------------------------------- .15
403 Ice Prevention on Aircraft by Means of Engine
Exhaust Heat and a Technical Study of Heat
Transmission from a Clark Y Airfoil. By
Theodore Theodorsen and William C. Clay.
Eighteenth Annual, 1932)------------------- .20
112472-32-2









AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

No. Title Price

406 Drop and Flight Tests on NY-2 Landing Gears,
Including Measurements of Vertical Velocities
at Landing. By W. C. Peck and A. P. Beard.
(Eighteenth Annual, 1932)----------------- $0. 15
408 General Formulas and Charts for the Calcula-
tion of Airplane Performance. By W. Bailey
Oswald. (Eighteenth Annual, 1932)-------- .25
413 A Method for Computing Leading Edge Loads.
Bv Richard V. Rhode and Henry A. Pearson.
(Eighteenth Annual, 1932)----------------- 10
414 The Effect on Airplane Performance of Several
Types of Low-Drag Cowling for Radial Air-
Cooled Engines. Bv Wm. H. McAvoy, Oscar
W. Schey, and Alfred W. Young. (Eigh-
teenth Annual, 1932)---------------------- .20
415 Tests of Nacelle-Propeller Combinations in Va-
rious Positions with Reference to Wings.
Part I. Thick Wming-N. A. C. A. Cowled
Nacelle-Tractor Propeller. By Donald H.
Wood. (Eighteenth Annual 1932)---------- 10
418 Preliminary Investigation of Modifications to
Conventional Airplanes to give Nonstalling
and Short-Landing Characteristics. By Fred
E. Weick. (Eighteenth Annual, 1932)------- .05

AIRPLANES-MODEL EXPERIMENTS

3 74 Construction of Models for Tests in Wind Tun-
nels. By F.H. Norton. (Fifth Annual, 1919) ----
119 The Pressure Distribution over the Horizontal I
Tail Surfaces of an Airplane-II. By F. H.
Norton and D. L. Bacon. (Seventh Annual,
1921) ---------------------------------' $0. 10
122 Preliminary Experiments to Determine Scale
and Slip Stream Effects on a 1/24 Size Model
of a JN4H Biplane. By D. L. Bacon. (Sev-
enth Annual, 1921) ------------------------ 05
'133 The Tail Plane. By Max M. Munk. (Eighth
Annual, 1922)-----......--------------- ------
s Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.









AIRPLANES-MODEL EXPERIMENTS-Continued

No. Title Price

136 Damping Coefficients due to Tail Surfaces in Air-
craft. ByLynnChu. (Eighth Annual, 1922) $0.05
137 Point Drag and Total Drag of Navy Struts No.
1 Modified. By A. F. Zahm, R. H. Smith,
and G. C. Hill. (Eighth Annual, 1922)------ .05
S140 Lift 3nd Drag Effects on Wing Tip-Rake. By
SA. F. Zahm, R. M. Bear, and G. C. Hill.
(Eighth Annual, 1922)---------------------------
219 Some Aspects of the Comparison of Model and i
Full-Scale Tests. By D. W. Taylor. (Elev-
enth Annual, 1925)------------------------ 10
3225 The Air Forces on a Model of the Sperry Mes-
senger Airplane Without Propeller. By Max
M. Munk and Walter S. Diehl. (Eleventh
SAnnual, 1925)---------------------------------
236 Tests on Airplane Fus( lages, Floats, and Hulls.
By Walter S. Diehl. (Twelfth Annual, 1926)_ 15
254 Distribution of Pressure over Model of the
Upper Wing and Aileron of a Fokker D-VII
Airplane. By A. J. Fairbanks. (Twelfth
Annual, 1926)---------------------------- 10
256 I The Air Forces on a Systematic Series of Biplane
and Triplane Cellule Models. By Max M.
Munk. (Twelfth Annual, 1926)----------- 15
260 The Effect of a Flap and Ailerons on the N. A.
C. A.-M6 Airfoil Section. By George J. Hig-
Sgins and Eastman N. Jacobs. (Thirteenth
Annual, 1927)---------------------------- 10
266 Air Force and Moment of N-20 Wing with Cer-
tain Cut-Outs. Bv R. H. Smith. (Thir-
teenth Annual, 1927) ---------------------- .05
'269 Air Force Tests of Sperry Messenger Model
with Six Sets of Wings. By James M. Shoe- I
maker. (Thirteenth Annual, 1927)----------
273 Wind Tunnel Tests on Autoiotation and the
"Flat Spin." By Montgomery Knight.
(Thirteenth Annual, 1927)----------------- 10
279 Tests on Models of Three British Airplanes in
the Variable Density Wind Tunnel. By
George J. Higgins, W. S. Diehl, and George
L. DeFoe. (Thirteenth Annual. 1927)------- 15
Out or print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.









AIRPLANES-MODEL EXPERIMENTS-Continued

No. Title Price

296 Pressure Distribution Tests on PW-9 Wing
Models from -18 through 90 Angle of At-
tack. By Oscar E. Loeser, jr. (Fourteenth
Annual, 1928)-------------------------- $0. 15
417 Pressure Distribution Tests on a Series of Clark
Y Biplane Cellules with Special Reference to
Safety. By Richard W. Noyes. (Eighteenth
Annual, 1932) --- -------- 10
419 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. I-Ordinary Ailerons on Reciangu-
lar Wings. By Fred E. Weick and Carl J.
Wenzinger. (Eighteenth Annual, 1932)------ .10
422 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. II-Slotted Ailerons and Frise Ail-
erons. By Fred E. Weick and Richard 'W.
Noyes. (Eighteenth Annual, 1932) -------
423 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. Ill-Ordinary Ailerons Rigged up
10 When Neutral. By Fred E. Weick and
Carl J. Wenzinger. (Eighteenth Annual,
1932) -------------------------
424 Wind-Tunnel Research Comparing Lateral Con-
trol Devices, Particularly at High Angles of
Attack. IV-Floating-Tip Ailerons on Rec-
tangular Wings. By Fred E. Weick and
Thomas A. Harris. (Eighteenth Annual,
1932)-----------------------

AIRSHIPS

'115 Bending Moments, Envelope and Cable Stresses
in Nonrigid Airships. By C. P. Burgess.
(Seventh Annual, 1921)---- -----------
117 The Drag of Zeppelin Airships. By Max M.
Munk. (Seventh Annual, 1921)------------ $0.05
S(hiut of print. Available as a separate report for reference or loan in the office
of A croniim ical Intelligence, National Advisory Committee for Aeronautics.









AIRSHIPS-Continued


Title


Price


138


164

* 184

204

208


210

211

212

215


223

291

318

324

325


3 Out of print. Available as a separate report for reference or loan in thi
of Aeronautical Intelligence, National Advisory Committee for Aeronautic!


The Drag of "C" Class Airship Hull with Vary-
ing Lengths of Cylindric Midships. By A. F.
Zahm, R. H. Smith, and G. C. Hill. (Eighth
Annual, 1922)---------------------------
The Inertia Coefficients of an Airship in a Fric-
tionless Fluid. By H. Bateman. (Ninth
Annual, 1923)---------------------------
The Aerodynamic Forces on Airship Hulls. By
Max M. Munk. (Ninth Annual, 1923)------
Forces on Airships in Gusts. By C. P. Burgess.
(Tenth Annual, 1924)----- -----_
Determination of the Turning Characteristics of
an Airship by Means of a Camera Obscura.
By J. W. Crowley, jr., and R. G. Freeman.
(Tenth Annual, 1924)-- ____---_
Inertia Factors of Ellipsoids for Use in Airship
Design. By L. B. Tuckerman. (Eleventh
Annual, 1925)----------------------------
Water Model Tests for Semirigid Airships. By
L. B. Tuckerman. (Eleventh Annual, 1925) -
Stability Equations for Airship Hulls. By A. F.
Zahm. (Eleventh Annual, 1925)_
Air Forces, Moments, and Damping on Model
of Fleet Airship Shenandoah. By A. F.
Zahm, R. H. Smith, and F. A. Louden.
(Eleventh Annual, 1925)-------------------
Pressure Distribution on the C-7 Airship. By
J. W. Crowley, jr., and S. J. DeFrance.
(Eleventh Annual, 1925)-------------------
Drag of C-Class Airship Hulls of Various Fine-
ness Ratios. By A. F. Zahm, R. H. Smith,
and F. A. Louden. (Fourteenth Annual, 1928) -
Speed and Deceleration Trials of U. S. S. Los
Angeles, September, 1927. By S. J. DeFrance
and C. P. Burgess. (Fifteenth Annual, 1929)-
Flight Tests on U. S. S. Los Angeles. Part I.
Full-Scale Pressure Distribution Investigation.
By S. J. DeFrance. (Fifteenth Annual, 1929).
Flight Tests on U. S. S. Los Angeles. Part II.
Stress and Strength Determination. By C.
P. Burgess. (Fifteenth Annual, 1929)-------


No.


