List of reports with prices

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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:
AA00022345:00004

Table of Contents
    Front Cover
        Front Cover 1
        Front Cover 2
    Title Page
        Page i
        Page ii
    Introduction
        Page iii
        Page iv
    Interview
        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
    Back Cover
        Back Cover 1
        Back Cover 2
Full Text









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NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS





LIST OF REPORTS
WITH PRICES



EDITION JUNE 1, 1930


UNITED STATES
GOVERNMENT PRINTING .OFFICE
WASHINGTON: 1930




















Digitized by the Internet Archive
in 2013














http://archive.org/details/I istofreport1930unit










NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


NOTE
This is a list of the Reports of the National Advisory Com-
mnittee for Aeronautics prepared as of June 1, 1928, 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 o:n application to the Sutperin-
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 Intelli-
gence, National Advisory Committee for Aeronautics, Wash-
ington, D. C.
fIII)







































1


















INDEX
Page
Annual reports ------------------------------------- 1
Bibliographies- ------------------------------------ 1
Technical reports- --------------------------------- 3
Aerodynamics --------------------------------- 3
Airfoils and wing sections----------------------- 4
Airplanes-Full-scale experiments ----------------- 7
Airplanes-Model experiments------------------ 9
Airships ------------------------------------- 11
Engines and accessories------------------------- 12
Fuels ---------------------------------------- 20
Gases ---------------------------------------21
Helicopters----------------------------------- 21
Instruments---------------------------------- 21
Materials ------------------------------------24
Meteorology---------------------------------- 26
Miscellaneous -------------------------------- 27
Nomenclature- --------------------------------27
Parachutes ----------------------------------28
Propellers- -----------------------------------28
Seaplanes ------------------------------------31
Stability and control--------------------------- 31
Strength of construction ------------------------ 32
Wind tunnels and laboratories -------------------34
(v)











NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


ANNUAL REPORTS


First -------
Second 1- - -
Third-------
Fourth 1 ....
Fifth '
Sixth -------
Seventh 1 .
Eighth 1 ....
Ninth ------,
Tenth' ------
Eleventh .
Twelfth
Thirteenth_ -_ _
Fourteenth ---


Year

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


With
With
With
W it. h
With
With
With
With
With
With
With
With
With
With


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


Nos.
N,)s.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.
Nos.


Price


1-7------------
8-12-----------
13-23 ----- $1.50
24-50-----
51-82-----
83-110.- ------
111-132_...---. -
133-158 ------_
159-185---------
186-209_ .......
210-232____ _
233-256---------
257-282 -_- 1.25
283-308--- 1.25


1 Out of print. Available for reference or loan in the officeof Aeronautical Intel-
ligence, National Advisory Committee for Aeronautics, Washington, D. C., and
in the libraries of large cities.

BIBLIOGRAPHIES


Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography
Bibliography


Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics
Aeronautics


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


---------- $2.00
--- ------ .75
---------- .35
---------- .25
---------- .25
---------- .25
---------- .50
---------- .20
-.-------- 35
- .- --.-. -- 50











TECHNICAL REPORTS


AERODYNAMICS

No. Title Price

1 12 Experimental Researches on the Resistance of
Air. By L. Marchis. (Second Annual, 1916) ------
20 Aerodynamic Coefficients and Transformation
Tables. By Joseph S. Ames. (Third Annual,
1917)------------------------------------ $0.05
3 78 The Limiting Velocity in Falling from a Great
Height. By Edwin Bidwell Wilson. (Fifth
Annual; 1919)----------------------------------
3 79 Bomh Trajectories. By Edwin Bidwell Wilson.
(Fifth Annual, 1919)----------------------------
3 83 Wind Tunnel Studies in Aerodynamic Phe-
nomena at High Speed. By F. W. Caldwell
and E. N. Fales. (Sixth Annual, 1920)------------
3 97 General Theory of the Steady Motion of an
Airplane. Byv George de Bothezat. (Sixth
Annual, 1920)----------------------------------
3114 Some New Aerodynamical Relations. By Max
M. Munk. (Seventh Annual, 1921)-------- -----
116 Applications of Modern Hydrodynamics to
Aeronautics. By L. Prandtl. (Seventh An-
nual, 1921)------------------------------- 10
139 Influence of Model Surface and Air Flow Tex-
ture on Resistance of Aerodynamic Bodies.
By A. F. Zahm. (Eighth Annual, 1922)----- .05
144 The Decay of a Simple Eddy. By H. Bateman.
(Eighth Annual, 1922) --------------------- .05
, 151 General Biplane Theory. By Max M. Munk.
(Eighth Annual, 1922)---------------------
185 The Resistance of Spheres in Wind Tunnels
and in Air. By David L. Bacon and Elliott
G. Reid. (Ninth Annual, 1923)------------ 10
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash-
ington, D. C., 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.
(8)










AERODYNAMICS-Continued

No. Title Price

3 197 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)-----------------
213 A Resurn6m of the Advances in Theoretical
Aeronautics MaIde bv Max M. Munk. By
Joseph S. Ames. (Eleventh Annual, 1925) -.-- $0. 15
3 247 Pressure of Air on Coming to Rest from Various !
Speeds. By A. F. Zahm. (Twelfth Annual, 1926)_! ------
3 253 Flow and Drag Formulas for Simple Quadries.
By A. F. Zahm. (Twelfth Annual, 1927)---- ------
287 Theories of Flow Similitude. By A. F. Zahm.
( Thirteenth Annual, 1927)----------------- .05
289 Forces on lE.lliptic Cylinders in Uniform Air
Stream. By A. F. Zahm, R. H. Smith, and
F. A. Luiden. (Fourteenth Annual, 1928)--_ .05
311 Aerodynamic The,'rv and Test of Strut
Formis-1. By R. H. Smith. (Fifteenth
Annual, 1I129) ---------------------------- 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,
S1929)------------------------------- .20

AIRFOILS AND WING SECTIONS

4 18 Aerofoils and Aerofoil Strucetural Combinations.
By Lieut. Col. Edgar S. Gorrell and Maj.
H. S. Martin. (Third Annual, 1917)-------------
a 28 An Introduction to the Study of the Laws of Air
Resistance of Aerofoils. By George de
Botlhezat. (Fourth Annual, 191)--------------
S Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.
I Not issue',l as a separate report. The annual volume containing this report is
still available






