Citation
List of reports with prices

Material Information

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

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:
This item is a work of the U.S. federal government and not subject to copyright pursuant to 17 U.S.C. §105.
Resource Identifier:
030814821 ( ALEPH )
10739617 ( OCLC )
Classification:
Z5063 .U64 ( lcc )
016.62913 U62 ( ddc )

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NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS





LIST OF REPORTS
WITH PRICES



EDITION MAY 1,1929


UNITED STATES
GOVERNMENT PRINTING OFFICE
WASHINGTON : 1929


















Digitized by the Internet Archive
in 2013












http://archive.org/details/listof1929unit















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.
(:ll)





















INDEX
Page
Annual reports------------------------------------ I
Bibliographies------------------------------------- 1
Technical reports---------------------------------- 3
Aerodynamics--------------------------------- 3
Airfoils and wing sections----------------------- 4
Airplanes-Full scale experiments ---------------- 7
Airplanes-Model experiments -----.... -------------- 9
Airships----------- --------------------------- 10
Engines and accessories------------------------- 11
Fuels ----------------------------------------- 18
Gases---------------------------------------- 19
Helicopters------------------------------------- 19
Instruments----------------------------------- 19
Materials_------------------------------------- 22
Meteorology------------- --------------------- 24
Miscellaneous --------------------------------- 25
Nomenclature--------------------------------- 25
Parachutes_----------------------------------- 25
Propellers -_---------------------------------- 26
Seaplanes------------------------- ---------- 28
Stability and control--------------------------- 2S
Strength of construction------------------------ 30
Wind tunnels and laboratories------------------- 31















NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICS


ANNUAL REPORTS

Year Price


First1 1915 With Reports Nos. 1-7--------
Second I- 1916 With Reports Nos. 8-12 ----
Third--- 1917 With Reports Nos. 13-23----- $1.50
Fourth -_- 1918 With Reports Nos. 24-50-----------
Fifth1 ----- 1919 With Reports Nos. 51-82------
Sixth 1 1920 With Reports Nos. 83-110-- -----
Seventh-- 1921 With Reports Nos. 111-132- -----
Eighth '_-- 1922 With Reports Nos. 133-158-1-------
Ninth 1--. 1923 With Reports Nos. 159-185------
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_ ------
Thirteenth._ 1927 With Reports Nos. 257-282_ - 1. 25

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 (1909-1916)----------
Bibliography of Aeronautics (1917-1919)-------------
Bibliography of Aeronautics (1920-1921)--- ----
Bibliography of Aeronautics (1922) -----
Bibliography of Aeronautics (1923), -------------
Bibliography of Aeronautics (1924)-________.____
Bibliography of Aeronautics (1925) ------ ---
Bibliography of Aeronautics (1926)----------------
.Bibliography of Aeronautics (1927)- -------------


$2. 00
.75
.35
.25
.25
25
.50
.20
.35











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
78 The Limiting Velocity in Falling from a Great
Height. By Edwin Bidwell Wilson. (Fifth
Annual, 1919) -----------------
8 79 Bomb Trajectories. By Edwin Bidwell Wilson.
(Fifth Annual, 1919) ----------- ---
S83 Wind Tunnel Studies in Aerodynamic Phe-
Snomena 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
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
8 151 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 EUlliott
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. 0., 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.
42476-29-2 (q)










AERODYNAMICS-Continued


No.


Title


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 Resumtm6 of the Advances in Theoretical
Aeronautics Made by Max M. Munk. By
Joseph S. Ames. (Eleventh Annual, 1925)---
247 Pressure of Air on Coming to Rest from Various
Speeds. By A. F. Zahm. (Twelfth Annual,
1926)-----------------------------------
3253 Flow and Drag Formulas for Simple Quadrics. '
By A. F. Zahm. (Twelfth Annual, 1927) ----.
287 Theories of Flow Similitude. By A. F. Zahm.
(Thirteenth Annual, 1927) ------------
289 Forces on Elliptic Cylinders in Uniform Air
Stream. By A. F. Zahm, R. H. Smith, and
F. A. Louden. (Fourteenth Annual, 1928)--
311 Aerodynamic Theory and Test of Strut
Forms-1I. By R. H. Smith. (Fifteenth
Annual, 1929)---------------------------

