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:
AA00022345:00002

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
    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, 1928


UNITED STATES
GOVERNMENT PRINTING OFFICE
WASHINGTON
1928


















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 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 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 Intelli-
gence, National Advisory Committee for Aeronautics, Wash-
ington, D. C.
(IiI)























































0



















INDEX
Page
Annual reports------------------------------------ 1
Bibliographies ----------------------------------1---
Technical reports---------------------------------- 3
Aerodynamics --------------------------------- 3
Airfoils and wing sections----------------------- 4
Airplanes-Full scale experiments ...---------------- 6
Airplanes-Model experiments-------------------- 8
Airships --------------------------------------- 10
Engines--------------------------------------- 11
Fuels----------------------------------------- 17
Gases---------------------------------------- 18
Helicopters- ------------------ -------- --- 18
Instruments- ---------------------------------- 18
Materials ------------------------------------- 21
Meteorology ------------------------------------ 23
Nomenclature ---------------------------------- 23
Parachutes ------_------------------------------ 24
Propellers ------_--------------------- ---------24
Seaplanes-------------- ----------------------- 26
Stability and control --------------------------- 27
Strength of construction ------------------------ 28
Wind tunnels and laboratories------------------- 29
(v)

















Digitized by the Internet Archive
in 2013











http://archive.org/details/Ilis 1928unit















NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


ANNUAL REPORTS

Year Price


First1----- 1915 With Reports Nos. 1-7-------------
Second 1-- 1916 With Reports Nos. 8-12----------
Third----- 1917 With Reports Nos. 13-23----- $1. 50
Fourth 1--- 1918 With Reports Nos. 24-50-----------
Fifth------ 1919 With Reports Nos. 51-82-.--. 1.50
Sixth 1---- .1920 With Reports Nos. 83-110-----------
Seventh 1_ 1921 With Reports Nos. 111-132----------
Eighth 1 --- 1922 With Reports Nos. 133-158-----------
Ninth----- 1923 With Reports Nos. 159-185--- 1.00
Tenth----- 1924 With Reports Nos. 186-209--_ 1. 35
Eleventh__ 1925 With Reports Nos. 210-232--- 1.00
Twelfth -.. 1926 With Reports Nos. 233-256-_- 1.50
Thirteenth- 1927 With Reports Nos. 257-282 (in-------
press).

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


BIBLIOGRAPHIES


Bibliography of Aeronautics
Bibliography of Aeronautics
Bibliography of Aeronautics
Bibliography of Aeronautics
Bibliography of Aeronautics
Bibliography of Aeronautics
Bibliography of Aeronautics


(1909-1916)------------
(1917-1919)------------
(1920-1921)- ----- ------
(1922)----------------
(1923)--_--------------
(1924)-----------------
(1925)------------------


$2.00
.75
35
25
25
.25
.50














































































































I










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
2 78 The Limiting Velocity in Falling from a Great
Height. By Edwin Bidwell Wilson. (Fifth
Annual, 1919)---------------------------------
2 79 Bomb 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)------------
97 General Theory of the Steady Motion of an
Airplane. By George de Bothezat. (Sixth
Annual, 1920)--------------------------- 15
114 Some New Aerodynamical Relations. By Max
M. Munk. (Seventh Annual, 1921)----------. 05
116 Applicacations 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
S151 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
1 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.
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.


100978-28-2


(3)










AERODYNAMICS-Continued


No. Title Price

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)-------------- $0.05
213 A Resum6 of the Advances in Theoretical
Aeronautics Made by Max M. Munk. By
Joseph S. Ames. (Eleventh Annual, 1925)-.- 15
247 Pressure of Air on Coming to Rest from Various
Speeds. By A. F. Zahm. (Twelfth Annual,
1926)------------------------------------ .05
253 Flow and Drag Formulas for Simple Quadrics.
By A. F. Zahm. (Twelfth Annual, 1927)-- 10
287 Theories of Flow Similitude. By A. F. Zahm.
(Thirteenth Annual, 1927)------------------------
289 Forces on Eliptic Cylinder in Uniform Air
Stream. By A. F. Zahm, R. H. Smith, and
F. A. Louden. (Fourteenth Annual, 1928)--------

AIRFOILS AND WING SECTIONS


S18


28

S75

2 77

* 93

'111


Aerofoils and Aerofoil Structural Combinations.
Combinations. By Lieut. Col. Edgar S.
Gorrell and Maj. H. S. Martin. (Third An-
nual, 1917)---------------------------
An Introduction to the Study of the Laws of Air
Resistance of Aerofoils. By George de
Bothezat. (Fourth Annual, 1918)-----------
The Aerodynamic Properties of Thick Aerofoils
Suitable for Internal Bracing. By F. H.
Norton. (Fifth Annual, 1919)--------------
The Parker Variable Camber Wing. By H. F.
Parker. (Fifth Annual, 1919)---------------
Aerodynamic Characteristics of Airfoils. By
National Advisory Committee for Aero-
nautics. (Sixth Annual, 1920) --------------
The Variation of Airfoil Lift and Drag Coeffi-
cients with Changes in Size and Speed. By
W. S. Diehl. (Seventh Annual, 1921) --------


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.
4 Not issued as a separate report. The annual volume containing this report is
still available.