5

AIRFOILS AND WING SECTIONS-Continued

No. Title Price

3 75 The Aerodynamic Properties of Thick Acrofoil.,
Suitable for Internal Bracing. By F. H.
Norton. (Fifth Annual, 1919. ---- -------------
3 77 The Parker Variable Camber Wing. Bv H. F.
Parker. (Fifth Annual, 1919)--------- -- ------
393 Aerodynamic Characteristics of Airfoils. By
National Advisory Committee for Avro-
nautics. (Sixth Annual, 1920)------------- ------
3 111 The Variation of Airfoil Lift and Drag Coeffi-
cients with Changes in Size alnd Speed. Br
W S. Diehl. (Sevenith Annual, 1921) ------------
3 121 The Minimum Induced Drag of Airfoils. By
Max MN. Munk. (Seventh Annual, 1921)----------
124 Aerodynamic Characteristics of Airfoils-II.
By the National Advisory Committee for
Aeronautics. (Seventh Annual, 1921) ------ l). 1)
3 142 General Theory of Thin Wing Sections. By
Max M. Munk. (Eighth Annual, 1922 --v.- ------
3 150 Pressure Distribution over Thick Aerofoils-
Model Tests. Br F. H. Norton and D. L.
Bacon. i Eighth Annual, 1922.)-----------------
3 152 The Aerodynamic Properties of Thick Aero-
foils-11. By F. H. Norton and D. L.
Bacon. (Eighth Annual, 1922)-------------
3 169 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 the National Advisory Committee for
Aeronautics. (Ninth Annual, 1923) ---------------
191 Elements of the Wing Section Theory atnd 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)------------ 10
. 201 The Effects of Shielding thle Tips of Airfoils.
By Elliott G. Reid. (Tenlth Annual, 1924) ------
3 207 Aerodynamic Characteristics of Airfoils at Higlh
Speeds. By L. J. Briggs, G. F. Hull, and
H. L. Dryden. (Tenth Annual, 1924) -------------
3 Out of print. Available as a separate report for reference or loan in thie police
-of Aeronautical Intelligence, Nation:l Ad vi-'ory Committee for aeronautics .









AIRFOILS AND WING SECTIONS-Continued

No. Title Price

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)----------- $0. 10
S221 Model Tests with a Systematic Series of 27
Wing Sections at Full Reynolds Number.
By Max M. Munk and Eilton W. Miller.
iEleventh Annual, 1925)------------------------
229 Pressure Distribution Over Thick, Tapered Air- I
foils, N. A. C. A. 81, U. S. A. 27 C Modified I
and U. S. A. 35. By Elliott G. Reid.
(Eleventh Annual, 1925)------------------- 10
2233 The Aerodynamic Characteristics of Seven Fre-
quently Used Wing Sections at Full Reynolds
Number. By Max M. Munk and Elton W.
Miller. .Twelfth Annual, 1926)
244 Aerodynamic Characteristics of Airfoils-IV.
By National Advisory Committee for Aero-
nautics. Twelfth Aninual, 1926)----------- ..20
255 Pressure Distribution Over Airfoils at High
Speeds. By L. J. Briggs and H. L. Dryden.
(Twelfth Annual, 1927) -------------------- 15
267 Drag of Wings with End Plates. By Paul E.
Henimkc. (Thirteenth Annual, 1927) --------- 10
271 Pressure Distribution Tests on PW-9 Wing
Models Showing Effects of Biplane Interfer-
ence. By A. J. Fairbanks. (Thirteenth
Anal, 1927)---------------------------- 10
278 Lift, Drag, and Elevator Hinge Moments of
flandlev-Page Control Surfaces. By R. H.
Smith. (Tlirteenth Annual, 1927)---------- 10
285 A St.iudy of WVing Flutter. By A. F. Zahm and
R. M. Bear. (Fourteenth Annual, 1928)...- 15
286 Aerodynamic Chlaracteristics of Airfoils-V.
By National Advisory Committee for Aero-
nautics. (Fourteentli Annual, 1928)-------- 25
288 Pressure Distribution Over a Rectangular Mono-
6lane Winig Model up to 90 Angle of Attack.
'I Montgomery Knight and Oscar Loeser, jr.
(Fourtcenth Annual, 1928)----------------- 10
U Out of print. Availaible as a separate report for reference or loan in the Office
of Aeronautical riftelligence, Ns:ational Adlvisory Cominu ltee for Aeronautics.








AIRFOILS AND WING SECTIONS-Continued
No. Title Price

309 Joint Report on Standardization Tests on
N. P. L. R. A. F. 15 Airfoil Model. By
Walter S. Diehl. (Fifteenth Annual, 1929)-- $0. 10
312 The Prediction of Airfoil Characteristics. By
SGeorge J. Higgins. (Fifteenth Annual, 1929,) 10
315 Aerodynamic Characteristics of Airfoils-VI.
I By the National Advisory Committee for
SAeronautics. (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
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. 11. 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
and W. G. Brown. (Eighth Annual, 1922) --____
A Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.








8

AIRPLANES-FULL-SCALE EXPERIMENTS-Continued


No.

3 154

3 155

162

1i63


167


3170

173


174

3 1.92

3 193


194

203

219

228


Price


Title

A Study of Taking Off and Landing an Airplane.
B1. T. Carroll. (Eighth Annual, 1922) - -
A Study- of Airplane Maneuvers with Special
Reference to Angular Velocities. B- H. J.
E. Reid. (Eiglhth Annual, 1922.)--------
Complete Study of tlhe Longitudinal Oscillation
of a VE-7 Airplane. By F. H. Norton and
W. G. Brown. (Nintht Annual, 1923) -----
''The Vert(ical, Longit iudin(iiail, a!l(d Lateral Accelera-
tions Experienced by an S-5A Airplane while
MIaumtivering. Bv F. 11. Norton and T.
Carroll. (Ninth Annual, 1923)-----------
The Measurement of the Damping in Roll on a
JN4H in Fliglht. By F. H. Norton. (Ninth
A.-n'ual, 1923)---------------------------
A Sttiudv of Longitudinal Dynamic Stability in
Flight.. By1v F. I1. Norton. (Ninth Annual,
1923 ---------------------------------
Reliable Fo'rmniihe for Estimating Airplane
Performance and the Effects of the Changes in
Weight, Wing Area, or Power. By Walter
S. Diehl. (Ninth Annual, 1923)------------
Thle Small Angular Oscillations of Airplanes in
Steady F'liglit. By F. H. Norton. (Ninth
Annual, 1923)--------------------------
(Charts for Graphical Estimation of AirpLane
Performance. By Walter S. Diehl. (Tenth
Annual, 1924) .--------.-------------------
Pressure Distribution Over the Wings of an
MB-3 Airplane in Fliglht. By F. 11. Norton.
(Tenth Annual, 1924)-- -- -- ---- -
Investigation (of Slip Stream Velocity. By J. \V.
('rowley, jr. (Ttl Annual, 1924)----
Accelerations in Flight. By J. 11. Doolittle.
(Tenth Annual, 1924) ----- --- -
Some Aspects of the Comparison of Model and
Full-scale Tests. By% 1). W. Taylor. (Elev-
,ntlh Annual, 1925)----------------------
A Stldy of tihe Effect of L I)iving Start on Air-
plae Speed. By Walte(r S. DI)iehl. (Eleventh
A1\11 l], 1925) ------------- -- --- --


.05

.05


.10

.10


.05


a (uL of prinil. A iilatble as i seliinile re:iit for reference or loanl in the Oflice
of Aermiiiiici..al iiieliheince, Naliiimiitl .\Ivisury (C'omniittee for Aeronautics.