$0.05

.05


.05


10

.05

05

05


15

15

S10

S10

15

S15
e Office
I.







16


Al RSHIPS-Continued

No. Title Price

333 Full-Scale Turning Characteristics of the U. S. S.
Los Angeles. ByF.L. Thompson. (Fifteenth
Annual, 1929)---------------------------- $0. 10
394 Airship Model Tests in the Variable Density
Wind Tunnel. By Ira H. Abbott. (Seven-
teenth Annual, 1931)---------------------- .20
397 The Drag Characteristics of Several Airships
Determined by Deceleration Tests. By F. L.
Thompson and H. W. Kirschbaumn. (Seven-
teenth Annual, 1931)---------------------- 10
405 Application of Practical Hydrodynamincs to Air-
ship Design. By R. H. Upson and W. A.
Klikoff. (Eighteenth Annual, 1932)--------- 15


ENGINES AND ACCESSORIES

1 7 Thermnodynamic Efficiency of Present Types of
Internal Combustion Engines for Aircraft.
By Columbia University. (First Annual, 1915) ------
Part 1. Review of the Development of
Engines Suitable for Aeronautic Service.
Part 2. Aero Engines Analyzed with Refer-
ence to Elements of Process or Function.
S10 Mufflers for Aeronautic Engine. By H. Die-
derichs and G. B. Upton. (Second Annual,
1916)------------------------------------
'11 Carburetor Design-A Preliminary Study of the
State of the Art. By Charles Edward Lucke,
assisted by Friedrich Otto Willhofft. (Sec-
ond Annual, 1916)-------------------------------
4 23 Aeronautic Power-Plant Investigations. By the
Subcommittee on Power Plants. (Third
Annual, 1917)------------------------------
Part 1. Performance of Aeronautic Engines
at High Altitudes.
Part 2. Radiator Design.
Part 3. Spark Plugs. i
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
4 Not issued as a sej)raie report. rrThe annual volume containing this report ia
still a1 ailhble.









ENGINES AND ACCESSORIES-Continued

No. Title Price

3 24 Air Flow through Poppet Valves. By G. W.
Lewis and E. M. Nutting. (Fourth Annual,
1918)-----------------------------------------
3 43 Synopsis of Aeronautic Radiator Investigations
for the years 1917 and 1918. By R. V. Klein-
schmidt. (Fourth Annual, 1918)-----------------
3 45 Effect of Compression Ratio, Pressure, Tem-
perature, and Humidity on Power. (Fourth
Annual, 1918)----------------------------------
Part 1. Variation of Horsepower with Al-
titude and Compression Ratio. By
H. C. Dickinson, W. S. James, and G. V.
Anderson.
Part 2. Value of Supercharging. By H. C.
Dickinson and G. V. Anderson.
Part 3. Variation of Horsepower with
Temperature. By H. C. Dickinson,
W. S. James, and G. V. Anderson.
Part 4. Influence of Water Injection on En-
gine Performance. By V. W. Brinkerhoff.
1 46 A Study of Airplane Engine Tests. By V. R.
Gage. (Fourth Annual 1918)-------------------
3 48 Carbureting Conditions Characteristic of Air-
craft Engines. By P. S. Tice. (Fourth
Annual, 1918)----------------------------------
3 49 Metering Characteristics of Carburetors. By
P. S. Tice. (Fourth Annual, 1918) ---------------
3 51 Spark-Plug Defects and Tests. (Fifth Annual,
1919)------------------------------------------
Part 1. Causes of Failure of Spark Plugs.
By F. B. Silsbee.
Part 2. Gas Leakage in Spark Plugs. By
L. Sawyer.
I Part 3. Methods for Tests of Spark Plugs.
By H. C. Dickinson.
52 Temperatures in Spark Plugs having Steel and
Brass Shells. By C. S..Cragoe. (Fifth Annual,
1919)----------------------------------- $0.05
SOut of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of larger cities.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence. National Advisory Committee for Aeronautics.









ENGINES AND ACCESSORIES-Continued
i I
No. Title Price
__}____________________________ I __________________
* 53 Properties and Preparation of Ceramic Insula-
tors for Spark Plugs. (Fifth Annual, 1919)--------
Part 1. Methods of Measuring Resistance
of Insulators at High Temperatures.
By F. B. Silsbee and R. K. Honaman.
Part 2. Electrical Resistance of Various In-
sulating Materials at High Temperatures.
By R. K. Honaman and E. L. Fonseca.
Part 3. Preparation and Composition of
Ceramic Bodies for Spark-Plug Insula-
tors. By A. V. Bleininger.
Part 4. Cements for Spark-Plug Electrodes.
By H. F. Staley.
54 Effect of Temperature and Pressure on the
Sparking Voltage. By F. B. Silsbee and L.
B. Loeb. (Fifth Annual, 1919)-----
55 Investigation of the Muffling Problem for Air-
plane Engines. By G. B. Upton and V. R.
Gage. (Fifth Annual, 1919) --.........----------- $0.10
3 56 Heat Energy of Various Ignition Sparks. (Fifth
Annual, 1919)-------------------- ------
Part 1. Method of Measuring Heat Energy
of Ignition Sparks. By F. B. Silsbee, L.
B. Loeb, and E. L. Fonseca.
Part 2. Measurement of Heat Energy per
Spark of Various Ignition Systems. By
F. B. Silsbee and E. L. Fonseca.
57 The Subsidiary Gap as a Means for Improving
Ignition. By W. S. Gorton. (Fifth Annual,
1919)----------------
3 58 Characteristics of High-Tension Magnetos.
(Fifth Annual, 1919)---- --------------
Part 1. Cycle of Operation of Jump-Spark
Ignition Systems. By F. B. Silsbee.
Part 2. Transformation Ratio and Coupling
in High-Tension Magnetos. By F. B.
Silsbee.
59 General Analysis of Airplane Radiator Problems.
By H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt. (Fifth Annual, 1919)------- .05
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.









ENGINES AND ACCESSORIES-Continued


No.


* Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.


Title Price

General Discussion of Test Methods for Radi-
ators. By H. C. Dickinson, W. S. James, and
W. B. Brown. (Fifth Annual, 1919)------ $0. 10
Head Resistance Due to Radiators. (Fifth
Annual, 1919)---------------------------- .10
Part 1. Head Resistance of Radiator Cores.
By R. V. Kleinschmidt and S. R. Parsons.
Part 2. Preliminary Report on Resistance
Due to Nose Radiator. By R. V. Klein-
schmidt.
Part 3. Effect of Streamline Casing for
Free Air Radiators. By S. R. Parsons.
Effect of Altitude on Radiator Performance.
By W. S. James and S. R. Parsons. (Fifth
Annual, 1919)--------------------------- .10
Results of Tests on Radiators for Aircraft En-
gines. (Fifth Annual, 1919)---------------- .10
Part 1. Heat Dissipation of Radiators. By
H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt.
Part 2. Water Flow through Radiator
Cores. By W. S. James.
Properties of Special Types of Radiators. By
S. R. Parsons. (Sixth Annual, 1920)-------- .10
Effects of Nature of Cooling Surface on Radiator
Performance. By S. R. Parsons and R. V.
Kleinschmidt. (Sixth Annual, 1920)----------
Pressure Drop in Radiator Air Tubes. By S. R.
Parsons. (Sixth Annual, 1920)------------- .05
The Calculated Performance of Airplanes
Equipped with Supercharging Engines. By
E. C. Kemble. (Sixth Annual, 1920)--- 15
Performance of a Liberty 12 Airplane Engine.
By S. W. Sparrow and H. S. White. (Sixth
Annual, 1920)-------------------------- ----
Performance of a 300-horsepower Hispano-
Suiza Airplane Engine. By S. W. Sparrow
and H. S. White. (Sixth Annual, 1920)------ ---
Turbulence in the Air Tubes of Radiators for
Aircraft Engines. By S. R. Parsons. (Sixth
Annual. 1920)--------------------------- .05


62

63





86

3 87

88
101

3102

3103

106









ENGINES AND ACCESSORIES-Continued


No.