AIRFOILS AND WING SECTIONS


4 18 Aerofoils and Aerofoil Structural Combinations.
Combinations. By Lieut. Col. Edgar S.
Gorrell and Maj. H. S. Martin. (Third An-
nual, 1917)-------------- --------------
t 28 An Introduction to the Study of the Laws of Air
Resistance of Aerofoils. By George de
Bothezat. (Fourth Annual, 1918)--------------
$ 75 The Aerodynamic Properties of Thick Aerofoils
Suitable for Internal Bracing. By F. H.
Norton. (Fifth Annual, 1919) --------.....-
77 The Parker Variable Canmber Wing. By H F.
Parker. (Fifth Annual, 1919)-----------------
S93 Aerodynamic Characteristics of Airfoils. By
National Advisory Committee for Aero-
inalitics. (Sixth Annual, 1920)--.....--- ---.. -----
SOut of print. A v.'iilble is n spiirni e report for reference or loan in the Office of
Aeronaitiial Irinfelligiiv', N:.i ionil Ad visorv ( oinnii tee fur Aeronautics.
* Not issiiJd. as a s,,iiira,' reporr T'he :inri imi l volume containiDingR this report is
still avnil:bile.


Price


$0.05


.15

.05


.05


.05

.10








AIRFOILS AND WING SECTIONS-Continued

No. Title Price

3 111 The Variation of Airfoil Lift and Drag Coeffi-
cients with Changes in Size and Speed. By
W. S. Diehl. (Seventh Annual, 1921)--------------
3121 The Minimum Induced Drag of Airfoils. By
Max M. Munk. (Seventh Annual, 1921)------
124 Aerodynamic Characteristics of Airfoils-II.
By the National Advisory Committee for
SAeronautics. (Seventh Annual, 1921) --------$0. 10
3142 General Theory of Thin Wing Sections. By
Max M. MLunk. (Eighth Annual, 1922)-- ----
3150 Pressure Distribution over Thick Aerofoils-
Model Tests. By F. H. Norton and D. L.
Bacon. (Eighth Annual, 1922)--- ____-
2152 The Aerodynamic Properties of Thick Aero-
foils-If. By F. H. Norton and D. L. I
Bacon. (Eighth Annual, 1922)--------------
2169 The Effect of Airfoil Thickness and Plan Form I
on Lateral Control. By H. I. Hoot. (Ninth
Annual, 1923) ---------------------------- 05
182 Aerodynamic Characteristics of Airfoils-III.
By the National Advisory Committee for
Aeronautics. (Ninth Annual, 1923) --------- 15
2 191 Elements of the Wing Section Theory and of the
Wing Theory. By Max M. Munk. (Tenth
Annual, 1924) -------------------------
200 Some Problems on the Lift and Rolling Mo-
ments of Airplane Wings. By Jas. B. Scar-
borough. (Tenth Annual, 1924) ------------ 10
2201 The Effects of Shielding the Tips of Airfoils.
By Elliott G. Reid. (Tenth Annual, 1924)----
207 Aerodynamic Characteristics of Airfoils at High
Speeds. By L. J. Briggs, G. F. Hull, and
H. L. Dryden. (Tenth Annual, 1924)------- 10
217 Preliminary Wing Model Tests in the Variable
Density Wind Tunnel of the National Advi-
sorv Committee for Aeronautics. By Max M.
Munk. (Eleventh Annual, 1925) ------------ 10
221 Model Tests with a Systematic Series of 27
Wing Sections at Full Reynolds Number.
By Max. M. Munk and Elton WV. Miller.
(Eleventh Annual, 1925) ------------------i 10
2 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 t lie Office
of Aeronautical Intelligence, National Advisory Committee for Aeronmitics.










AIRFOILS AND WING SECTIONS-Continued

No. Title Price

229 Pressure Distribution Over Thick, Tapered Air-
foils, N. A. C. A. 81, U. S. A. 27 C Modified
and U. S. A. 35. By Elliott G. Reid.
(Eleventh Annual, 1925) ------------------- $0. 10
233 The Aerodynamic Characteristics of Seven Fre-
quently Used Wing Sections at Full Reynolds
Number. Bv Max M. Munk and Elton W.
Miller. (Twelfth Annual, 1926)------------ 1. 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. Bv L. J. Briggs and H. L. Dryden.
(Twelfth Annual, 1927)-_ --_ .15
267 Drag of Wings with End Plates. Bv Paul E.
Hemke. (Thirteenth Annual, 1927)------- .10
271 Pressutre 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
Hlandley-Page Control Surfaces. By R. H.
Smith. (Thirteenth Annual, 1927)-------- .10
2S5 A Study of Wing Flutter. By A. F. Zahmi and
R. 1. Bear. (Fourteenth Annual, 1928)_... 15
286 Acrodynamrnic Characteristics of Airfoils-V.
By National Advisory Committee for Aero-
nautics. (Fourteenth Annual, 1928) -.----- 25
288 Pressure Distribution Over a Rectangular Mono-
pilane Wing Model up to 90 Angle of Attack.
Bv Nlontgoinery Knight and Oscar Loeser, jr.
(F'ourteenth Annual, 1928).-...-.---------- 10
309 Joint, Report on Standardization Tests on
N. P. L. R. A. F. 15 Airfoil Model. Bv
Walter S. Dielil. (Fifteenth Annual. 1929)---. 10
312 Tlhe Prediction of Airfoil Characteristics. BY
eorge J. 1tiggins. (Fifteenth Annual, 1929)_ 10
315 Aerody namic Characteristics of Airfoils-VI.
By th le National Advisory Committee for
Aeronautics. (Fifteenth Annual, 1929)----I 20