$). 05


.05

.05








AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

No. Title Price

234 Three Methods of Calculating Range and En-
durance of Airplanes. By Walter S. Diehl.
(Twelfth Annual, 1926) ------------------- $0. 10
238 The Effect of Flight Path Inclination on Airplane
Velocity. By Walter S. Diehl. (Twelfth
Annual, 1926)---------------------------- .05
3249 A Comparison of the Take-off and Landing
Characteristics of a Number of Service Air-
planes. By Thomas Carroll. (Twelfth An-
nual, 1927)-------------------------------
257 Pressure Distribution Over a Wing and Tail
Rib of a VE-7 and of a TS Airplane in Flight.
By J. WV. Crowley, jr. (Thirteenth Annual,
1927)------------------------------------- 15
265 A Full-Scale Investigation of Ground Effect.
By Elliott G. Reid. (Thirteenth Annual,
1927)------------------------------------ .05
297 The Reducation of Observed Airplane Perform-
ance to Standard Conditions. By Walter S.
Diehl. (Fourteenth Annual, 192S) ---------- 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

AIRPLANES-MODEL EXPERIMENTS

3 74 Construction of Models for Tests in Wind Tun-
nels. By F. H. Norton. (Fifth Annual, 1919).------
3119 The Pressure Distribution Over the Horizontal
Tail Surfaces of an Airplane-II. By F. H.
Norton and D. L. Bacon. (Seventh Annual,
1921)------------- -- ------ ----------
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, Natii.al Advisory Committee for Aeronautics.








10

AIRPLANES-MODEL EXP E RIMENTS-Continued

No. Title Price

3 122 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)-----------------------------
3 133 The Tail Plane. By Max M. Munk. (Eighth
Annual, 1922) -------------------------------_
136 Damping Coefficients Due to Tail Surfaces in Air-
craft. By Lynn Chu. (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
140 Lift and Drag Effects on Wing Tip-rake. By
A. F. Zahm, R. M. Bear, and G. C. Hill.
(Eighth Annual, 1922)--------------------| .05
219 Some Aspects of the Comparison of Model and
Full-scale Tests. By D. W. Taylor. (Elev-
enth Annual, 1925)------------------------ 10
S225 The Air Forces on a Model of the Sperry Mes-
senger Airplane Without Propeller. By Max
M. Munk and Walter S. Diehl. (Eleventh
Annual, 1925)---------------------------------
236 Tests on Airplane Fuselages, 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, 1927)---------------------------- 10
256 The Air Forces on a Systematic Series of Biplane
and Triplane Cellule Models. By Max M.
Munk. (Twelfth Annual, 1927)------------ 15
260 The Effect of a Flap and Ailerons on the N. A.
C. A.-M6 Airfoil Section. By George J. Hig-
gins 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)---------------------i .05
2 269 Air Force Tests of Sperry Messenger Model
with Six Sets of Wings. By James M. Shoe-
maker. (Thirteenth Annual, 1927)---------_
1 Out of print as a separate report. The annual volume containing this report is
still available.
I 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

273 Wind Tunnel Tests on Autorotation and the
"Flat Spin." By Montgomery Knight.
(Thirteenth Annual, 1927)------------------ $0. 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
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)----------------------------- 15

AIRSHIPS

115 Bending Moments, Envelope and Cable Stresses
in Nonrigid Airships. By C. P. Burgess.
(Seventh Annual, 1921) --------------------$0. 05
117 The Drag of Zeppelin Airships. By Max M.
Munk. (Seventh Annual, 1921) ------------ 05
138 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)---------------------------- 05
164 The Inertia Coefficients of an Airship in a Fric-
tionless Fluid. By H. Bateman. (Ninth
Annual, 1923)--------------------------- .05
184 The Aerodynamic Forces on Airship Hulls. By
Max M. Munk. (Ninth Annual, 1923)------ 10
204 Forces on Airships in Gusts. By C. P. Burgess.
(Tenth Annual, 1924) ---------------------- .05
208 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) --------_------- 10
210 Inertia Factors of Ellipsoids for Use in Airship
Design. By L. B. Tuckerman. (Eleventh
Annual, 1925)---------------------------- .05


101220-30----2










AIRSHIPS-Continued

No. Title Price

211 Water Model Tests for Semirigid Airships. By
L. B. Tuckerman. (Eleventh Annual, 1925) SO $0. 05
212 Stability Equations fur Airship Hulls. By A. F.
Zahmni. ('Eleventh Annual, 1925)----.------- 05
215 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)------------------- 15
223 Pressure Distribution on the C-7 Airship. By
J. W. Crowley, jr., and S. J. DeFrance.
(Eleventh Annual, 1925)------------------ 15
291 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) 10
318 Speed and Deceleration Trials of U. S. S. Los
Angeles, September, 1927. By S. J. DeFrance
and C. P. Burgess. (Fifteenth Annual, 1929)_ 10
324 Flight Tests on U. S. S. Los Angeles. Part I.
Full-scale Pressure Distribution Investigation.
By S. J. DeFrance. (Fifteenth Annual, 1929)_ 15
325 Flighit Tests on U. S. S. Los Angeles. Part, II.
Stress and Strength Determination. By C.
P. Burgess. (Fifteenth Annual, 1929) ------- 15
333 Full-scale Turning Characteristics of the U. S. S.
Los Angeles. By F. L. Thompson. (Fifteenth
Annual, 1929) ------------------------- 10

ENGINES AND ACCESSORIES

1 7 Thermodvynamic 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
110 Mufflers for Aeronautic Engine. By Prof. H.
Diedericlhs and Prof. G. B. ITU)pton. (Second
Annual, 1916).-------------------------------
i Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash.
ington, D. C., and in the libraries of large cities.










ENGINES AND ACCESSORIES-Continued

No. Title Price

1 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 their
Subcommittee on Power Plants. (Third
I Annual, 1917) ----------------- --------------
Part 1. Performance of Aeronautic Engines
at High Altitudes.
Part 2. Radiator Design.
S Part 3. Spark Plugs.
3 24 Air Flow Through Poppet Valves. By G. W.
Lewis and E. M. Nutting. (Fourth Annual,
1918)-----------------------------------------
3 43 S-nopsis of Aeronautic Radiator Investigations
Sfor 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 Rati). 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 H14. C. Dickinson,
W. S. James, and G. V. Anderson.
Part 4. Influence of Water Injection on En-
gine Performance. By V. W. Brinkerhoff.
3 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) ---------------------------- -----
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash-
ington, D. C., 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 separatee report. The annual volume containing this report
is still available.