Title


Price


3 108 Some Factors of Airplane Engine Performance. ,
By Victor R. Gage. (Sixth Annual, 1920)--------
S123 Simplified Theory of the Magneto. By F. B.
Silsbee. (Seventh Annual, 1921)- -----
3 134 Performance of Maybach 300-horsepower Air-
plane Engine. By S. W. Sparrow. (Eighth
Annual, 1922)------------------------- --
3 135 Performance of B. M. W. 185-horsepower Air-
Splane Engine. By S. W. Sparrow. (Eighth
Annual, 1922) ---------------------
3 158 Mathematical Equations for Head Conduction
in the Fins of Air-Cooled Engines. By D. R.
Harper and W. G. Brown. (Eighth Annual,
1922)------- --------------
3 159 Jet Propulsion for Airplanes. By Edgar Buck-
inghamn. (Ninth Annual, 1923)--------------
3 171 Engine Performance and the Determination of
Absolute Ceiling. By Walter S. Diehl.
(Ninth Annual, 1923)-------------
3 179 The Effect of Electrode Temperature on the
Sparking Voltage of Short Spark Gaps. By
F. B. Silsbee. (Ninth Annual, 1923) -------
3 187 Flame Speed and Spark Intensity. By D. W.
Randolph and F. B. Silsbee. (Tenth Annual,
1924)------------------------ -------
3 189 Relation of Fuel-Air Ratio to Engine Perform-
ance. Bv Stanwood W. Sparrow. (Tenth
Annual, 1924)..------------------ -------
s 190 Correcting Horsepower Measurements to a
Standard Temperature. By Stanwood W.
Sparrow. (Tenth Annual, 1924)-----------------
202 The Sparking Voltage of Spark Plugs. By F. B.
Silsbee. (Tenth Annual, 1924)------------- $0.05
205 The Effect of Changes in Compression Ratio
upon Engine Performance. By Stanwood
W. Sparrow. (Tenth Annual, 1924)------- .10
222 Spray Penetration with a Simple Fuel Injection
Nozzle. By Harold E. Miller and Edward G.
Beardsley. (Eleventh Annual, 1925)__..... .05
I ut of print. Annual volume available for reference or loan in the Office of
Aerfin iluical Intelligence, National Advisory Commitlee for Aeronautics, and in
he libhrairies of large cities.
of Aeronautical Intelligence. Nationql Advisory Committee for Aeronautics.







21

ENGINES AND ACCESSORIES-Continued


No. Title Price

224 An Investigation of the Coefficient of Discharge
of Liquids through Small Round Orifices.
By W. F. Joachim. (Eleventh Annual, 1925) $0.05
230 Description and Laboratory Tests of a Roots
Type Aircraft Engine Supercharger. By
Marsden Ware. (Eleventh Annual, 1925) -.-.-- .10
3 239 i Power Output and Air Requirements of a Two-
Stroke Cycle Engine for Aeronautical Use.
Bv C. R. Paton and Carlton Kemper.
(Twelfth Annual, 1926)--------------------------
241 Electrical Characteristics of Spark Generators
for Automotive Ignition. By R. B. Brode,
D. W. Randolph, and F. B. Silsbee. (Twelfth
Annual, 1926)--------------------------- .15
243 A Preliminary Study of Fuel Injection and Com-
pression Ignition as Applied to an Aircraft
Engine Cylinder. By Arthur W. Gardiner.
(Twelfth Annual, 1926)-------------------- 10
250 Description of the N. A. C. A. Universal Test
Engine and some Test Results. By Marsden
Ware. (Twelfth Annual, 1926)----------- -- 10
252 The Direct Measurement of Engine Power on an
Airplane in Flight with a Hub Type Dyna-
mometer. By W. D. Gove and M. W. Green.
(Twelfth Annual, 1926)-------------------- 10
258 Some Factors Affecting the Reproducibility of
Penetration and the Cut-Off of Oil Sprays for
Fuel Injection Engines. By E. G. Beardsiey.
(Thirteenth Annual, 1927)------------------ .05
3 261 Resistance and Cooling Power of Various Radia-
tors. By R. H. Smith. (Thirteenth Annual,
1927)----------------------------------------
262 Friction of Aviation Engines. By S. W. Spar-
row and M. A. Thorne. (Thirteenth Annual,
1927)------------------------------------ .10
263 Preliminary Flight Tests of the N. A. C. A.
Roots Type Aircraft Engine Supercharger.
By Arthur W. Gardiner and Elliott G. Reid.
(Thirteenth Annual, 1927)---------------- -- 10
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeionautics.







22


ENGINES AND ACCESSORIES-Continued


Title I Price


No.

268


272



274



276


277


280

281


3282


283


284


Factors in the Design of Centrifugal Type In-
jection Valves for Oil Engines. By W. F.
Joachim and E. G. Beardsley. (Thirteenth
Annual, 1927)------ ---------
The Relative Performance Obtained with Several
Methods of Control of an Overcompressed i
Engine Using Gasoline. By Arthur W. Gar-
diner and William E. Whedon. (Thirteenth
Annual, 1927) --------------
The N. A. C. A. Photographic Apparatus for
Studying Fuel Sprays from Oil Engine Injec-
tion Valves and Test Results from Several
Researches. By Edward G. Beardsley.
(Thirteenth Annual, 1927) ---------
Combustion Time in the Engine Cylinder and
Its Effect on Engine Performance. By
Charles F. Marvin, jr. (Thirteenth Annual,
1927) ----------------------
The Comparative Performance of an Aviation
Engine at Normal and High Inlet Air Tem-
peratures. By Arthur W. Gardiner and Oscar
W. Schey. (Thirteenth Annual, 1927) .------
The Gaseous Explosive Reaction-The Effect of
Inert Gases. By F. W. Stevens. (Thirteenth
Annual, 1927)---------------
The Effects of Fuel and Cylinder Gas Densities
on the Characteristics of Fuel Sprays for Oil
Engines. By W. F. Joachim and Edward G.
Beardsley. (Thirteenth Annual, 1927)---.-
The Performance of Several Combustion Cham-
bers Designed for Aircraft Oil Engines. By
William F. Joachim and Carlton Kemper.
(Thirteenth Annual, 1927)----------------
A Preliminary Investigation of Supercharging an
Air-Cooled Engine in Flight. By Marsden
Ware and Oscar W. Schey. (Fourteenth
Annual, 1928)-----------------------
The Comparative Performance of Roots Type
Aircraft Engine Superchargers as Affected by
Change in Impeller Speed and Displacement.
By Marsden Ware and Ernest E. Wilson.
(Fourteenth Annual, 1928)- ---------.---


.10


a Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National AdviEory Commitlee for Aeronautics.


$0. 10



.10



.10


.10


10

.10


.10






,10


I







23


ENGINES AND ACCESSORIES-Continued

No. Title Price

294 The Measurement of Maximum Cylinder Pres-
sures. By Chester W. Hicks. (Fourteenth
Annual, 1928)------------------------- $0.15
295 The Variation in Engine Power with Altitude
Determined from Measurements with a Hub
Dynamometer. Bv W. D. Gove. (Four-
teenth Annual, 1928)---------------------- 10
303 An Investigation of the Use of Discharge Valves
and an Intake Control for Improving the Per-
formance of N. A. C. A. Roots Type Super-
charger. Bv Oscar W. Schey and Ernest E.
Wilson. (Fourteenth Annual, 1928)--------- .10
313 Drag and Cooling with Various Forms of Cowl-
ing for a "Whirlwind" Radial Air-Cooled
Engine-I. By Fred E. Weick. (Fifteenth
Annual, 1929)----------------- ------ .15
314 Drag and Cooling with Various Forms of Cowl-
ing for a "Whirlwind" Radial Air-Cooled
Engine-I1. By Fred E. Weick. (Fifteenth
Annual, 1929)---------------------------- .20
327 The Effect of Supercharger Capacity on Engine
and Airplane Performance. By C. W. Schey
and W. D. Gove. (Fifteenth Annual, 1929)-- .10
330 Experimental and Analytical Determination of
the Motion of Hydraulically Operated Valve
Stems in Oil Engine Injection Systems. By
A. G. Gellales and A. M. Rothrock. (Fifteenth
Annual, 1929)---------------------------- .10
332 The Effect of Cowling on Cylinder Tempera-
tures and Performance of a Wright J-5 En-
gine. By Oscar W. Schey and Arnold E.
Biermann. (Fifteenth Annual, 1929)------- 15
341 The Design and Development of an Automatic
Injection Valve with an Annular Orifice of
Varying Area. By William F. Joachim,
Chester W. Hicks and Hampton W. Foster.
(Sixteenth Annual, 1930)------------------ .10
355 Comparative Flight Performance with an N. A.
C. A. Roots Supercharger and a Turbocen-
trifugal Supercharger. By Oscar W. Schey
and Alfred W. Young. (Sixteenth Annual,
1930).----------------------------------- 10