AIRPLANES-FULL-SCALE EXPERIMENTS


No. Title Price

3 69 A Study of Airplane Ranges and Useful Loads.
By J. C. Coffin. (Fifth Annual, 1919) --- ------
8 70 Preliminary Report on Free Flight Tests. By
Edward P. Warner and F. H. Norton. (Fifth
Annual, 1919)----------------------------------
105 Angles of Attack and Air Speeds During Maneu-
vers. By Edward P. Warner and F. H.
Norton. (Sixth Annual, 1920) ------------- $0. 05
118 The Pressure Distribution Over the Horizontal
Tail Surfaces of an Airplane. By F. H. Nor-
ton. (Seventh Annual, 1921)-------------- 15
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) -- -- -- -- --- ---- -----
3149 Pressure Distribution Over the Rudder and Fin
of an Airplane in Flight. By F. H. Norton
and W. G. Brown. (Eighth Annual, 1922) ---
154 A Study of Taking Off and Landing an Airplane.
By T. Carroll. (Eighth Annual, 1922) ----- .05
155 A Study of Airplane Maneuvers with Special
Reference to Angular Velocities. By H. J.
E. Reid. (Eighth Annual, 1922) -------. 05
162 Complete Study of the Longitudinal Oscillation
of a VE-7 Airplane. By F. H. Norton and
W. G. Brown. (Ninth Annual, 1923)------- .05
163 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
167 The Measurement of the Damping in Roll on a
JN4H in Flight. By F. H. Norton. (Ninth
Annual, 1923)---------------------------- .05
170 A Study of Longitudinal Dynamic Stability in
Flight. By F. H. Norton. (Ninth Annual,
1923)---------------------------------- 05
173 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
174 The Small Angular Oscillations of Airplanes in
Steady Flight. By F. H. Norton. (Ninth
Annual, 1923)---------------------------- .05
Out of print. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










AIRPLANES--FULL-SCALE EXPERIMENTS-Continued

No. Title Price

2 192 Charts for Graphical Estimation of Airplane
Performance. Bv Walter S. Diehl. (Tenth
.Annual, 1924).. -........ .. ........ .....-,.....
2193 Presrc DI)istribution Over the Wings of an
NMB-3 Airplane in Flight. By F. H. Norton.
(Tenth Annual, 192.1) __- _ _ _
194 Investigation of Slip Stream Velocity. By J. W.
Crowlev, jr. (Tenth Annual, 1924)--------- SO. 05
203 Accelerations in Flight. By J. H. Doolittle.
(Tenrth Anlnual, 1924) --------------------- .10
219 S(ome Aspects of the Comparison of Model and
Full-scale Tests. By D. W. Taylor. (Elev-
1enth .Annal, 1925) ------------------------ 10
22S A Study of the Effect of a Diving Start on Air-
plane Speed. By W\alter S. Diehl. (Eleventh
Annual, 1925)._ ---------------------------- .05
234 Three Methods of Calculating Range and En-
(ldurance of Airplanes. By Walter S. Diehl.
(Twelfth Annual, 1926)-------------- 10
238 The Effect of Flight Path Inclination on Airplane
Velocity. By Walter S. Diehl. (Twelfth
Annual, 1926 --------------------------- .05
249 A Comparison of the Take-off and Landing
Characteristics of a Number of Service Air-
planes. By Thomas Carroll. (Twelfth An-
1nual, 1927)------------------------------ 10
257 Pressuire 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)---.----------------------------- 15
265 A Full-Scale Investigation of Ground Effect.
Bv Elliott G. Reid. (Thirteenth Annual,
1927)------------------------------------ .05
297 The Reduction of Observed Airplane Perform-
ance to Standard Conditions. By Walter S.
Diehl. (Fourteenth Annual, 1928)---------- 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
2 Out or print as a separate report. The annual volume containing this report
Is still av:altable








AIRPLANES-FULL-SCALE EXPERIMENTS-Continued


Title


Price


No.