ENGINES AND ACCESSORIES-Continued

No. Title Price

3 49 Mctering Cl'haractcristic.- o-f Carburetors. By
P. S. Tice. kFuurthl Annual, 1918)---------------
3 51 Spark-plIug Defect.-l and Tests. (Fifth Annual,
1919 1- ------------------- --
Part 1. Ca.ises 4f Failure of Spark Plugs.
By F. B. Silsbee.
Part 2. Gas Leakage in Spark Plugs. By
L. Sawver.
Part 3. Mcthilds fr Tests of Spark Plugs.
B If. C. Dickinsin.
3 52 Temperatures in Spark Plugs Having Steel and
Brass Shells. Bx- C. S. Cragoe. (Fifth Annual,
1919)----------- ---- -- - ---------
8 53 Prupertics and Preparation of Ceramic Insula- ,
tors for Spark Plugs. ;Fifth Annual, 1919)---------
Part 1. Methods of Measuring Resistance
of Insnzlatrs at High Temperatures.
B% F. B. Silsbee andl R. K. Honaman.
Part 2. Electrical Resistance of Various In-
sulating Materials at High Temperatures.
By RI. K. Honamnan and E. L. Fonseca.
Part 3. Preparation and Composition of
Ceramic Bodies for Spark-plug Insula-
tors. By A. V. Bleininger.
Part 4. Ceiments fur Spark-plug Electrodes.
By 11. F. Staley.
[3 54 Effect of Temperature and Pressure on the
t Sparking Voltage. B\ F. B. Silsbee and L.
B. Loeb. i Fifth Annual, 1919)--- ------------
3 55 Investigation of the lMuffling Problem for Air-
plane Engines. By G. B. U'pton and V. R.
Gage. (Fifth Annual, 1919)---------------------
3 56 Heat Energy- of Various Ignition Sparks. (Fifth
Annual, 1919)--------------------------------
Part 1. Methold f 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.
I 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. Title Price

3 57 The Subsidiary Gap as a Means for Improving
Ignition. By W. S. Gorton. (Fifth Annual,
1919)---------------------------------------
3 r8 Characteristics of High-tension Magnetos.
(Fifth Annual, 1919)----------------------------
Part 1. Cycle of Operation of Jump-spark
Ignition Systems. By I. B. Silsbee.
Part 2. Transformation Ratio and Coupling
in High-tension Magnetos. By L. B.
Silsbee.
9 59 General Analysis of Airplane Radiator Problems.
By H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt. (jifth Annual, 1919)--------------
3 60 General Discussion of Test Methods for Radi-
ators. By H. C. Dickinson, W. S. James, and
W. B. Brown. (Fifth Annual, 1919. _)-----------
3 61 Head Resistance Due to Radiators. (I'ifth
Annual, 1919)-------------------------------
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.
3 62 Effect of Altitude on Radiator Performance.
By W. S. James and S. R. Parsons. (Fifth
Annual, 1919)---------------------------------
3 63 Results of Tests on Radiators for Aircraft En-
gines. (Fifth Annual, 1919)-----------------
Part 1. Heat Dissipation of Radiators. By
H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt.
Part 2. Water Flow through Radiator
I Cores. By W. S. James.
3 86 Properties of Special Types of Radiators. By
SS. R. Parsons. (Sixth Annual, 1920)-------
3 87 Effects of Nature of Cooling Surface on Radiator
Performance. Bv S. R. Parsons and R. V.
Kleinschmidt. (Sixth Annual, 1920)----------
SOut of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.








16

ENGINES AND ACCESSORIES-Continued

No. Title Price

3 S8" Pressure Drop in Radiator Air Tubes. By S. R.
Parsons. (Sixth Annual, 1920)-------------
'101 The Calculated Performance of Airplanes
Equipped with Supercharging Engines. By
E. C. Kemble. (Sixth Annual, 1920) .-------......
s 102 Performance of a Liberty 12 Airplane Engine.
By S. W. Sparrow and H. S. White. (Sixth
Annual, 1920)-..------------------------
S103 Performance of a 300-horsepower Hispano-
Suiza Airplane Engine. By S. W. Sparrow
and H. S. White. (Sixth Annual, 1920)------------
3 106 Turbulence in the Air Tubes of Radiators for
Aircraft Engines. By S. R. Parsons. (Sixth
Annual, 1920) ---------------------- ------
3 108 Some Factors of Airplane Engine Performance.
By Victor R. Gage. (Sixth Annual, 1920) ----.---
3 123 Simplified Theory of the Magneto. By F. B.
Silsbee. (Seventh Annual, 1921)--..---------- --
3 134 Performance of Maybach 300-horscpower Air-
plane Engine. By S. W. Sparrow. (Eighth
Annual, 1922)---------------------
135 Performance of B. M. W. 185-horsepower Air-
plane Engine. By S. W. Sparrow. (Eighth
Annual, 1922)-- -----------------------$0.05
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) ----- -------------
S159 Jet Propulsion for Airplanes. By Edgar Buck-
inglihamin. (Ninth Annual, 1923)----------------.
S171 Engine Performance and the Determination of
Absolute Ceiling. By Walter S. Dichl.
(Ninth Annual, 1923) ------------------------
1179 The Effect of Electrode Temperature on the
Sparking Voltage of Short Spark Gaps. By
F. B. Silsbce. (Ninthi Annual. 1923)------
S1S7 Flame Speed and Spark Initensity. By D. NW.
Randolph and F. B. Silsbee. (Tentlih Annual,
1924) ... .. ... .. ... .... .. ... ... .. ... . .
uiu 'itf iprint. Available as a separate report for refererrwe or Io:in in lt lie )ffice of
.\(r,,n:i]Hical Intelligence, National Advisory Conminiltee fi"r Aeronrutics.










ENGINES AND ACCESSORIES-Continued

No. Title Price

3 189 Relation of Fuel-air Ratio to Engine Perform-
ance. By Stanwood W. Sparrow. (Tenth
Annual, 1924).--------------------- - --...-.
3 190 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
3205 The Effect of Changes in Compression Ratio
upon Engine Performance. By Stanwood
W. Sparrow. (Tenth Annual, 1924)-------------
3 222 Spray Penetration with a Simple Fuel Injection
Nozzle. By Harold E. Miller and Edward G.
Beardsley. (Eleventh Annual, 1925)--------
3 224 An Investigation of the Coefficient of Discharge
of Liquids Through Small Round Orifices.
By W. F. Joachim. (Eleventh Annual, 1925) ------
233 Description and Laboratory Tests of a Roots
Type Aircraft Engine Supercharger. By
Marsden Ware. (Eleventh Annual, 1925) --.. -- 10
3 239 Power Output and Air Requirements of a Two-
stroke Cycle Engine for Aeronautical Use.
By 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 Corn- I
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, 1927)------------------i 10
8 Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.