No.

121

124

142

S150

'152

169

182

2191

200

201

207

217


221


5

AIRFOILS AND WING SECTIONS-Continued

Title

The Minimum Induced Drag of Airfoils. By
Max M. Munk. (Seventh Annual, 1921) -----
Aerodynamic Characteristics of Airfoils-II.
By the National Advisory Committee for
Aeronautics. (Seventh Annual, 1921) -----
General Theory of Thin Wing Sections. By
Max M. Munk. (Eighth Annual, 1922)---
Pressure Distribution over Thick Aerofoils-
Model Tests. By F. H. Norton and D. L.
Bacon. (Eighth Annual, 1922)----------
The Aerodynamic Properties of Thick Aero- I
foils-II. By F. H. Norton and D. L.
Bacon. (Eighth Annual, 1922) -------------
The Effect of Airfoil Thickness and Plan Form
on Lateral Control. By H. I. Hoot. (Ninth
Annual, 1923)----------------------------
Aerodynamic Characteristics of Airfoils-III.
By the National Advisory Committee for
Aeronautics. (Ninth Annual, 1923)---------
Elements of the Wing Section Theory and of the
Wing Theory. By Max M. Munk. (Tenth
Annual, 1924) -------- ---- --
Some Problems on the Lift and Rolling Mo-
ments of Airplane Wings. By Jas. B. Scar-
borough. (Tenth Annual, 1924)------------
The Effects of Shielding the Tips of Airfoils.
By Elliott G. Reid. (Tenth Annual, 1924)--
Aerodynamic Characteristics of Airfoils at High
Speeds. By L. J. Briggs, G. F. Hull, and
H. L. Dryden. (Tenth Annual, 1924)------
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)-----------
Model Tests with a Systematic Series of 27
Wing Sections at Full Reynolds Number.
By Max. M. Munk and Elton W. Miller. I
(Eleventh Annual, 1925)-----------------I


.05

.15


.10

.05

.10


.10


.10


* Out of print as a separate report. The annual volume containing this report is
still available.
* Out of print. Available as a separate report for reference or loan in the office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.


Price


$0.05

.10

.05










AIRFOILS AND WING SECTIONS-Continued

No. Title Price

229 Pressure Distribution Over Thick, Tapered Air- I
foils, N. A. C. A. 81, U. S. A. 27 C Modified
and U. S. A. 35. By Elliott G. Reid.
(Eleventh Annual, 1925) ------------------- $0. 10
233 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) ------------ 10
244 Aerodynamic Characteristics of Airfoils-IV.
By National Advisory Committee for Aero-
nautics. (Twelfth Annual, 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.
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.
Smith. (Thirteenth Annual, 1927)---------- 10
285 A Study of Wing Flutter. By A. F. Zahm and
R. M. Bear. (Fourteenth Annual, 1928)-----------
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.
Bv Montgomery Knight and Oscar Loeser, jr.
(Fourteenth Annual, 1928)----------------------

AIRPLANES-F U LL-SCALE EXPERIMENTS

2 69 A Study of Airplane Ranges and Useful Loads.
By J. C. Coffin. (Fifth Annual, 1919)-
2 70 Preliminary Report on Free Flight Tests. By
Edward P. Warner and F. H. Norton. (Fifth
Annual, 1919)- ---------------------------
I Out of print as a separate report. The annual volume containing this report
Is still available.










No.