24

ENGINES AND ACCESSORIES-Continued


Title


3.5)9


Price
i


:3 73

374


3S4


390


399


401

402

403



404


Art Investigation of the Effectiveness of Ign'tion
Sparks. By Melville F. Peters, Wayne L.
Summerville, and Merlin Davis. (Sixteenth
Annual, 1930)---------------------------
Pressure Fluctuation in a Common-Rail Fuel
Injection System. By A. M. Rothrock.
(Sixteenth Annual, 1930)---------------
Coeimciewiis of Discharge of Fuel Injection Noz-
zles for Compression-Ignition Engines. By
A. i. Gelalles. (Seventeenth Annual, 1931) -__
The Automotive Ignition Coil. By T. H. Dar-
nell. Note by F. B. Silsbee. (Seventeenth
Annual, 1931)---------------------------
Tie Comparative Performance of Superchargers.
By Oscar W. Schev (Seventeenth Annual,
1931)------------------------
Thel Effect of Valve Timing upon the Perform-
anve of a Supercharged Engine at Altitude and
an ULnssiipercharged Engine at Sea Level. By
Oscar W. Schey and Arnold E. Biermann.
(Seventeenth Annual, 1931)---------------
Hydraulics of Fuel Injection Pumps for Com-
pression-Ignition Engines. By A. M. Roth-
rock. (Seventeenth Annual, 1931)----------
Flamec Movement and Pressure D)evelopment in
an Engine Cylinder. By Charles F. MarvinI
and Robert D. Best. (Seventeenth Annual,
1931)------------------------------------
Combustion in High-Speed Compression-Igni-
tion Enigine. By A. M. Rothrock. (Eight-
centhi Annual, 1932)-----------------------
Effrect of Orifice Length-Diamneter Ratio on Fuel
Sprays for Compression-Ignition Engine. By
A. G. Gelalles. (Eighteenth Annual, 1932). -
Ice Prevention on Aircraft by Means of Engine
Exhaust Heat and a Technical Study of Heat
Tratnsmnission from a Clark Y Airfoil. By
Tiheodore Tfiheodorsen & William C. Clay.
(Eiglteenth ,Annual, 1932).-----------------
T'1ie Effect (if Iincreased Carburetor Pressure on
Engine Performriance at Several Compression
Ratios. By Oscar W. Schev and Vern G.
Rollin. (Eiglteenttlh Annual, 1932).-..-...!


.10


$0. 10


10

.10

25


.05



.10


.25


.10

15

15



.20







25


ENGINES AND ACCESSORIES-Continued


Title


Price


No.

409

414


FUELS

A New Process for the Production of Aircraft-
Engine Fuels. By Auguste Jean Paris, jr., and
W. Francklyn Paris. (Fourth Annual, 1918) - - - -
Power Characteristics of Fuels for Aircraft
Engines. (Fourth Annual, 1918)
Part 1. Power Characteristics of Aviation
Gasoline. By E. W. Roberts.
Part 2. Power Characteristics of Sumatra
and Borneo Gasolines. By E. W. Roberts.
Part 3. Power Characteristics of 20 per
cent Benzol Mixtures. By E. W. Roberts.
Comparison of Alcogas Aviation Fuel with
Export Aviation Gasoline. By V. R. Gage,
S. W. Sparrow, and D. R. Harper. (Sixth
Annual, 1920) ---------------------- $0.05
Comparison of Hector Fuel with Export Aviation
Gasoline. By H. C. Dickinson, V. R. Gage,
and S. W. Sparrow. (Sixth Annual, 1920.)___ .05
Fuels for High-Compression Engines. By Stan-
wood W. Sparrow. (Eleventh Annual, 1925)- 10
The Gaseous Explosive Reaction-A Study of
the Kinetics of Composite Fuels. By F. W.
Stevens. (Fourteenth Annual, 1928)-------- 15


I Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


The Elimination of Fire Hazard due to Back-
Fires. Theodore Theodorsen and Ira M.
Freeman. (Eighteenth Annual, 1932) ------ $0. 10
The Effect on Airplane Performance of Several
Types of Low-Drag Cowling for Radial Air-
Cooled Engines. By Wm. H. McAvoy,
Oscar W. Schey, and Alfred W. Young.
(Eighteenth Annual, 1932) ------------------ .20
The Effect of Nozzle Design and Operation Con-
ditions on the Atomization and Distribution
of Fuel Sprays. By Dana W. Lee. (Eight-
eenth Annual, 1932) ------- -------
The Effect of Humidity on Engine Power at
Altitude. By D. B. Brooks and E. A. Gar-
lock. (Eighteenth Annual, 1932)-------------


425


426


3 42

3 47






89


90

232

305







26

FUELS-Continued

No. Title Price

321 Fuel Vapor Pressures and Their Relation to the
Preparation of Fuel for Combustion in Fuel
Injection Engines. By W. F. Joachim and
A. M. Rothrock. (Fifteenth Annual, 1929) ----
337 The Gaseous Explosive Reaction at Constant $0. 10
Pressure-The Reaction Order and Reaction
Rate. By F. W. Stevens. (Sixteenth Annual,
1930)---------------------
372 The Gaseous Explosive Reaction: The Effect of 10
Pressure on the Rate of Propagation of the
Reaction Zone and upon the Rate of Molecular
Transformation, By F. W. Stevens. (Seven-
teenth Annual, 1931)---------------------- .15

GASES

40 The Ferrosilicon Process for the Generation of
Hydrogen. By E. R. Weaver, W. M. Berry, I
V. L. Bohnson, and B. D. Gordon. (Fourth
Annual, 1918)-------------------------- $0. 15
41 Testing of Balloon Gas. By Junius David
Edwards. (Fourth Annual, 1918)----------- .05

HELICOPTERS

a 80 Stability of the Parachute and Helicopter. By
H. Bateman. (Fifth Annual, 1919)---------------

HYDRODYNAMICS

116 Applications of Modern Hydrodynamics to
Aeronautics. By L. Prandtl. (Seventh
Annual, 1921)..-- --------------$0. 10
405 Application of Practical Hydrodynamics to Air-
1ship Design. By R. H. Upson and W. A.
Klikoff. (Eighteenth Annual, 1932)--------- .15

Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.







27


INSTRUMENTS


Title


12





8


31

32

50

81

94

99

100

3 107

2l10

125


Price


Investigation of Pitot Tubes. (First Annual,
1915)--------------------------------
Part 1. The Pitot Tube and Other Ane-
mometers for Airplanes. By W. H.
Herschel.
Part 2. The Theory of the Pitot and Ven-
turi Tubes. By E. Buckingham.
General Specifications Covering Requirements
of Aeronautic Instruments. By National
Advisory Committee for Aeronautics. (Sec-
ond Annual, 1916) ---------------
Development of Air Speed Nozzles. By A. F.
Zahm. (Fourth Annual, 1918) --------
The Airplane Tensiometer. By L. J. Larson.
(Fourth Annual, 1918)--------------------
Calculation of Low Pressure Indicator Dia-
grams. By E. C. Kemble. (Fourth Annual,
1918)------- -------------------------
Comparison of U. S. and British Standard
Pitot-Static Tubes. By A. F. Zahm and R. H.
Smith. (Fifth Annual, 1919)----------
The Efficiency of Small Bearings in Instruments
of the Type Used in Aircraft. By F. H.
Norton. (Sixth Annual, 1920) --------
Acceleration in Flight. By F. H. Norton and
E. T. Alien. (Sixth Annual, 1920)-----
Accelerometer Design. By F. H. Norton and
Edward P. Warner. (Sixth Annual, 1920)--
A High-Speed Engine Pressure Indicator of the
Balanced Diaphragm Type. By H. C. Dick-
inson and F. B. Newell. (Sixth Annual, 1920)
The Altitude Effect on Air Speed Indicators.
By M. D. Hersey, F. L. Hunt, and H. N.
Eaton. (Sixth Annual, 1920)--------------
Aeronautic Instruments: Section I-General
Classification of Instruments and Problems,
Including Bibliography. By Bureau of
Standards. (Seventh Annual, 1921)----


I .05


1 Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence. National Advisory Committee for Aeronautics, and in
the libraries of large cities.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.
112472-32-3


No.