307


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


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)---- $0. 10

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
Preliminary Experiments to Determine Scale
and Slip Stream Effects on a 1/24 Size Model
of a JN4H Biplane. By D. L. Bacon. (Sev-
enth Annual, 1921) ------------------------ 05
The Tail Plane. By Max M. Munk. (Eighth
Annual, 1922) -----------------------------. 10
Damping Coefficients Due to Tail Surfaces in
Aircraft. By Lynn Chu. (Eighth Annual,
1922)------------------------------------ .05
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
Lift and Drag Effects on Wing Tip-rake. By
A. F. Zahm, R. M. Bear, and G. C. Hill.
(Eighth Annual, 1922)--------------------- .05
Some Aspects of the Comparison of Model and
Full-scale Tests. By D. W. Taylor. (Elev-
enth Annual, 1925)------------------------ 10
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
Tests on Airplane Fuselages, Floats, and Hulls.
By Walter S. Diehl. (Twelfth Annual, 1926)_-- 15
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


3 74


119


122


133

136

137

140

219

225


236

254


Office








10

AIRPLANES-MODEL EXPERIMENTS-Continued


Title


The Air Forces on a Systematic Series of Biplane
and Triplane Cellule Models. By Max M.
Munk. (Twelfth Annual, 1927)------------
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)----------------------------
Air Force and Moment of N-20 Wing with Cer-
tain Cut-outs. By R. H. Smith. (Thir-
teenth Annual, 1927)-------------------
Air Force Tests of Sperry Messenger Model
with Six Sets of Wings. By James M. Shoe- I
maker. (Thirteenth Annual, 1927)---------
Wind Tunnel Tests on Autorotation and the
"Flat Spin." By Montgomery Knight.
(Thirteenth Annual, 1927)----------------
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)------
Pressure Distribution Tests on PW-9 Wing
Models from -18 through 90 Angle of At-
tack. By Oscar E. Loeser, jr. (Fourteenth
Annual, 1928) --------------------


AIRSHIPS


Bending Moments, Envelope and Cable Stresses
in Nonrigid Airships. By C. P. Burgess.
(Seventh Annual, 1921)-- *.-------
The Drag of Zeppelin Airships. By Max M.
Munk. (Seventh Annual, 1921)______
The Drag of "C" Class Airship Hull with Vary-
ing Lengths of Cylindric Midships. By A. F.
Zahm, R. H. Smith, and G. C. Hill. (Eighth
Annual, 1922) .------------------
The Inertia Coefficients of an Airship in a Fric-
tionless Fluid. By H. Bateman. (Ninth
Annual, 1923)-_ ..-
The Aerodynamic Forces on Airship Hulls. By
Max M. Munk. (Ninth Annual, 1923)-----


No.


256

260


266

269

273

279


296


Price


$0. 15


.10

05

610

.10


.15


.15


115


117

138


164

184


$0.05

.05


.05

.05


.10








A I RS HIPS -Continued

No. Title Price
__ _________________|_____
204 Forces on Airships in Gusts. By C. P. Burgess.
(Tenth Annual, 1924) ---------------------- $0. 05
208S Determination of the Turning Characteristics of
an Airship by Means of a Camera Obscura.
Bv 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
SAnnual, 1925)----------------------------I .05
211 Water Model1 Tcsts for Semirigid Airships. By
L. B. Tuckerman. (Eleventh Annual. 1925)__ 05
212 Stability Equations for Airship Hulls. By A. F.
SZahm. (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

ENGINES AND ACCESSORIES

1 7 Thermodynamic Efficiency of Present Types of
Internal Combustion Engines for Aircraft.
I By Columbia University. (First Annual,
1915)---------------------------------------
Part 1. Review of the Development of
Engines Suitable for Aeronautic Service.
Part 2. Aero Engines Analyzed with Refer-
ence to Elements of Process or Function.
S10 Mufflers for Aeronautic Engines. By Prof. H.
SDiederichs and Prof. G. B. Upton. (Second
Annual, 1916)---------------------------------
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)------------------------------
I Out of print. Annual volume available for reference or loan in the Office o
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash.
ington, D. C., and in the libraries of large cities.
42476-29- 3