2 Out of print as a separate report. The annual volume containing this report is
still available.


105

118

148


149

154

155

162

163


167

170

173


174

'192


AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

Title Price

Angles of Attack and Air Speeds During Maneu-
vers. By Edward P. Warner and F. H.
Norton. (Sixth Annual, 1920) ------------- $0. 05
The Pressure Distribution Over the Horizontal
Tail Surfaces of an Airplane. By F. H. Nor-
ton. (Seventh Annual, 1921)------------- 15
The Pressure Distribution Over the Horizontal
Tail Surfaces of an Airplane-III. By F. H.
Norton and W. G. Brown. (Eighth Annual,
1922)------------------------------------ .05
Pressure Distribution Over the Rudder and Fin
of an Airplane in Flight. Bv F. H. Norton
and W. G. Brown. (Eighth Annual, 1922)-..- 05
A Study of Taking Off and Landing an Airplane.
By T. Carroll. (Eighth Annual, 1922)------- .05
A Study of Airplane Maneuvers with Special
Reference to Angular Velocities. By H. J.
E. Reid. (Eighth Annual, 1922)------ .05.
Complete Study of the Longitudinal Oscillation
of a VE-7 Airplane. By F. H. Norton and
W. G. Brown. (Ninth Annual, 1923)---- 05.
The Vertical, Longitudinal, and Lateral Accelera-
tions Experienced by an S-5A Airplane while
Maneuvering. By F. H. Norton and T.
Carroll. (Ninth Annual, 1923)------------- .05
The Measurement of the Damping in Roll on a
JN4H in Flight. By F. H. Norton. (Ninth
Annual, 1923)----------------------------..... 05
A Study of Longitudinal Dynamic Stability in
Flight. By F. H. Norton. (Ninth Annual,
1923)------------------------------------.......................... 05
Reliable Formule for Estimating Airplane
Performance and the Effects of the Changes in
Weight, Wing Area, or Power. By Walter
S. Diehl. (Ninth Annual, 1923) ------------.. .05
The Small Angular Oscillations of Airplanes inii
Steady Flight. By F. H. Norton. (Ninth
Annual, 1923)----------- ... ..---------- .. 05
Charts for Graphical Estimation of Airplane
Performance. By Walter S. Diehl. (Tenth
Annual, 1924)---- - - - - - - - -


I












No.


Price


AIRPLANES-FULL-SCALE EXPERIMENTS-Continued

Title

Pressure Distribution Over the Wings of an
MB-3 Airplane in Flight. By F. H. Norton.
(Tenth Annual, 1924)--- ____
Investigation of Slip Stream Velocity. By J. W.
Crowley, jr. (Tenth Annual, 1924) ---
Accelerations in Flight. By J. H. Doolittle.
(Tenth Annual, 1924) ---------
Some Aspects of the Comparison of Model and
Full-scale Tests. By D. W. Taylor. (Elev-
enth Annual, 1925)------------------------
A Study of the Effect of a Diving Start on Air-
plane Speed. By Walter S. Diehl. (Eleventh
Annual, 1925) ------------------------
Three Methods of Calculating Range and En-
durance of Airplanes. By Walter S. Diehl.
(Twelfth Annual, 1926)--------------------
The Effect of Flight Path Inclination on Airplane
Velocity. By Walter S. Diehl. (Twelfth
Annual, 1926)---------------------------
A Comparison of the Take-off and Landing
Characteristics of a Number of Service Air-
planes. By Thomas Carroll. (Twelfth An-
nual, 1927)-------------------------------
Pressure Distribution Over a Wing and Tail
Rib of a VE-7 and of a TS Airplane in Flight.
By J. W. Crowley, jr. (Thirteenth Annual,
1927)------------------------------------
A Full-Scale Investigation of Ground Effect.
By Elliott G. Reid. (Thirteenth Annual,
1927)------------------------------------


AIRPLANES-MODEL EXPERIMENTS


Construction of Models for Tests in Wind Tun-
nels. By F. H. Norton. (Fifth Annual, 1919).
The Pressure Distribution Over the Horizontal
Tail Surfaces of.an Airplane-II. By F. H.
Norton and D. L. Bacon. (Seventh Annual,
1921) ---- ---------------------------


$0. 10


I Out of print as a separate report. The annual volume containing this report
Is still available.


193

194
I
203

r219

228

234

238

249


257


265


$0. 15
.05

.10

.10

.05

.10

.05


.10


15

.05


2 74

119
*










AIRPLANES-MODEL EXPERIMENT-Continued

No. Title Price

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)------------------------ $0.05
133 The Tail Plane. By Max M. Munk. (Eighth
Annual, 1922)----------------------------- 10
136 Damping Coefficients Due to Tail Surfaces in
Aircraft. By Lynn Chu. (Eighth Annual,
1922)------------------------------------ .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
225 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)----------------------------- .05
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. By 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-
maker. (Thirteenth Annual, 1927)--------- .10
273 Wind Tunnel Tests on Autorotation and the
"Flat Spin." By Montgomery Knight.
(Thirteenth Annual, 1927)------------------ .10








10

AIRPLANES-MODEL EXPERIMENT-Continued


No. Title Price

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)------ $0. 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. Bv 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
I 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 lse in Airship
Design. By L. B. Tuckerman. (Eleventh
Annimal, 1925)---------------------------- .05
211 Water Model Tests for Semirigid Airships. By
L. B. Tuctkerman. (Eleventh Annual, 192.5)__.. .05
212 Stabitlity E:quations for Airs.hip Huills. By A. F.
Zahm. (Eleventh Annual, 1925)------------- .05
215 Air Forces, Moments, and Damping on Model I
of Fleet Airship Sheiiandoah. By A. F.
Zalim, RI. 1. Smith, and F. A. Louden.
(El(:hevIIth Anniual, 1925)_ ------------------- 15
223 Pressure D)istribution on the (C-7 Airship. By
J. W. Crowley, jr., and S. J. DeFrance.
(Eleventh Annual, 1925)-------------------- 15