$0. 10

.05

.05

.05

.05

.10


I







28


INSTRUMENTS-Continued


Title


126







127





128








129








130

131


3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautcsa.


No.


Aeronautic Instruments: Section II-Altitude
Instruments. By Bureau of Standards.
(Seventh Annual, 1921)__ ------
Part 1. Altimeters and Barographs.
Part 2. Precision Altimeter Design.
Part 3. Statiscopes and Rate-of-Climb In-
dicators. .
Part. 4. Aerographs and Strut Thermome-
ters.
Aeronautic Instruments: Section III-Aircraft
Speed Instruments. By Bureau of Stand-
ards. (Seventh Annual, 1921)-- -..----
Part 1. Air Speed Indicators.
Part 2. Testing of Air Speed Meters.
Part 3. Principles of Ground-Speed Instru-
ments.
Aeronautic Instruments: Section IV-Direc-
tion Instruments. By Bureau of Standards.
(Seventh Annual, 1921)------ ----
Part 1. Inclinometers and Banking Indi-
cators.
Part 2. The Testing and Use of Magnetic
Compasses for Airplanes.
Part 3. Aircraft Compasses-Description
and Classification.
Part 4. Turn Indicators.
Aeronautic Instruments: Section V-Power-
Plant Instruments. By Bureau of Stand-
ards. (Seventh Annual, 1921)---------
Part 1. Airplane Tachometers.
Part 2. Testing of Airplane Tachometers.
Part 3. Thermometers for Aircraft Engines.
Part 4. Air-Pressure and Oil-Pressure
Gages.
Part 5. Gasoline-Depth Gages and Flow
Meters for Aircraft.
Aeronautic Instruments: Section VI-Oxygen
Instruments. By Bureau of Standards.
(Seventh Annual, 1921)--------------------
Aeronautic Instruments: Section VII-Aerial
Navigation Instruments. By Bureau of
Standards. (Seventh Annual, 1921).....--


Price



$0. 25







.10





.25


1 .10


I







29

INSTRUMENTS-Continued

No. Title Price

132 Aeronautic Instruments: Section VIII-Recent
Developments and Outstanding Problems.
By Bureau of Standards. (Seventh Annual,
1921)----------------------------------- $0.05
3 156 The Altitude Effect of Air Speed Indicators-II.
By H. N. Eaton and W. A. McNair. (Eighth
Annual, 1922)------- --- ---
160 An Airship Slide Rule. By E. R. Weaver and
S. F. Pickering. (Ninth Annual, 1923)----------
165 Diaphragms for Aeronautic Instruments. By
M. D. Hersey. (Ninth Annual, 1923)-------------
166 The Aerodynamic Plane Table. By A. F.
Zahm. (Ninth Annual, 1923)-------------- .05
176 A Constant-Pressure Bomb. Bv F. W. Stevens.
(Ninth Annual, 1923)---------------------- .05
198 Astronomical Methods in Aerial Navigation.
By K. Hiding Beij. (Tenth Annual, 1924)-- 15
199 Interference Tests on an N. A. C. A. Pitot Tube.
SBy Elliott G. Reid. (Tenth Annual, 1924) -- 05
206 Nonmetallic Diaphragms for Instruments. By
H. N. Eaton and C. T. Buckingham. (Tenth
SAnnual, 1924)-----------------------------
264 Differential Pressures on a Pitot-Venturi and a
Pitot-static Nozzle Over 360 Pitch and Yaw.
By R. M. Bear. (Thirteenth Annual, 1927)__ .05
270 The Measurement of Pressure Through Tubes
in Pressure Distribution Tests. By Paul E.
Hemke. (Thirteenth Annual, 1927) --------- 10
299 Investigation of Damping Liquids for Aircraft
Instruments. By G. H. Keulegan. (Four-
teenth Annual, 1928)---------------------- 10
310 Pressure Element of Constant Logarithmic
Stiffness for Temperature Compensated Alti-
meter. By W. G. Brombacher and F.
Cordero. (Fifteenth Annual, 1929)--------- 10
320 The Measurement of Fluctuations of Air Speed
by the Hot Wire Anemometer. By H. L.
Dryden and A. M. Keuthe. (Fifteenth An-
nual, 1929)-------------------------------- 15
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical IntelItence, National Advisory Committee for Aeronautics.







30

INSTRUMENTS-Continued

No. Title Price

358 Temperature Coefficient of the Modulus of
Rigidity of Aircraft Instrument Diaphragm
and Spring Materials. By W. G. Brom-
bacher and E. R. Melton. (Sixteenth Annual,
1930) -------------------------- $0.10
371 Present Status of Aircraft Instruments. By
the Subcommittee on Air Navigation In-
struments. (Seventeenth Annual, 1931)------ .15
388 Pressure Cell Investigation. By Theodore
Theodorsen. (Seventeenth Annual, 1931)---- .10
398 Investigation of Damping Liquids for Aircraft
Instruments-II. By M. R. Houseman and
H. W. Kirschbaum. (Seventeenth Annual,
1931)----------------------------------- .15
420 Aircraft Speed Instruments. By K. Hilding
Beij. (Eighteenth Annual, 1932) --------

MATERIALS

15 Relative Worth of Improvements on Fabrics.
Bv the Goodyear Tire & Rubber Co.
(First Annual, 1915)-- ---------------
1 6 Investigations of Balloon and Airplane Fabrics.
(First Annual, 1915) --------------
Part 1. Balloon and Airplane Fabrics. By
Willis A. Gibbons and Omar H. Smith.
Part. 2. Skin Friction of Various Surfaces
in Air. By Willis A. Gibbons.
S16 The Stretching of the Fabric and the Deforma-
tion of the Envelope in Nonrigid Balloons.
(Third Annual, 1917) ------------
Part 1. The Stretching of the Fabric and
the Shape of the Envelope. By Rudolf
Haas.
Part 2. The Deformation of the Envelope
of the Siemens-Schuckert Airships.
By Alexander Dietzius.*
I Out of print. Annual volume available for reference or loan In the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
SNot issued as a separate report. The annual volume containing this report is
still available.









MATERIALS-Continued

No. Title Price

1 22 Fabrics for Aeronautic Construction. By Sub-
committee on Standardization and Investi-
gation of Materials. (Third Annual, 1917)--- -----
Part 1. Cotton Airplane Fabrics.
Part 2. Balloon Fabrics.
3 33 Self-Luminous Materials. By N. E. Dorsey.
(Fourth Annual, 1918)-----------------------
1 34 Aluminum and Its Light Alloys. By Paul D.
Merica. (Fourth Annual, 1918)--------------
136 The Structure of Airplane Fabrics. By E.
Dean Walen. (Fourth Annual, 1918)---------
3 37 Fabric Fastenings. By E. Dean Walen and R.
T. Fisher. (Fourth Annual, 1918)-------------
1 38 Airplane Dopes and Doping. By W. H. Smith.
(Fourth Annual, 1918)----------------------
39 The Testing of Balloon Fabrics. By Junius
David Edwards and Irwin L. Moore.
(Fourth Annual, 1918)-------------------- $0.05
Part 1. Characteristic Exposure Tests of
Balloon Fabrics.
Part 2. Use of Ultra-Violet Light for Test-
ing Balloon Fabrics.
8 65 The Kiln Drying of Woods for Airplanes. By
Harry D. Tieman. (Fifth Annual, 1919)----
3 66 Glues Used in Airplane Parts. By S. W. Allen
and T. R. Truax. (Fifth Annual, 1919)------
3 67 Supplies and Production of Aircraft Woods.
By W. N. Sparhawk. (Fifth Annual, 1919)----
68 The Effect of Kiln Drying on the Strength of
Airplane Woods. By T. R. C. Wilson. (Fifth
Annual, 1919)----------------------------. 15
84 Data on the Design of Plywood for Aircraft.
By Armin Elmendorf. (Sixth Annual, 1920)----
3 85 Moisture Resistant Finishes for Airplane Woods.
By M. E. Dunlap. (Sixth Annual, 1920)-----
S145 Internal Stresses in Laminated Construction.
By A. L. Heim, A. C. Knauss, and Louis Seut-
ter. (Eighth Annual, 1922)-- -- --- ___
I Out of print. Annual volume available foo reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the librarier of large cities.
I Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.
Not issued as a separate report. The annual volume containing this report is
still available.