is

ENGINES AND ACCESSORIES-Continued

No. Title I Price

258 Some Factors Affecting the Reproducibility of
Penetration and the Cut-off of Oil Sprays for
Fuel Injection Engines. By E. G. Beardsley.
(Thirteenth Annual, 1927)--- -------- $0. 05
2 261 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 WV. Gardiner and Elliott G. Reid.
(Thirteenth Annual, 1927)..--..-------- 10
2268 Factors in the Design of Centrifugal Type In-
jection Valves for Oil Engines. By W. F.
Joachim and E. G. Beardsley. (Thirteenth
Annual, 1927)--------------------
272 The Relative Performance Obtained with Several
Methods of Control of an Overcompressed
Engine Using Gasoline. By Arthur W. Gar-
diner and William E. Whedon. (Thirteenth
Annual, 1927)---------------------------- .10
2 274 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)..- -------- --- ---
2276 Com bbustion Time in the Engine Cylinder and
Its Effect on Engine Performance. By
Charles F. Marvin, jr. (Thirteenth Annual,
1927) ----------------- .--------
277 The Comparative Performance of ain Aviation
Engine at Normal and 11igl Inlet Air Tem-
peratures. By Arthur W. Gardiner and Oscar
W. Schey. (Thirteenth Annual, 1927)------- .10
2280 The Gaseous Explosive Reaction-The Effect of
Inert Gases. By F. W. Stevens. (Thirteenth
Annual, 1927)- --- ----- ---------
I Out of print as a separate report. The annual volume containing this report
is still available.










ENGINES AND ACCESSORIES-Continued

No. Title Price

281 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)------ $0. 10
282 The Performance of Several Combustion Cham-
bers Designed for Aircraft Oil Engines. By
William F. Joachim and Carlton Kemper.
(Thirteenth Annual, 1927)--------------- 10
283 A Preliminary Investigation of Supercharging an
Air-cooled Engine in Flight. By Marsden
Ware and Oscar WV. Scliev. (Fourteenth
Annual, 1928)---------------------------- 10
284 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
294 The Measurement of Maximum Cylinder Pres-
sures. By Chester W. Hicks. (Fourteenth
SAnnual, 1928)---------------------------- .15
295 The Variation in Engine Power with Altitude
SDetermined from Measurements with a Hub
Dynamometer. By W. D. Gove. (Four-
teenth Annual, 1928)---------------------- .10
303 An Investigation of thle 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. Schev 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-1I. By Fred E. Weick. (Fifteenth
Annual, 1929)----------------------- .15
314 Drag and Cooling with Various Forms of Cowl-
ing for a "Whirlwind" Radial Air-Cooled
SEngine-11. 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








20

ENGINES AND ACCESSORIES-Continued

No. Title Price

330 Experimental and Analytical Determination of
the Motion of Hydraulically Operated Valve
Sterns in Oil Engine Injection Systems. By
A. G. Delailes and A. M. Rothrock. (Fifteenth
Annual, 1929)---------------------------- $0. 10
332 The Effect of Cowling on Cylinder Tempera-
Itures and Performance of a Wright J-5 En-
gine. Bv Oscar W. Schey and Arnold E.
Bierman. (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

FUELS

S42 A New Process for t' e Production of Aircraft-
engine Fuels. By Auguste Jean Paris, jr., and
W. Francklyn Paris. (Fourth Annual, 1918) )-------
347 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.
89 Comparison of Alcogas Akviation Fuel with
Export Aviation Gasoline. By V. R. Gage,
S. W. Sparrow, and D. R. Harper. (Sixth
Annual, 1920)---------------------------- $0.05
90 Comparison of hIector Fuel with Export Aviation
Gasoline. Byv 11. C. Dickinson, V. R. Gage,
and S. \V. Sparrow. (Sixth Annual, 1920) -...-- 05
232 Fuels for Ii igl-compression Engines. By Stan-
A ood W. Sparrow. (Eleventh Annual, 1925)_ 10
305 The Gaseous Explosive Rteaction-A Study of
the Kinetics (of (Composite Fuels. By F. W.
Stcv\ens. (Fourteenthl Annual, 1928) ---------. 15
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Aidvisory Committee for Aeronautics.








21

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,and P. A. Pearsall. (Fifteenth
Annual, 1929)---------------------------- $0. 101
337 The Gaseous Explosive Reaction at Constant
Pressure-The Reaction Order and Reaction
Rate. By F. W. Stevens. (Sixteenth Annual,
1930)------------------------------------ 10

GASES

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

HELICOPTERS

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

INSTRUMENTS

S2 Investigation of Pitot Tubes. (First Annual,
1915)-----------------------------------------
Part 1. The Pitot Tube and Other Ane-
mometers for Airplanes. By WV. H.
Herschel.
Part 2. The Theory of the Pitot and Ven-
turi Tubes. By E. Buckingham.
1 8 General Specifications Covering lRequiretments
of Aeronautic Instruments. By the National
Advisory Committee for Aeronautics. (Sec-
ond Annual, 1916)------------------------------
SOut. of print. Annual volume available for reference or loan in tlie Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash-
ington, D. C., and in the libraries of large cities.
a Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










INSTRLUMENTS-Continued


Tit le


Development o(f Air Speed Nozzles. By A. F.
Zahm. i Fourth Annual, 1918)------
The Airplane Tensiomieter. By L. J. Larson.
tFourth Annual, 191S)- --- - -
Calculation of Low Pressure Indicator Dia-
grains. By E. C. Keinble. (Fourth Annual,
191Si --------------- --------------
Comparison of U. S. and British Standard
Pitot-static Tubes. Bv A. F. Zahm and R. H.
.Snith. (Fifth Annual, 1919)---- ----
The Efficiency of Small Bearings in Instruments
of the Type IUsed in Aircraft. By F. H.
Norton. ,'Sixth Annual, 1920) _
ACCIeleration in Flight. By F. H. Norton and
L. T. Alien. (.Sixth Annual, 1920)----------
Accelerometer Design. Bv F. 11. Norton and
E(dwarl P. Warner. (Sixth Annual, 1920) ---
A High-speed Engine Pressure Indicator of the
Balanced Diaphragm Typ)e. By IH. C. Dick-
inson and F. B. Newell. (.Sixth Annual, 1920)_
The Altitude Effect on Air Speed Indicators.
By M. D. HIersey, F. L. Hunt, and 11. N.
l'aton. (Sixth Annual, 1920)--------------
A.ero1,iittict Instruments: Section 1--General
Classification of Instruments and Problems,
Includilng Bibliographly. By Bureau of
Standards. (.Seventh annuall 192 1) ----
Aeronta'utic Instr6i uments: Section II--Altitude
Instrumetnts. Bv Bureau of Standards.
,Seventh Annual. 1921)-------- -------
Part 1. A.ltimweters and Barographs.
Part 2. Precision Altimeter Design.
Part 3. Statiscopes and Rate-of-climb In-
dicators.
Part. 4. Aerographs and Strut Thermome-
t ( rs.