11

ENGINES

No. Title Price

1 7 Thermodynamic 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.
1 10 Mufflers for Aeronautic Engines. By Prof. H.
Diederichs and Prof. G. B. Upton. (Second
Annual, 1916)----------------------------------
1 11 Carburetor Design-A Preliminary Study of the
State of the Art. By Charles Edward Lucke,
assisted by Friederich 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 Ein-
gines at High Altitudes.
Part 2. Radiator Design.
Part 3. Spark Plugs.
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
Altitude 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.
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 Offioe
yf Aeronautical Intelligence, National Advisory Committee for Aeronautics.
4 Not issued as a separate report. The annual volume containing this report
is still available.
100978-28--3








12

ENGINES-Continued

No. Title Price

Effect of Compression Ratio, etc.-Continued.
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.
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)---------------------------- --
3 49 Metering Characteristics of Carburetors. By
SP. S. Tice. (Fourth Annual, 1918)------------
2 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.
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
2 53 Properties and Preparation of Ceramic Insila-
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 Hi igh Temperatures.
By R. K. Honaman ani E. L. Fonseca.
Part 3. Preparation and Composition of
Ceramic Bodies for Spark-plug Insula-
tors. By A. V. Bloininger.
Part 4. Cements for Spark-plug Electrodes.
I By If. F. StaleY.
54 Effect of Tremperature and Pressure on the
Sparking Voltage. By F. B. Silsbee and L.
B. Loci). (Fifth Annuiial, 1919)------------ .05
2 Out of print as a separate report. The annual volume containing this report is
still available.
I Out of print. Available as a sejiarale rpport for reference or loan in the Off&le
of Aeronaut ical Intelligoence, National Advisory (Commnittee for Aeronautics.








13

ENGINES-Continued

No. Title Price

55 Investigation of the Muffling Problem for Air-
plane Engines. By G. B. LUpton and V. R.
Gage. (Fifth Annual, 1919)---------------- $0. 10
2 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.
257 The Subsidiary Gap as a Means for Improving
Ignition. By W. S. Gorton. (Fifth Annual,
1919)----------- -- --- -------------- --
58 Characteristics of High-tension Magnetos.
(Fifth Annual, 1919)----------------------- 10
Part 1. Cycle of Operation of Jump-spark
Ignition Systems. By F. B. Silsbee.
Part 2. Transformation Ratioand Coupling
in High-tension Magnetos. By F. B.
Silsbee.
59 General Analysis of Airplane Radiator Problems. I
By H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt. (Fifth Annual, 1919)-------- .05
60 General Discussion of Test Methods for Radi-
ators. By H. C. Dickinson, W. S. James, and
W. B. Brown. (Fifth Annual, 1919)--------- .10
61 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. B%- S. R. Parsons.
62 Effect of Altitude on Radiator Performance.
By W. S. James and S. R. Parsons. ,Fifth
Annual, 1919)--------------------------- 10
I Out of print as a separate report. The annual volume containing this report is
still available.








14

ENGINE S-Continued

No. Title Price

63 Results of Tests on Radiators for Aircraft En-
gines. (Fifth Annual, 1919)-------------- $0.10
Part 1. Heat Dissipation of Radiators. By
H. C. Dickinson, W. S. James, and R. V.
Kleinschmidt.
Part 2. Water Flow through Radiatdr
Cores. By W. S. James.
86 Properties of Special Types of Radiators. By
S. R. Parsons. (Sixth Annual, 1920)-------- 10
87 Effects of Nature of Cooling Surface on Radiator
Performance. By S. R. Parsons and R. V.
Kleinschmidt. (Sixth Annual, 1920) ------- .05
88 Pressure Drop in Radiator Air Tubes. By S. R.
Parsons. (Sixth Annual, 1920)------------ .05
101 The Calculated Performance of Airplanes
Equipped with Supercharging Engines. By
E. C. Kemble. (Sixth Annual, 1920)-------- 15
8102 Performance of a Liberty 12 Airplane Engine.
By S. W. Sparrow and H. S. White. (Sixth
Annual, 1920)----------------------------------
103 Performance of a 300-horsepower Hispano-
Suiza Airplane Engine. By S. W. Sparrow
and H. S. White. (Sixth Annual, 1920)----- .05
106 Turbulence in the Air Tubes of Radiators for
Aircraft Engines. By S. R. Parsons. (Sixth
Annual, 1920)-------------------------- .05
108 Some Factors of Airplane Engine Performance.
Bv Victor R. Gage. (Sixth Annual, 1920) --- .10
1123 Simplified Theory of the Magneto. By F. B.
Silsbee. (Seventh Annual, 1921)..----------------
134 Performance of Maybach 300-horsepower Air-
plane Engine. By S. W. Sparrow. (Eighth
Annual, 1922)---------------------------- .05
135 Performance of B. M. W'. 185-horsepower Air-
plarine Enigine. By S. W'. Sparrow. (Eighth
Annual, 1922)--------------------------- .05
S158 Mathematical Equations for Head Conduction
in the Fins of Air-cooled Engines. By D. R.
Harper and W. G. Brown. (Eighth Annual,
1922)----------------------------------------
159 Jet Propulsion for Airplanes. By Edgar Buck-
irbghamni. (Ninth Annual, 1923)------------- .05
I Out of print. Av'ilil'le as a separate report for reference or loan in the Office of
Aeroria jticu.J lutelligence, Natijoval Advisory Committee for Aeronautics.