MATERIALS-Continued

No. Title Price

248 The Corrosion of Magnesium and of the Mag-
nesium Aluminum Alloys Containing Manga-
nese. ByJ. A. Boyer. (Twelfth Annual,1926). $0. 20
354 Aircraft Woods: Their Properties, Selection,
and Characteristics. By L. J. Markwardt.
(Sixteenth Annual, 1930) ------------------- 20
356 Strength of Rectangular Flat Plates under Edge
Compression. By Louis Schuman and Goldie
Back. (Sixteenth Annual, 1930)------------ .15
382 The Elastic Instability of Members having Sec-
tions Common in Aircraft Construction. By
George W. Trayer and H. W. March. (Sev-
enteenth Annual, 1931)--------------------- .25

METEOROLOGY

1 4 Preliminary Report on the Problem of the At-
mosphere in Relation to Aeronautics. By
Charles F. Marvin. (First Annual, 1915)-------
13 Meteorology and Aeronautics. By Win. R.
Blair. (Third Annual, 1917)--------------- $0.10
Part 1. Physical Properties and Dynamics
of the Atmosphere.
Part 2. Topograpllic and Climatic Factors
in Relation to Aeronautics.
Part 3. Current Meteorology and Its Use.
3 147 Standard Atmosphere. By Willis Ray Gregg.
(Eighth Annual, 1922)-----------------------
1 216 The Reduction of Airplane Flight-Test Data to
Standard At mosphere Conditions. By Wal-
ter S. Diclil and E. P. Lesley. (Eleventh An-
nual, 1925)-------------------------------------
218 Staml:ard Atnimsplllere-Tales and Data. By
Walter S. Dicil. (Eleventh Annual, 1925) --- 10
245 Meteorol,,gicail Conditions along Airways. By
W. R. Gregg. (Twelfth Annual, 1926 ---. 10
SOut of print. Annual volume available fur reference or loan in the Office of
Aeronau;ical Intelligence, National Advisory Committee fur Aeronautics, and in
the libraries ,f large cities.
' Out of print. A available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.







33

METEOROLOGY-Continued

No. Title Price

'246 Tables for Calibrating Altimeters and Com-
puting Altitudes Based on the Standard At-
mosphere. By W. G. Brombacher. (Twelfth
Annual, 1926)---------------------------------
376 Some Approximate Equations for the Standard
Atmosphere. By Walter S. Diehl. (Seven-
teenth Annual, 1931)---------------------- $0.15

MISCELLAN EOUS

308 Aircraft Accidents-Methods of Analysis. By
the Special Committee on the Nomenclature,
Subdivision, and Classification of Aircraft
Accidents, N. A. C. A. (Fourteenth Annual,
1928)----------------------------------- $0. 10
357 Aircraft Accidents-Method of Analysis. By
the Committee on Aircraft Accidents. (Six-
teenth Annual, 1930)---------------------- 10

NOMENCLATURE

2 9 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Sec-
ond Annual, 1916)-----------------------------
215 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Third
Annual, 1917)----------------------------------
S25 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Fourth
Annual, 1918)-------------------------------
91 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Sixth
Annual, 1920)---------------------------- $0. 15
3157 Nomenclature for Aeronautics. By National
Advisory Committee for Aeronautics. (Eighth
Annual, 1922)----------- -- -----
S Out of print as a separate report. The annual volume containing this report is
still available.
s Out of print. Available as a separate report for reference or loan in the Offce
of Aeronautical Intelligence, Nationiil Advisory ('ommiltee for Aeronautics.









NOM ENCLATU RE-Continued
No. Title Price

240 Nomenclature for Aeronautics. By Nation- I
al Advisory Committee for Aeronautics.
(Twelfth Annual. 1926)------------------ $0.20
NOTE-Reports 9, 15, 25, 91, 157 are obso-
lete.

PARACHUTES

3 80 Stability of the Parachute and Helicopter. By
H. Bateman. (Fifth Annual, 1919) ------

PROPELLERS

3 14 Experimental Research on Air Propellers. Byv
Win. F. Durand. (Third Annual, 1917)--------
Part 1. The Aerodynamic Laboratory at
Leland Stanford Junior University and
the Equipment Installed with Special
Reference to Tests on Air Propellers.
Part 2. Tests on 48 Model Forms of Air
Propellers, with Analysis and Discussion
of Results and Presentation of the Same
in Graphic Form.
Part 3. A Brief Discussion of the Law of
Similitude as Affecting the Relation Be-
tween the Results Derived from Model
Forms and Those to be Anticipated from
Full-sized Forms.
2 19 Periodic Stresses in Gyroscopic Bodies-with
Applications to Air Screws. By A. F. Zahm.
(Third Annual, 1917)------------------------
Part 1. The Gyroscopic Particle.
Part 2. The Gyroscopic Three-Dimensional
Bod y.
3 29 The General Theory of Blade Screws. By
George de Bothezat. (Fourth Annual, 1918) ------
130 Experimental Research on Air Propellers-II.
By Wmin. F. Durand and E. P. Lesley. (Fourth
Annual, 1918)---------------------------------
SOuti of print. Annual volume available for reference or loan in the Office of
Aeronrauticail Intelligence, National Advisory Committee for Aeronautics, and In
the libraries of large cities.
L Out of print as a separate report. The annual volume containing this report is
still available.
3 Out of print. Available as a separate report for reference or loan in the Office
of A.erornaiit ical lnlelligence. National Advisory Committee for Aeronautics.







35


PROPELLERS-Continued


No. Title Price

64 Experimental Research on Air Propellers-III.
By Wm. F. Durand and E. P. Lesley. (Fifth
Annual, 1919)---------------------------- $0.10
71 Slip-Stream Corrections in Performance Com-
putation. By Edward P. Warner. (Fifth
Annual, 1919)---------------------------- .05
3109 Experimental Research on Air Propellers-IV.
By Wm. F. Durand and E. P. Lesley. (Sixth
Annual, 1920)----------------------------------
113 Tests on Air Propellers in Yaw. By Wm. F.
Durand and E. P. Lesley. (Seventh Annual,
1921)----------------------------------- .10
141 Experimental Research on Air Propellers-V.
By Wm. F. Durand and E. P. Lesley. (Eighth
Annual, 1922)---------------------------- .15
S168 The General Efficiency Curve for Air Propellers.
By Walter S. Diehl. (Ninth Annual, 1923)_
S175 Analysis of W. F. Durand's and E. P. Lesley's
Propeller Tests. By Max M. Munk. (Ninth
Annual, 1923)-----------------------------
'177 The Effect of Slip-Stream Obstructions on Air
Propellers. By E. P. Lesley and B. M.
Woods. (Ninth Annual, 1923)-------------------
S178 Relative Efficiency of Direct and Geared Drive
Propellers. By Walter S. Diehl. (Ninth An-
nual, 1923)------------------------------------
' 183 The Analysis of Free-Flight Propeller Tests and
Its Application to Design. By Max M.
Munk. (Ninth Annual, 1923)--------------
3186 Application of Propeller-Test Data to Design
and Performance Calculations. By Walter
S. Diehl. (Tenth Annual, 1924)------ -----
's196 Comparison of Model Propeller Tests with the
Airfoil Theory. By W. F. Durand and E. P.
Lesley. (Tenth Annual, 1924)-----------
220 Comparison of Tests on Airplane Propeller in
Fligh t with Wind-Tu nnel Model Tests on Simi-
lar Forms. Bv W. F. Durand and E. P. Les-
ley. (Eleventh Annual, 1925)-------------- 15
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Commitiee for Aeronautics.







36


PROPELLERS-Conlinucd


No.