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


SPrice


100

107

3 110


125


121


$0. 10

05


.05


.05


.05

.10

05

.05


.05

. 15








INSTRUMENTS-Continued

No. Title Price

127 Aeronautic Instrruments: Secti,_t III-Aircraft
Spcel Instruments. B' Bureau of St..ald-
ards. (Seventh Annual. 1921'------------ 0. 10
Part 1. Air Speed Indicat,,r,.
Part 2. Testing of Air SlI)eed Meter-.
Part 3. Principles of Gr,,itI--pleed Il-trui-
ments.
12S Aeronautic Inistrumenets: Sectio, IV- Direc-
lion Instrunmeits. By Bureau 4f Standalrd,.
(Seventh Annual, 1921, -------------------- .15
Part 1. Iniclinometers and Banking iJidi-
cators.
Part 2. Thile Testing aild Use of Magnetic
Compasses for Airplanes.-
Part 3. Aircraft Comp:ases-De.cripti, ,i
and Classification.
Part 4. Turn Indicators.
129 Aeronautic Instrumients: Section V-P\,wer-
plant Instruments. By Bureau ,if Stanid-
ards. (Seventh Annual, 1921 1 -------------- 15
Part 1. Airplane Tachometers.
Part 2. Testing of Airplane Tacho ometer-s.
Part 3. Thermometers for Aircraft Engitnes..
Part 4. Air-pressure a.nd( Oil-pressure
Gages.
Part 5. Gasoline-depth Gages and Flow
Meters for Aircraft.
130 Aeronautic Instruments: Section VI-Oxygen
Instruments. By Bureau of Standards.
(Seventh Annual, 1921) -------------------- 10
131 Aeronautic Instruments: Section VII-Aerial
Navigation Instruments. B- Bureauti of
Standards. iSeventh Annual. 19211---- | .10
132 Aeronautic Instruments: Section VIII-Recent
Developments and Outstanding Problems.
By Bureau of Standards. (Seventh Anlnual.
1921) ------------------..------------------ .05
3156 The Altitude Effect of Air Speed Indicators-II.
By H. N. Eaton and W. A. McNair. 'Eighth
Annual, 1922) .---------------------------------
3 Out of print. Available as a separate report for reference or loan in the Uloffice
of Aeronautical Intelligence. National Advisory Committee for Aernaautics.








24

INSTRUMENTS-Conrinued

No. Title Price

160 An Airship Slide Rule. By E. R. Weaver and
S. F. Pickering. (Ninth Annual. 1923)------ $0.05
165 Diaplhragmins for Aeronautic Instruments. By
M. D. Hlersey. i Ninth Annual, 19231)------- -----
166 The Aerodynamic Plane Table. By A. F.
Zahnt. (Ninth Annual, 1923- --------------- .05
S176 A Constant-pressure Bomb. By F. W. Stevens. I
(Ninth Annual, 1923'----------------------------
198 Astrionmical Methods in Aerial Navigation.
By K. Hilding Beij. iTenth Annual. 1924)-- .15
199 Interference Tests on n'u N. A. C. A. Pitot Tube.
By Elliott G. Reid. (Tenth Annual, 1924) --- .05
206 Ninmmetallic Di:plhragms for Instruments. By
H. N. Eatonm and C. T. Buckinghamn. iTenth
Annual. 1924 ------------------------ .10
26-4 1)ifferential Pressures on a Pit't-Venturi and a
Pitwit-static Notzzle Over 360 Pitch aind Yaw.
By R. M. Bear. ,Thirteenth Annual. 1927)-- .05
270 lThe Mea,,rement( of Pressure Through Tubes
in Pressure Distribt tion Tests. Bv Paul E.
H.Wnke. (Thirteenthi Annual,. 1927)__--------- 10
299 Investigation of Da'ping Liquidls for Aircraft
Instruments. Bv G. H. Keulegan. (Four-
trenth Annual, 192S)-----------------------. 10
310 Pressure Element o(f Constant Logarithmic
Stifftriess for Termperature Cimipensated Alti-
meter. Bv W. G. lBrtnbl)acher and F.
Cordertr. iFifteenth Annual. 19291 --------- 10
:321 TIhe Measuremenut oif Fluectuations of Air Speed
br tilhe Hot Wire Ane.-mometter. By H. L.
Drvden alnd A. M!. Kent lhe. [Fifteenth An-
nual, 1929)--- ----------------------------... 15

MATERIALS

15 RhelLtive Worth of Tmpl)rovemenets on Fabrics.
Bv tlhe (oodear Tire & Rubber Co.
(First Annual, 1915)---------------------------
: Out of prinil Anniual oluimen available fur refe-ence or loan in the Office or
Aeronautical Intelligence, National Ailvisury Commiiiittee for Aeronaulics, Wash-
inglon, I). C., nnil in the libraries of large cities.
SOiut of print. Available as a seijeparale report for reference or loan in the Office
of Aeronautical Irintelligew e. Nat ional Advisory ConiuiLtLee for Aeronaulics.










MATERIALS-Continued

No. Title Price

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, 19171-----------------------
Part. 1. The Stretching of the Fabric and
I the Shape of the Envelope. By Rudolf
Haas.
Part 2. The Deformation of the Envelope
of the Siemens-Schuckert Airships.
By Alexander Dietzius.
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. Dorsev.
(Fourth Annual, 1918,)---------------------------
3 34 Aluminum and Its Light Alloys. By Paul D.
Merica. (Fourth Annual, 1918)----------------
3 36 The Structure of Airplane Fabrics. By E.
Dean Walen. tFourth Annual, 1918)-------------
3 37 Fabric Fastenings. By E. Dean Walen and R.
T. Fisher. (Fourth Annual, 1918)----------------
3 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.
1 Out oT print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash.
ington, D. C., 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.








26

MATERIALS-Continued

No. Title Price

3 65 The Kiln Drying of Woods for Airplanes. By
Harry D. Tieman. (Fifth Annual, 1919)__
3 66 Glues f'sed in Airplane Parts. Bv S. W. Allen
and T. R. Truax. (Fifth Annual, 1919)----------
3 67 Supp)lies and Production of Aircraft Woods.
By W. N. Sparhawk. ;Fifth Annual, 1919)---
3 68 The Effect of Kiln Drying on the Strength of
Airplane Woods. By T. R. C. Wilson. (Fifth
Annual, 1919)----------------------- ----

3 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)
3145 Internal Stresses in Laminated Construction.
By A. L. Heini, A. C. Knauss, and Louis Seut-
ter. (Eighth Annual, 1922)---------------------
248 Tlhe Corrosion of Magnesium and of the Mag-
nesium Altinminmin Alloys Containing Manga-
nese. ByJ.A.Boyer. ,TwelfthAnnual, 1926)._ $0. 20

METEOROLOGY

14 Preliminary Report on the Problem of the At-
mosphere in Relation to Aeronautics. By
Prof. Charles F. Marvin. (First Annual,
1915)------------------------------------
2 13 Meteorology and Aeronautics. By Win. R.
Blair. (Third Annual, 1917)--------------------
Part 1. Physical Properties and Dynamics
of the Atmosphere. *
Part 2. Topographic and Climatic Factors
in Relation to Aeronautics.
Part 3. Current Meteorology and Its Use.
147 Standard Atmosphere. By Willis Ray Gregg.
(Eighth Annual, 1922) --------------------- $0.05
1 Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Adilvisory Committee for Aeronautics, Wash-
ington, D. C., andl 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.