ENGINES-Continued


No. Title Price

171 Engine Performance and the Determination of
Absolute Ceiling. By Walter S. Diehl.
(Ninth Annual, 1923)---------------------- $0.05
179 The Effect of Electrode Temperature on the
Sparking Voltage of Short Spark Gaps. By
F. B. Silsbee. (Ninth Annual, 1923)-------- .05
2187 Flame Speed and Spark Intensity. By D. W.
Randolph and F. B. Silsbee. (Tenth Annual,
1924)---------------------------------------
2189 Relation of Fuel-air Ratio to Engine Perform-
ance. By Stanwood W. Sparrow. (Tenth
Annual, 1924)-------------------------------
190 Correcting Horsepower Measurements to a
Standard Temperature. By Stanwood W.
Sparrow. (Tenth Annual, 1924) ------------ .05
202 The Sparking Voltage of Spark Plugs. By F.
B. Silsbee. (Tenth Annual, 1924) ---------- .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
224 An Investigation of the Coefficient of Discharge
of Liquids Through Small Round Orifices.
By W. F. Joachim. (Eleventh Annual, 1925)-- .05
230 Description and Laboratory Tests of a Roots
Type Aircraft Engine Supercharger. By
Marsden Ware. (Eleventh Annual, 1925)--' . 10
239 Power Output and Air Requirements of a Two-
stroke Cycle Engine for Aeronautical Use.
Bv C. R. Paton and Carlton Kemper.
(Twelfth Annual, 1926) -------------------- 10
241 Electrical Characteristics of Spark Generators
for Automotive Ignition. By R. B. Brode,
D. W. Randolph, and F. B. Siisbee. (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
2 Out of print as a separate report. The annual volume containing this report
is still available.








16

ENGINES-Continued


No. Title Price

250 Description of the N. A. C. A. Universal Test
Engine and Some Test Results. By Marsden
Ware. (Twelfth Annual, 1926) ------------ $0. 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)-------------------- .10
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)------------------ .05
261 Resistance and Cooling Power of Various Radia-
tors. By R. H. Smith. (Thirteenth Annual,
1927)------------------------------------ .10
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
268 Factors in the Design of Centrifugal Type In-
jection Valves for Oil Engines. By W. F.
Joachim and E. G. Beardsley. (Thirteenth
Annual, 1927)---------------------------- .10
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
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)------------------ .10
27t6 Combustion Time in the Engine Cylinder and
Its Effect on Engine Performance. By
Charles F. Marvin, jr. (Thirteenth Annual,
1927)------------------------------------ 10
277 The Comparative Performance of an Aviation
Engine at Normal and High Inlet Air Ternm-
peratures. By Arthur W. Gardiner and Oscar
W. Schey. (Thirteenth Annual, 1927)----- .10








17

ENGINES-Continued

No. Title Price

280 The Gaseous Explosive Reaction-The Effect of
Inert Gases. By F. W. Stevens. (Thirteenth
Annual, 1927)---------------------------- $0. 10
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)------ - .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 W. Schey. (Fourteenth
Annual, 1928)--------------------------- 10
284 The Comparative Performance of Roots Type
Aircraft Engine Superchargers as Affected by
Change in Impeller Speed and Displacement. i
By Marsden Ware and Ernest E. Wilson.
(Fourteenth Annual, 1928)----------------- 10


FUELS

42 A New Process for the Production of Aircraft-
engine Fuels. By Auguste Jean Paris, jr.,
and W. Francklyn Paris. (Fourth Annual,
1918)----------------------------- ------ $0.05
47 Power Characteristics of Fuels for Aircraft
Engines. (Fourth Annual, 1918)----------- 10
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 Aviation Fuel with Ex-
port Aviation Gasoline. By V. R. Gage, S. W.
Sparrow, and D. R. Harper. (Sixth Annual,
1920)------------------------------------ .05








18

FUELS-Continued

No. Title Price


90 Comparison of Hector Fuel with Export Avia-
tion Gasoline. By H. C. Dickinson, V. R.
Gage and S. W. Sparrow. (Sixth Annual,
1920)----------------------------- ------ $0. 05
232 Fuels for High-compression Engines. By Stan-
wood W. Sparrow. (Eleventh Annual, 1925)__- 10