Title


3


S( )ti of print. Avaiiliiable as a separate report fir reference or loan in the Office
of Aeronautical Intelligence. National Advisiiry committeeee fur Aeronautics


235 Interaction between Air Propellers and Airplane
Structures. By WV. F. Durand. (Twelfth An-
nual, 1926)-------------------------
237 Tests on Thirteen Navv Type Model Propellers.
By \'. F. Durand. (Twelfth Annual, 1926)--
259 Characteristics of Propeller Sections Tested in
the Variable Density Wind Tunnel. By East-
man N. Jacobs. (Thirteenth Annual, 1927)--
292 Characteristics of Five PropeUers in Flight.
By J. W. Crowley, jr., and R. E. Mixson.
(Fourteenth Annual, 192S)-----------------
301 Full Scale Tests of Wood Propellers on a VE-7
Airplane in the Propeller Research Tunnel.
By Fred E. Weick. (Fourteenth Annual,
192S)------------------------------------
302 Full Scale Tests on a Thin Metal Propeller at
Various Tip Speeds. By Fred E. Weick.
(Fourteenth Annual, 1928)-----------------
306 Full Scale Wind Tunnel Tests of a Series of
Metal Propellers on a VE-7 Airplane. By
Fred E. Weick. (Fourteenth Annual, 1928) -
326 Tests of Five Metal Model Propellers with Va-
riouts Pitch Distributions in a Free Wind
Stream and in Comibination with a Model
VE-7 Fuselage. By E. P. Leslev and Elliott
G. Reid. (Fifteenth Annual, 1929)---------
338 The Effect of Reduction Gearing on Propeller-
Body Interference as Shown by Full Scale
Wind 'Tunnel Tests. By Fred E. Weick.
(Sixteenth Annual, 1930)---------------
339 Full Scale Wind Tunnel Tests with a Series of
Propellers of Differentt Diameters on a Single
IFuselage. By Fred E. Weick. (Sixteenth
..An\ nual, 1 3'( I- --- ------------------------
340 Full Scale Wind 'uimnel Tests on Several Metal
lPrpellers having Differentt Blade Forms.
I\By Frcd E. Weick. (Sixteenth Annual, 1930)__-
35.( \\ A\ll( v Propellers of a Stnadard Form to
()]>i'te w\ithi Various Aircraft Engines aind
IBodies. By Fred E. \Veick. (Sixteentht
.\iiriitil, 193()----------------------------


Price


$0. 10

.10

.15


.15

.10

.10



15


.15


.15


.10


I .10









PROPELLERS-Continued


Title


Full-Scale Wind Tunnel Tests of a Propeller
with the Diameter Changed by Cutting Off
the Blade Tips. By Donald H. Wood. (Six-
teenth Annual, 1930)----------------------
Tests of Metal Propeller at High Tip Speeds.
By Donald H. Wood. (Seventeenth Annual,
1931)-----------------------------------
A Comparison of Propellers having R. A. F.-6
and Clark Y Airfoil Sections. By Hugh
B. Freeman. (Seventeenth Annual, 1931)---
The Effect of Small Angles of Yaw and Pitch
on the Characteristics of Airplane Propellers.
By Hugh B. Freeman. (Seventeenth Annual,
1931)-----------------------------------
Tests of Nacelle-Propeller Combinations in
Various Positions with Reference to Wings.
Part I. Thick Wing-N. A. C. A. Cowled
Nacelle-Tractor Propeller. By Donald H.
Wood. (Eighteenth Annual, 1932)---------
Measurement of the Differential and Total
Thrust and Torque of Six Full-Scale Adjust-
able-Pitch Propellers. By George W. Stickle.
(Eighteenth Annual, 1932)-------------


SEAPLANES


Characteristics of a Single-Float Seaplane during
Take-off. By J. W. Crowley, jr., and K. M.
Ronan. (Tenth Annual, 1924)---- --
Characteristics of a Boat-Type Seaplane during
Take-Off. By J. W. Crowley, jr., and K. M.
Ronan. (Eleventh Annual, 1925)-----------
Characteristics of a Twin-Float Seaplane during
Take-Off. By John W. Crowley, jr., and K.
M. Ronan. (Twelfth Annual, 1926)------
Water Pressure Distribution on a Seaplane
Float. By F. L. Thompson. (Fourteenth
Annual, 1928) ---------------------
Water Pressure Distribution on a Twin-Float
Seaplane. By F. L. Thompson. (Fifteenth
Annual, 1929)- ---------------------


$0.10

.10

.10


'Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


No.


351


375

378

389


415



421


Price




$0. 15

.10

.10


.10



.10


3 209

9226

242

290

328


-1 -









SEA PLANES-Continued

No. Title Price

346 Water Pressure Distribution on a Flying Boat
Hull. By F. L. Thompson. (Sixteenth
Annual, 1930) --------------------------_ $0. 10

STABILITY AND CONTROL

1 1 Report on Behavior of Airplanes in Gusts.
(First Annual, 1915)--------- -----------------
Part 1. Experimental Analysis of Inherent
Longitudinal Stability for a Typical Bi-
plane. By J. C. Hunsaker.
Part 2. Theory of an Airplane Encounter-
ing Gusts. By E. B. Wilson.
4 17 An Investigation of the Elements which Con-
tribute to Statical and Dynamical Stability,
and of the Effects of Variation in those Ele-
ments. By Alexander Klemin, Edward P.
Warner, and George M. Denkinger. (Third
Annual, 1917)-------------------------------
4 21 Theory of an Airplane Encountering Gusts-II.
By E. B. Wilson. (Third Annual, 1917)----------
2 26 The Variation of Yawing Moment Due to Roll-
ing. By E. B. Wilson. (Fourth Annual, I
1918)-------------------------------------
2 27 Theory of an Airplane Encountering Gusts-III. I
By E. B. Wilson. (Fourth Annual, 1918)----------
2 95 Diagrams of Airplane Stability. By H. Bate-
men. (Sixth Annual, 1920) --------------------
1 96 Statical Longitudinal Stability of Airplanes. I
By Edward P. Warner. (Sixth Annual, 1920)-------
112 Control in Circling Flight. By F. H. Norton 1
and E. T. Allen. (Seventh Annual, 1921)_--- $0. 10
8 120 Practical Stability and Controllability of Air-
planes. By F. H. Norton. (Seventh Annual,
1921)---------------------- --------..----
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities.
2 Out of print as a separate report. The annual volume containing this report is
still available.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.
4 Not Issued as a separate report. The annual volume containing this report Is
still available.







39


STABILITY AND CONTROL-Continued

No. Title Price

3 153 Controllability and Maneuverability of Air-
planes. By F. H. Norton and W. G. Brown.
(Eighth Annual, 1922)----------------------
172 Dynamic Stability as Affected by the Longi-
tudinal Moment of Inertia. By Edwin B.
Wilson. (Ninth Annual, 1923)----------- $0. 05
293 Two Practical Methods for the Calculation of
the Horizontal Tail Area Necessary for a
StaticaUlly Stable Airplane. By Walter S.
Diehl. (Fourteenth Annual, 1928)---------- .10
298 Effect of Variation of Chord and Span of Aile-
rons on Rolling and Yawing Moments in
Level Flight. By R. H. Held and D. L.
Strother. (Fourteenth Annual, 1928) ------- 10
343 Effect of Variation of Chord and Span of Aile-
rons on Rolling and Yawing Moments at
Several Angles of Pitch. By R. H. Heald,
D. H. Strother, and B. H. Monish. (Sixteenth
Annual, 1930)--------------------- .15
379 Rolling Moments due to Rolling and Yaw for
Four Wring Models in Rotation. By Mont-
gomery Knight and Carl J. Wenzinger.
(Seventeenth Annual, 1931)---------------- .15
393 Span-Load Distribution as a Factor in Stability
in Roll. By Montgomery Knight and Richard
W. Noyes. (Seventeenth Annual, 1931)---- .10

STRENGTH OF CONSTRUCTION

1 3 Report on the Investigations of Aviation Wires
and Cables, Their Fastenings and Terminal
Connections. By John A. Roebling's Sons
Co. (First Annual, 1915)----------------------
3 35 The Strength of One-Piece, Solid, Built-Up, and
Laminated Wood Airplane Wing Beams.
By John H. Nelson. (Fourth Annual, 1918)----_
3 76 Analysis of Fuselage Stresses. By Edward P.
Warner and Roy G. Miller. (Fifth Annual,
1919)-----------------------
Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, and in
the libraries of large cities
'Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.