27

M ETEOROLOGY-Continued

No. Title Price

S216 The Reduiction of Airplane Flight-test Data to
Standard Atmosphere Conditions. By Wal-
ter S. Diehl and E. P. Lesley. (Eleventh An-
nual, 1925)-------------- ------------ ----
218 Standard Atmosphere-Tables and Data. By
Walter S. Diehl. (Eleventh Annual, 1925) --- $0. 10
245 Meteorological Conditions along Airways. By
W. R. Gregg. (Twelfth Annual, 1926) ------- 10
246 Tables for Calibrating Altimeters and Com-
puting Altitudes Based on the Standard At-
mosphere. By W. G. Brombacher. (Twelfth
Annual, 1926)------------------------------

MISCELLANEOUS

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 ------------------------------------ SO. 10

NOMENCLATURE

3 9 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
i Second Annual, 1916)----------------------
2 15 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
iThird Annual, 1917) --------- -------- -------
3 25 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Fourth Annual, 1918)--------------------------
91 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Sixth Annual, 1920) ---------------------- -0. 15
2 Out of print as a separate report. The annual volume containing this relp',it i
still available.
3 Out of print. Available as a separate report for reference or loan in (hlie (Wit.-e
of Aeronautical Intelligence, National Advisory Commii ee for .\erounaui ii.s
101220-30--3








28

NOMENCLATURE-Continued

No. Title Price

3 157 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Eighth Annual, 1922)-------------- --
240 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Twelfth Annual, 1926)-------------------- $0. 20
NOTE-Reports 9, 15, 25, 91, 157 are obso-
lete.

PARACHUTES

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

PROPELLERS

2 14 Experimental Research on Air Propellers. By
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.
S19 Periodic Stresses in Gyroscopic Bodies-with
Applications to Air Screws. By A. F. Zahni.
(Third Annual, 1917-----
Part 1. The Gyroscopic Particle.
Part 2. The Gyroscopic Three-Dimensional
Body.
2 i p cif print as a seimrale report. T t- annual v.)ltirnie coni gaining this repl),irt is
st ill ,t\ ,tililihh
I ( ut if Iprint. Avnilahle Las a separate report fior reference or lImn in the Office
of enr, :ti IiIt i iii Intelligncee, Nat ionaitl Ad isory (Coniuii| I ee for A ernnu I irs.








29

PROPELLERS-Continued


Title "


'29

'30

'64

S71


'109

113

141

3168

'175

S177

S178


183

S186


3196


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


No.


The General Theory of Blade Screws. By
George de Bothezat. (Fourth Annual, 1918)-- -
Experimental Research on Air Propellers-II.
By Win. F. Durand and E. P. Lesley. (Fourth
Annual, 1918)----------------------------
Experimental Research on Air Propellers-III.
By Wm. F. Durand arid E. P. Lesley. (Fifth
Annual, 1919)-----------------------------
Slip-stream Corrections in Performance Com-
putation. By Edward P. Warner. (Fifth
Annual, 1919) ----------------------------
Experimental Research on Air Propellers-IV.
By Wm. F. Durand and E. P. Lesley. (Sixth
Annual, 1920) --------------------------
Tests on Air Propellers in Yaw. By Win. F.
Durand and E. P. Lesley. (Seventh Annual,
1921)------------------------------ ----
Experimental Research on Air Propellers-V.
By Wm. F. Durand and E. P. Lesley. (Eighth
Annual, 1922)---------------------------
The General Efficiency Curve for Air Propellers.
By Walter S. Diehl. (Ninth Annual, 1923)-- -
Analysis of W. F. Durand's and E. P. Lesley's
Propeller Tests. By Max M. Munk. (Ninth
Annual, 1923)--------------------------- -
The Effect of Slip-stream Obstructions on Air
Propellers. By E. P. Lesley and B. M.
Woods. (Ninth Annual, 1923) -------------
Relative Efficiency of Direct and Geared Drive
Propellers. By Walter S. Diehl. (Ninth An-
nual, 1923)-------------------------------
The Analysis of Free-flight Propeller Tests and
Its Application to Design. By Max IM.
Munk. (Ninth Annual, 1923)------------
Application of Propeller-test Data to Design
and Performance Calculations. By Walter
S. Diehl. (Tenth Annual, 1924) ---------
Comparison of Model Propeller Tests with the
Airfoil Theory. By W. F. Durand and E. P.
Lesley. (Tenth Annual, 1924)--------------


Price


$0. 10

15


.05








30


PROPELLERS-Continued

No. Title Price

220 Comparison of Tests on Airplane Propeller in
Flight with Wind-tunnel Model Tests on Simi-
lar Forms. BRy W. F. Durand and E. P. Les-
ley. (Eleventh Annual, 1925)-------------- $0. 15
3 235 Interaction between Air Propellers and Airplane
Structures. By W. F. Durand. (Twelfth An-
nual, 1926)_- - - - - - - - -
237 Tests on Thirteen Navv Type Model Propellers.
By W. F. Durand. (Twelfth Annual, 1926.)--., 10
259 Characteristics of Propeller Sections Tested in
tlhe Variable Density Wind Tunnel. By East-
man N. Jacobs. (Thirteenth Annual, 1927)- 10
292 Characteristics of Five Propellers in Flighlit.
By J. W. Crowley, jr., and R. E. Mixson.
(Fourteentli Annual, 1928)------------------. 15
301 Full Scale Tests of Wood Propellers on a VE-7
Airplane in Ithe Propeller Research Tunnel.
By Fred E. Weick. (Fourteenth Annual,
192s)---------------------------------- .15
302 Fuill Scale Tests on a Thin Metal Propeller at
Various Tip Speeds. By Fred E. Weick.
(Fourteenth Annual, 192.) -.---- -------- 10
306 Full Scale Wind ITuinnel Tests of a Series of
IMetal Propellers on a VE-7 Airplane. By
Fred E. Weick. (Fourteenth Annual, 192S)'.- .10
326 Tests of Five Metal Model Propellers with Va-
Srious Pitclh Distribuiit ions in a Free Wind
Stream and in (Conilinlation within a Model
VE-7 Fuselage. lBv E. P. Lesley and Elliot
(G. Reid. (Fifteenth Annual, 1929)---_------- 15
33S The Effect of Red(iluction Gearing on Propeller-
boly Intcrfcre-nce as Sluown by Full Scale
A\iind TlIlncnl Tests. By Fred E. Weick.
(Sixteenth Annual, 1930) ------------------- 15
339 Full Scale Wind rITunel Tests with a Series of
Propellers of D)ifferent D)ianmeters on a Single
lFuselage. Bv Fred E'. Weick. (Sixteenth
Annual, 193d) -----------------------------. 15
340 tFull Scale Wind l'tIu tine! Tests on Several Metal
Pr(l)pellers having I)ifferent Blade Forms.
BYl Fred 1:. Weick. (Sixteenth Annual, 1930)-- 10

SOut of print. Available as a separate report for reference or loan in the Offlice
of AeronautLical Intelligence, Natlinal Ailvisury ('unminitlee for Aeronaut irs.