GASES

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


HELICOPTERS

280 Stability of the Parachute anrid Hielicopter. By
11. Bateman. (Fifth Annual, 1919)


INSTRUMENTS


1 2 Investigation of Pitot Tubel'. (First Annual,
19)15)---------------------------------------
Part. 1. The Pitot Tube and Other Anemrnom-
eters., for Airplanes. By \W. H1. Herschel.
Part 2. The Theory of the Pitot and Venturi
1'tIbes. By E. B ickinlighain.
I S (General Specifications Covering Requirements
of Aeronauttic Instruments. By the National
.\visor (y i Committee for Aeronautics. (Sec-
mid l.\nintal, 191)--------------------- ---
I 1Il 'if I4rilf. .\ A11111i l %l(1itle avait ii.]c for reference or loan in the Office of
A.kernimmi iil 1w' if T Igencr, Nat!ional A'l'visiiry ('oliiitlllee for Aeronaulics, Wash-
irl ,im. jI :ir,,l in I li: Iih'airi e, of Iirgt' cilieS.
()ul (1f r1! ,, u 'Uiritraile report. The anijual volume containing this report is
.still uVlall:tl)h1.








19

INSTRUMENTS-Continued

No. Title Price

31 Development of Air Speed Nozzles. By A. F.
Zahm. (Fourth Annual, 1918)-------------- $0. 10
32 The Airplane Tensiometer. By L. J. Larson.
(Fourth Annual, 1918)--------------------- .05
50 Calculation of Low Pressure Indicator Dia-
grams. By E. C. Kemble. Fourth Annual,
1918)------------------------------------- .05
81 Comparison of U. S. and British Standard
Pitot-static Tubes. By A. F. Zahm and
R. H. Smith. (Fifth Annual, 1919)---------- .05
94 The Efficiency of Small Bearings in Instruments
of the Type Used in Aircraft. By F. H.
Norton. (Sixth Annual, 1920)-------------- .05
99 Acceleration in Flight. By F. H. Norton and
E. T. Allen. (Sixth Annual, 1920)-------- --- 10
100 Accelerometer Design. By F. H. Norton and
Edward P. Warner. (Sixth Annual, 1920) -- .05
107 A High-speed Engine Pressure Indicator of
the Balanced Diaphragm Type. By H. C.
Dickinson and F. B. Newell. (Sixth Annual,
1920)------------------------------------ .05
110 The Altitude Effect on Air Speed Indicators.
By M. D. Hersey, F. L. Hunt, and H. N.
Eaton. (Sixth Annual,.1920)-------------- 10
125 Aeronautic Instruments: Section I-General
Classification of Instruments and Problems
Including Bibliography. By Bureau of
Standards. (Seventh Annual, 1921)--------- .05
126 Aeronautic Instruments: Section II-Altitude
Instruments. By Bureau of Standards.
(Seventh Annual, 1921) ---------------------. 15
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.
127 Aeronautic Instruments: Section III-Aircraft
Speed Instruments. By Bureau of Stand-
ards. (Seventh Annual, 1921)------------- 10
Part 1. Air Speed Indicators.
Part 2. Testing of Air Speed Meters.
Part 3. Principles of Ground-speed In-
struments.








20


INSTRUMENTS-C ontinued

No. Title Price

128 Aeronautic Instruments: Section IV-Direc-
tion Instruments. By Bureau of Standards.
(Seventh Annual, 1921)------------------- $0. 15-
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.
129 Aeronautic Instruments: Section V-Power-
plant Instruments. By Bureau of Stand-
ards. (Seventh Annual, 1921)-------------- 15
Part 1. Airplane Tachometers.
Part 2. Testing of Airplane Tachometers.
Part 3. Thermometers for Aircraft Engines. L '
Part 4. Air-pressure and Oil-pressure r'
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. By Bureau of
Standards. (Seventh Annual, 1921) --------- 10
132 Aeronautic Instruments: Section VIII-Recent
Developments and Outstanding Problems.
By Bureau of Standards. (Seventh Annual,
1921)------------------------------------ .05
156 The Altitude Effect of Air Speed Indicators-11.
By H. N. Eaton and W. A. McNair. (Eighth
Annual, 1922) ----------------------------. 10
160 An Airship Slide Rule. By E. R. Weaver and
S. F. Pickering. (Ninth Annual, 1923)------- .05
165 Diaphragms for Aeronautic Instruments. By
MN. D. Hersey. (Ninth Annual, 1923)------ .10
166 The Aerodynamic Plane Table. By A. F.
Zahm. (Ninth Annual, 1923)-------------- .05
176 A Constant-pressure Bomb. By F. W. Stevens.
(Ninth Annual, 1923)---------------------- 0
198 Astronomical Methods in Aerial Navigation.
By K. Hilding Beij. (Tenth Annual, 1924)-----








21


INSTRUMENTS-Continued


No. Title Price

199 Interference Tests on an N. A. C. A. Pitot Tube.
By EUlliott G. Reid. (Tenth Annual, 1924)-..- $0. 05
206 Nonmetallic Diaphragms for Instruments. By
H. N. Eaton and C. T. Buckingham. (Tenth
Annual, 1924)----------------------------- .10
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

MATERIALS

1 5 Relative Worth of Improvements on Fabrics.
By the Goodyear Tire and 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.
4 16 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.
4 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.
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.
I Not issued as a separate report. The annual volume containing this report is
still available.