40

STRENGTH OF CONSTRUCTION-Continued

No. Title Price

3 82 Airplane Stress Analysis. By A. F. Zahm.
(Fifth Annual, 1919)------------- -- --
3 92 Analysis of Wing Truss Stresses. By Edward
P. Warner and Roy G. Miller. (Sixth Annual,
1920)----------------------------------
S104 Torsion of Wing Trusses at Diving Speeds.
By Roy G. Miller. (Sixth Annual, 1920)--------
137 Point Drag and Total Drag of Navy Struts
No. 1 Modified. By A. F. Zahmin, R. H.
Smith, and G. C. Hill. (Eighth Annual, 1922). $0. 05
140 Lift and Drag Effects on Wing Tip-Rake. By
A. F. Zahm, R. M. Bear, and G. C. Hill.
.Eighth Annual, 1922)-------------- ----
s 143 Analysis of Stresses in German Airplanes. By
Wilhelm Hoff. (Eighth Annual, 1922)...----
3 161 The Distribution of Lift over Wing Tips and
Ailerons. By David L. Bacon. (Ninth
Annual, 1923). ----------------- ----
180 The Influence of the Furm of a Wooden Beam
on Its Stiffness and Strength-I: Deflection
of Beams with Special Reference to Shear
Deformations. By J. A. Newlin and G. W.
Trayer. (.Ninth Annual, 1923) ------------
IS1 The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-lI: Form
Factors of Beams Subjected to Transverse
Loading Only. By J. A. Newlin and G. W.
Trayer. (Ninth Annual, 1923)-------------------
3 188 The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-III: Stresses
in Wood Members Subjected to Combined
Column and Beam Action. By J. A. Newlin
and G. WV. Trayer. (Tenth Annual, 1924)..........
214 Wing Spar Stress Charts and Wing Truss
Proportions. By Edward P. Warner. (Elev-
enth Annual, 1925)------------------------- 10
251 Approximations for Column Effect in Airplane
Wing Spars. By Edward P. Warner and
Mac Short. (Twelfth Annual, 1926)-------- 10
329 The Torsional Strength of Wings. By C. P.
i Burgess. (Fifteenth Annual, 1929)---------I- .10
Out of print. Avinilahile as a separate report for reference or loan in the Office
of Aeronautical Intelligence. National Advisory Committee for Aeronautics.









STRENGTH OF CONSTRUCTION-Continued
No. Title Price

334 The Torsion of Members Having Sections
Common in Aircraft Construction. By
George W. Trayer and H. W. March. (Fif-
teenth Annual, 1929)--------------------- $0.25
344 The Design of Plywood Webs for Airplane Wing
Beams. By George W. Trayer. (Sixteenth
Annual, 1930)---------------------------- .10
345 The Design of Airplane Wing Ribs. By J. A.
Newlin and George W, Trayer. (Sixteenth
Annual, 1930) ---------------------------- .25
347 A Method of Calculating the Ultimate Strength
of Continuous Beams. By J. A. Newlin and
Geo. W. Trayer. (Sixteenth Annual, 1930)-- 10
348 Strength of Welded Joints in Tubular Members
for Aircraft. By H. L. Whittemore and
W. C. Brueggeman. (Sixteenth Annual, 1930) .30
382 The Elastic Instability of Members having
Sections Common in Aircraft Construction.
By George W. Traver and H. W. March.
(Seventeenth Annual, 1931)--------------- .25

WIND TUNNELS AND LABORATORIES

3 44 The Altitude Laboratory for the Testing of
Aircraft Engines. By H. C. Dickinson and
H. G. Boutell. (Fourth Annual, 1918)-----------
72 Wind-tunnel Balances. By Edw-ard P. Warner
and F. H. Norton. (Fifth Annual, 1919)_--- $0. 10
3 73 The Design of Wind Tunnels and Wind-tunnel
Propellers. By Edward P. Warner and F.
H. Norton. (Fifth Annual, 1919)---------------
3 74 Construction of Models for Tests in Wind Tun-
nels. By F. H. Norton. (Fifth Annual,
1919)------------------------
98 Design of Wind Tunnels and Wind-Tunnel
Propellers-I1. By F. H. Norton and Ed-
ward P. Warner. (Sixth Annual, 1920)----- .10
3 146 The Six-Component Wind Balance. By A. F.
Zahm. (Eighth Annual, 1922)----------------
195 Standardization Tests of N. A. C. A. No. 1
Wind Tunnel. By Elliott G. Reid. (Tenth
Annual, 1924)---------------------------- .10
:'Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.









WIND TUNNELS AND LABORATORIES-Continued

No. Title Price

227 The Variable-Density Wind Tunnel of the
National Advisory Committee for Aeronau-
tics. By Max M. Munk and Elton W. Miller.
(Eleventh Annual, 1925)------------------ $0. 10
231 Investigation of Turbulence in Wind Tunnels by
a Study of the Flow About Cylinders. By
H. L. Dryden and R. H. Heald. (Eleventh
Annual, 1925)--------------------------- 10
275 The Effect of the Walls in Closed Type Wind
Tunnels. By George J. Higgins. (Thirteenth
Annual, 1927)---------------------------- .10
300 The Twenty-Foot Propeller Research Tunnel of
the National Advisory Committee for Aero-
nautics. By Fred E. Weick and Donald H.
Wood. (Fourteenth Annual, 1928)---------- .10
322 Investigation of Air Flow in Open Throat Wind
Tunnels. By Eastman N. Jacobs. (Fifteenth
Annual, 1929)----------------------------- .10
342 Effect of Turbulence in Wind Tunnel Measure-
ments. Bv H. L. Dryden and A. M. Kuethe.
(Sixteenth Annual, 1930)----- ----------- 10
387 The Vertical Wind Tunnel of the National
Advisory Committee for Aeronautics. By
Carl J. Wenzinger and Thomas A. Harris.
(Seventeenth Annual, 1931)---------------- .10
392 Reduction of Turbulence in Wind Tunnels.
Bv Hugh L. Dryden. (Seventeenth Annual,
1931)-------------------------------------- 10
410 The Theory of Wind-Tunnel Wall Interference.
Theodore Theodorsen. (Eighteenth Annual,
1932) ----------------------------------.. .10
412 The 7 by 10 Foot Wind Tunnel of the National
Advisory Committee for Aeronautics. By
Thomas A. Harris. (Eighteenth Annual, 1932)_- .10
416 The N. A. C. A. Variable-Density Wind Tunnel.
Bv Eastn.an N. Jacol.s. and Ira H. Abbott.
(lK:ightcenth Annual, 1932 ------------------ .05











































;.- ,,.. ., ... , *' *
.' .. I*^ *- .A
P 'A... ..



.. .
:' :'-r "7


...:.: ,: I, .


.. -' ', " !,





















A .l
a... .




,. K# .,
.t- ..- .








:1' .1.


r . A }








. .. ., "
:-: : u"4 ,,


2; I.


'Sk


*1j


; .-1


I ~ A


i.


.5' -' %


-a
S. ~


LI


'"->-*
:'' r .



!. : \
-:



:
.: :









%it
,: ** *







.I. .
.1 -- t


4 '


I





....2.' V n rt Lal111

..... ^ ; *,' :* :* ,''.:. ^' ^ ;< :**:l*'






,* ": .. .. > **"* .** ""* *' "; i**" 'i ~ ~ ~i-^ .."." .. F .: ,
. . .t .. *. ., ...U *:
\t" : 1"' .. . ...'' "" .
f l, ;;... *.. .








I' % E S *" .:i *: : i v : ...j.

..i. .. :. . < *** . ... ;.
:CA









t ** : / :*** -.' '" .*:-' "".' ; ' v : ; ^ - :-'
ii 4 :' ,
."" i 1E "" "-"u I i J a 424 ~








', .* . : I*, jt 'J .
E t .. ...- .:: ... . -

E4." W* #E
... .. . .. . /.. ...


71 .
" .. i ".- .. ... *** :*. .....,; -:.. ..*':-*,*'. "
"*.:...,. '.".. t. ':\ "* : : "... :*. :^ s*":*,.



..; 4 '.: t!E. .'. i .t ...








r ., ....t .. .**". .,. ....., ,.. .. .i:... .,* .: ..: y
Ai 'N':'~










^~ ~ ** 'N*e&H^^^
.... . .. c. .. ,'.N 7 . -: ; ..., 4.>; -
:*-',', .., .' *" .'. *" .* ,, ," .. .. .*,** .; ,, .' ". *.'..; *
.. ....* . ... . .., ". ,. .- - .. .. ,,, ./< ; :il '































-:i .. ' "' .... ^ ;' . 1... ... .
......-. .. .... S . ..
.. 4* - : ... : "- .:*j : *j**.
, . ... . N . .*" ::. .'' .











*. .*. *". ... ., ak
*" '* '" ;

:.1),. .,..
rr4


2 N


M a
*.... .....:. ...,, ; '., N:,, .- ., : 7.4., N.
N.. .: : ."S_ *4.,.. .;.
S. ,. .: 1





... .:.. .. f"N 'j IW 4 4 I
::.. ; a 0 411







ANd
I .*:. .. .. J.'.t.. ...~ ,j.. ,.









. ,. .. A
LILN' r /:... .. .
:. 4" E." ,i 1. .: .. ,, . in S.,' i,
. .. ~e ... ... ....















jf..: K. : ..
A ll y . .. ... : ...
,.,. :' ,o ,. .:. ?' -,; ,..%:

01 .lud ...."! b


UNIVERSITY OF FLORIDA

I III liii111111111ii111111
3 1262 09082 6990


z,