SEAPLANES

No. Title Price

3209 Characteristics of a Single-float Seaplane during
Take-off. By J. W. Crowley, jr., and K. M.
Ronan. (Tenth Annual, 1924)-------------------
3226 Characteristics of a Boat-type Seaplane during
Take-off. By J. W. Crowley, jr., and K. M.
Ronan. (Eleventh Annual, 1925)-----------------
242 Characteristics of a Twin-float Seaplane during
Take-off. By John W. Crowley, jr., and K.
M. Ronan. (Twelfth Annual, 1926)---------$0. 10
290 Water Pressure Distribution on a Seaplane
Float. Bv F. L. Thompson. (Fourteenth
Annual, 1928)----------------------------- .10
328 Water Pressure Distribution on a Twin-float
Seaplane. By F. L. Thompson. (Fifteenth
Annual, 1929)---------------------------- 10

STABILITY AND CONTROL

11 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)----------
3 26 The Variation of Yawing Moment Due to Roll-
ing. By E. B. Wilson. (Fourth Annual,
1918)------------------------------------------
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronaut ics,Wash-
ington, D. C., and in the libraries of large cities.
S'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.








32

STABILITY AND CONTROL-Continued

No. Title Price

3 27 Theory of an Airplane Encountering Gusts-III.
By E. B. Wilson. (Fourth Annual, 1918)-_ ------
3 95 Diagrams of Airplane Stability. By H. Bate-
men. (Sixth Annual, 1920)-------------------
3 96 Statical Longitudinal Stability of Airplanes.
By Edward P. Warner. (Sixth Annual, 1920) ------
' 112 Control in Circling Flight. By F. H. Norton
and E. T. Allen. (Seventh Annual, 1921) --- ------
3 120 Practical Stability and Controllability of Air-
planes. By F. H. Norton. (Seventh Annual,
1921)------------------------------------ ------
$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. Bv Edwin B.
Wilson. (Ninth Annual, 1923)------------- $0.05
293 Two Practical Methods for the Calculation of
the Horizontal Tail Area Necessary for a
Statically 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. Heald 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

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)---------------..................---'.....
I Out nrif print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash-
ington. 1). ('.. and in the libraries of large cities.
3 Out of print. Available as a separate report for reference or loan in the Office
of Aeronatuical Intelligence, National Advisory Committee for Aeronautics.










STRENGTH OF CONSTRUCTION-Continued

No. Title Price

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)---------- ----------------------------
3 82 Airplane Stress Analysis. By A. F. Zahm.
(Fifth Annual, 1919)----------------------i------
3 92 Analysis of Wing Truss Stresses. By Edward
P. Warner and Roy G. Miller. (Sixth Annual,
1920)------------------------------------------
3 104 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. Zahm, 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. Bea.r, and G. C. Hill.
(Eighth Annual, 1922)---------------------- .05
3143 Analysis of Stresses in German Airplanes. By
Wilhelm Hoff. (Eighth Annual, 1922)--..-. -- I------
3161 The Distribution of Lift Over Wing Tips and
Ailerons. By David L. Bacon. NintIt
Annual, 1923)-----------------------------------
3 180 The Influence of the Form of a WVooden 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)-------------------
3 181 The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-II: Form
Factors of Beams Subjected to Transverse
Loading Only. By J. A. Newlin and G. W.
Trayer. (Ninth Annual, 1923)-------------------
3 188 Thle 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
Sand G. W. Trayer. (Tenth Annual, 1924)......
I (ut of print. Available as a separate report for reference or loan in lthe Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










STRENGTH OF CONSTRUCTION-Continued


Title


214 Wing Spar Stress Charts and Wing Truss
Proportions. By Edward P. Warner. (Elev-
enth Annual, 1925)----------------------
3251 Approximations for Column Effect in Airplane
Wing Spars. By Edward P. Warner and
Mac Short. (Twelfth Annual, 1927)------..
329 The Torsional Strength of Wings. By C. P.
Burgess. (Fifteenth Annual, 1929)-----
334 The Torsion of Members Having Sections
Common in Aircraft Construction. By
George W. Trayer and H. W. March--------
344 The Design o)f Plywood Webs for Airplane Wing
Beams. By George W. Trayer. (Sixteenth
Annual, 1.130) -- --- --- --


Price


$0. 10


10

S25

S10


WIND TUNNELS AND LABORATORIES

The Altitu:de Laboratory for the Testing of
Aircraft Engines. By H. C. Dickinson and
H. G. Boutell. (Fourth Annual, 1918)-_--- $0. 10
Wind-tunnel Balances. By Edward P. Warner
and F. H. Norton. (Fifth Annual, 1919)_.. 10
The Design of Wind Tunnels and Wind-tunnel
Propellers. By Edward P. Warner and F.
H. Norton. (Fifth Annual, 1919)----------------
Construction of Models for Tests in Wind Tun-
nels. By F. H. Norton. (Fifth Annual,
1919)--------------------------------- ------
Design of Wind Tunnels and Wind-tunnel
Propellers-11. By F. H. Norton and Ed-
ward P. Warner. (Sixth Annual, 1920)-----------
The Six-component Wind Balance. By A. F.
Zahm. (Eighth Annual, 1922)------------- .05
Standardization Tests of N. A. C. A. No. 1
Wind Tiunnel. By Elliott G. Reid. (Tenth
Annual. 1924)---------------------------- 10
The Variable-density Wind Tunnel of the
National Advisory Committee for Aeronau-
tics. By Max M. Munk and Eiton W. Miller.
(Eleventh Annual, 1925)------------------- 10


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


No.


44

72
3 73

3 74

3 98


146


195

227


I








35


WIND TUNNELS AND LABORATORIES-Continued

No. Title Price

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)---------------------------- $0. 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. Bv Eastman N. Jacobs. (Fifteenth
Annual, 1929)----------------------------- 10
342 Effect of Turbulence in Wind Tunnel Measure-
ments. By H. L. Dryden and A. M. Kuethe.
(Sixteenth'Annual, 1930)-------------------------




























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UNIVERSITY OF FLORIDA
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3 1262 09082 7006