22


MATERIALS-Continued

No. Title Price

33 Self-luminous Materials. By N. E. Dorsey.
(Fourth Annual, 1918)--------------------- $0.05
34 Aluminum and its Light AllUovs. By Paul D.
Merica. (Fourth Annual, 1918)------------ .05
3 36 The Structure of Airplane Fabrics. By E.
Dean Walen. (Fourth Annual, 1918)-------------
37 Fabric Fastenings. By E. Dean Walen and R.
T. Fisher. (Fourth Annual, 1918)---------- .05
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) ------------------- .05
Part 1. Characteristic Exposure Tests of
Balloon Fabrics.
Part 2. Use of Ultra-violet Light for Test-
ing Balloon Fabrics.
65 The Kiln Drying of Woods for Airplanes. By
Harry D. Tieman. (Fifth Annual, 1919)----- 10
2 66 Glues Used in Airplane Parts. By S. W. Allen
and T. R. Truax. (Fifth Annual, 1919).---------
67 Supplies and Production of Aircraft Woods.
By W. N. Sparhawk. (Fifth Annual, 1919)-- 15
68 The Effect of Kiln Drying on the Strength of
Airplane Woods. By T. R. C. Wilson. (Fifth
Annual, 1919)---------------------------- .15
8 84 Data on the Design of Plywood for Aircraft.
By Armin Elmnendorf. (Sixth Annual, 1920)-------
2 85 Moisture Resistant Finishes for Airplane Woods.
By NI. E. Dunlap. (Sixth Annual, 1920)----------
145 Internal Stresses in Laminated Construction.
By A. L. Heim, A. C. Knauss, and Louis Seut-
ter. (Eighth Annual, 1922) ---------------- 10
248 The Corrosion of Magnesium and of the Mag-
nesium Aluminum Alloys Containing Manga-
nese. By J. A. Boycr. (Twelfth Annual, 1926). .20

2 Out of print as a separate report. The annual volume containing this report is
still available.
a Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Commuuuittlee for Aeronautics.








23


METEOROLOGY


No.


NOMENCLATURE


Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Second Annual, 1916)---------------------
Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Third Annual, 1917)-----------
Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Fourth Annual, 1918)---------- --


Price


Title

Preliminary Report on the Problem of the At-
mosphere in Relation to Aeronautics. By
Prof. Charles F. Marvin. (First Annual,
1915)------------------------------------
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.
Standard Atmosphere. By Willis Ray Gregg.
(Eighth Annual, 1922) ----------
The Reduction of Airplane Flight-test Data to
Standard Atmosphere Conditions. By Wal-
ter S. Diehl and E. P. Lesley. (Eleventh An-
nual, 1925)------------------------------
Standard Atmosphere-Tables and Data. By
Walter S. Diehl. (Eleventh Annual, 1925)---
Meteorological Conditions along Airways. By
W. R. Gregg. (Twelfth Annual, 1926)----
Tables for Calibrating Altimeters and Com-
puting Altitudes Based on the Standard At-
mosphere. By W. G. Brombacher. (Twelfth
Annual, 1926)-- ------------


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.
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.


14



13





147

216


218

245

246


$0. 10





.05


.10

.10

.10


.10


39

2 15


3 25








24

NOMENCLATURE-Continued


No. Title Price

91 Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Sixth Annual, 1920)---------------------- $0. 15
2 157 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)-------------------- .20
NoTE.-Reports 9, 15, 25, 91, 157 are obso-
lete.


PARACHUTES

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

PROPELLERS

3 14 Experimental Research on Air Propellers. By
Wm. 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.
I 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.








25


PROPELLERS-Continued


No. Title Price

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
Body.
29 The General Theory of Blade Screws. By
George de Bothezat. (Fourth Annual, 1918)._ $0. 20
30 Experimental Research on Air Propellers-II.
By Win. F. Durand and E. P. Lesley.
(Fourth Annual, 1918) --------------------- .15
64 Experimental Research on Air Propellers-III.
By Win. F. Durand and E. P. Lesley. (Fifth
Annual, 1919)---------------------------- .10
71 Slip-stream Corrections in Performance Com-
putation. By Edward P. Warner. (Fifth
Annual, 1919)---------------------------- .05
109 Experimental Research on Air Propellers-IV.
By Win. F. Durand and E. P. Lesley. (Sixth
Annual, 1920)---------------------------- .05
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
168 The General Efficiency Curve for Air Propellers.
By Walter S. Diehl. (Ninth Annual, 1923) - .05
' 175 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)-------------------
178 Relative Efficiency of Direct and Geared Drive
Propellers. -By Walter S. Diehl. (Ninth
Annual, 1923)---------------------------- .05
183 The Analysis of Free-flight Propeller Tests and
Its Application to Design. By Max M.
Munk. (Ninth Annual, 1923)-------------- .05
2 Out of print as a separate report. The annual volume containing this report is
still available.








26

PROPELLERS-Continued


Title


Price


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)-------------- $0. 10
Comparison of Tests on Airplane Propeller in
Flight with Wind-tunnel Model Tests on Simi-
lar Forms. By W. F. Durand and E. P. Les-
ley. (Eleventh Annual, 1925) -------------- 15
Interaction between Air Propellers and Airplane
Structures. By W. F. Durand. (Twelfth
Annual, 1926)---------------------------- .10
Tests on Thirteen Navy Type Model Propellers.
By W. F. Durand. (Twelfth Annual, 1926)--! .10
Characteristics of Propeller Sections Tested in
the Variable Density Wind Tunnel. By East-
man N. Jacobs. (thirteenth Annual, 1927)-- 10


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)--------


No.


2186


196

220


235

237


259


209

226

242


$0.05

.05

.10


2 Out of print as a separate report. The annual volume containing this report is
still available








27


STABILITY AND CONTROL

No. Title Price

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-I.
By E. B. Wilson. (Third Annual, 1917)---------
3 26 The Variation of Yawing Moment Due to
Rolling. By E. B. Wilson. (Fourth Annual,
1918)------------------------------------------
3 27 Theory of an Airplane Encountering Gusts-III.
By E. B. Wilson. (Fourth Annual, 1918) ....
95 Diagrams of Airplane Stability. By H. Bate-
man. (Sixth Annual, 1920) ---------------- $0. 10
2 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)- ... 10
3 120 Practical Stability and Controllability of Air-
planes. By F. H. Norton. (Seventh An-
nual, 1921)-------------------------------------
3153 Controllability and Maneuverability of Air-
planes. By F. H. Norton and W. G. Brown.
(Eighth Annual, 1922) ------------------- .05
172 Dynamic Stability as Affected by the Longitu-
dinal Moment of Inertia. By Edwin B.
Wilson. (Ninth Annual, 1923)------------- .05

1 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.
I 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.








28

STRENGTH OF CONSTRUCTION


No. Title Price

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)-----------------------
S 35 The Strength of One-piece, Solid, Built-up, and
Laminated Wood Airplane Wing Beams.
By John H. Nelson. (Fourth Annual, 1918)--------
2 76 Analysis of Fuselage Stresses. By Edward P.
Warner and Roy G. Miller. (Fifth Annual,
1919)------------------------------------------
S82 Airplane Stress Analysis. By A. F. Zahm.
(Fifth Annual, 1919)----------------------------
92 Analysis of Wing Truss Stresses. By Edward
P. Warner and Roy G. Miller. (Sixth An-
nual, 1920)-------------------------------------
104 Torsion of Wing Trusses at Diving Speeds.
By Roy G. Miller. (Sixth Annual, 1920)---- $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
2143 Analysis of Stresses in German Airplanes. By
Wilhelm Hoff. (Eighth Annual, 1922)-----------
161 The Distribution of Lift Over Wing Tips and
Ailerons. By David L. Bacon. (Ninth
Annual, 1923)---------------------------- .10
2 180 The Influence of the Form of a Wooden Beam
on Its Stiffness and Strength-I: Deflection of
Beams with Special Reference to Shear Def-
ormations. By J. A. Newlin and G. W.
Trayer. (Ninth Annual, 1923)-------------------
S181 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 0. W.
Trayer. (Ninth Annual, 1923)-------------------
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.
I 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.










STRENGTH OF CONSTRUCTION-Continued


No. Title Price

2188 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. W. Trayer. (Tenth Annual, 1924)----
214 Wing Spar Stress Charts and Wing Truss
Proportions. By Edward P. Warner
(Eleventh Annual, 1925)------------------ $0. 10
251 Approximations for Column Effect in Airplane
Wing Spars. By Edward P. Warner and
Mac Short. (Twelfth Annual, 1927)-------- 10


WIND TUNNELS AND LABORATORIES


44

72
2 73

274


98

146

195

227


The Altitude Laboratory for the Testing of
Aircraft Engines. By H. C. Dickinson and
H. G. Boutell. (Fourth Annual, 1918)-----
Wind-tunnel Balances. Bv Edward P. Warner
and F. H. Norton. (Fifth Annual, 1919) --....--
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-IL. By F. H. Norton and Ed-
ward P. Warner. (Sixth Annual, 1920)------
The Six-component Wind Balance. By A. F.
Zahm. (Eighth Annual, 1922) ------
Standardization Tests of N. A. C. A. No. 1
Wind Tunnel. By Elliott G. Reid. (Tenth
Annual, 1924)--------- --- --
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

.10


.10

.05

.10


I 10


I Out of print as a separate report. The annual volume containing this report i s
still available.


I










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
































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