ENGINES AND ACCESSORIES-Continued

No. Title Price

4 23 Aercnautic Poxer-plant Investigations. By
tlhe S)ubcommittee on Power Plants. (Third
A.nnual. 1917)-----------------------
Part 1. Performance of Aeronautic En-
gines at High Altitudes.
Part 2. Radiator Design.
Part 3. Spark Plugs.
3 24 Air Flow Thlrough Poppet Valves. By G. W.
Lewis and E. M. Nutting. (Fourth Annual,
1918)--------------------------------------
3 43 Synop.-is of Aeronautic Radiator Investigations
for the ears 1917 and 191S. Bv R. V. Klein-
schmidt. (Fourth Annual, 1918)
3 45 Effect of Compres.ion Ratio, Pressure, Tem-
perature, and Humidity on Power. (Fourth
A.inu1al, 1918)---------------
Part 1. Variation of Horsepower with
Altitude and Compression Ratio. By
H. C. Dickinson, W. S. James, and G. V.
Andcr..on.
Part 2. Value of Supercharging. By H. C.
Dickinson and G. V. Anderson.
Part 3. Variation of Horsepower with
Temperature. By I1. C. Dickinson,
\W. S. James, and G. V. Anderson.
Part 4. Influienice of Water Injection on En-
g-ine Performance. By V.W. Brinkerhoff.
3 46 A Study of Airplane Eiigiie Tests. By V. R.
Gage. "Fouirth annualal, 191S)----------------
a 48 Carbureting Conditions Characteristic of Air-
craft Engines. By P. S. Tice. (Fourth
Annual, 1918)----------------------------------
3 4) M.vtering Characteristics of Carburetors. By
P. S. Tierc. (Fourth A.iiual, 191,)_S).
1 Out ipf pIint :vi i hi ,ic i i as iiraio reppi'url fir nrftrenee or loan in the 0111ce
Of A or, iii icil iit1iflliciice. N:ilt iil A 'luury C'iminil lee for Aeronautics.
SN-t i-ii'l i'I :i : l.ir.it. rt'lijrl. TI' annual vulunl containing this report
as tnill :iv.il:il'lh










ENGINES AND ACCESSORIES-Continued

No. Title Price

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
a 53 Properties and Preparation of Ceramic Insula-
tors for Spark Plugs. (Fifth Annual, 1919)---------
Part 1. Methods of Measuring Resistance
of Insulators at High Temperatures.
By F. B. Silsbee and R. K. Honamnan.
Part 2. Electrical Resistance of Various In-
Ssulating Mlaterials at High Temperatures.
By R. K. Honaman and E. L. Fonseca.
S Part 3. Preparation and Composition of
Ceramic Bodies for Spark-plug Insula-
tors. By A. V. Bleininger.
Part 4. Cements for Spark-plug Electrodes.
By H. F. Staley.
54 Effect of Temperature and Pressure on the
Sparking Voltage. By F. B. Silsbee and L.
B. Loeb. (Fifth Annual, 1919) ------------- .05
55 Investigation of the Muffling Problem for Air-
plane Engines. By G. B. Upton and V. R.
Gage. (Fifth Annual. 1919) ---------------- 10
8 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.
3 57 The Subsidiary Gap as a Means for Improving
Ignition. By W. S. Gorton. (Fifth Annual,
1919) ----- ------------ -- -
Out of print. Available as a separate report for 'o e-r tn(ce or lo:in in lit-Offlce
of Aeronautical Intelligence, National Advisory Committee for Aeruon.iutics.








14

ENGINES AND ACCESSORIES-Continued

No. Title Prhi L

5s Clia-ract criit ic-' Cf I igh-tension .'Magnetos.
I.Filti Aril. 1919)- ------------------- SO. 10
Part 1. C'vele of Operation of Jump-spark
Ignitio-,1 Sy'stem1s. Iy F. B. Silsbee.
Part 2. Trarinsformiattioii Ratio anld Conupling
in Iii.li-teiision 'Magnetos. By F. B.
.il- i i,.
59 Ginor:l A.iml:lvsis of Airplane Radliat or Prollemis.
Byv H. C. Dickinsmri, W. S. Jamones. and R. V.
KlIcillhiliidt. (Fifth An.\ill, 1919 --- 05
i)0 GC-'iT'rtl Di-triiui,)l If T'ot N. tlilorls for Radi-
:iior.. B\ 1I. C. D)ickiiison, \V. S. .Janmes, nnd
\V. B. Broit, (Fiftlh A1uiiii:tl. 19190) --------- 10
6l H1i R. c ,ie.imcl e D)ue to Hia'liators. (Fifth
Ai11ul. 191.))---------------------------- 10
Part 1. lle:i'l Ii'-i-t:,iiic of o R:aliator ('ores.
BYv R. V. KI-ciii-linimit mir.1 S-. R. Ir~on.
Part 2. Pr'iiiiiiiiary Rejort oi Pei.?taiive
Di,' to No-c IRaliatior. ]BY It. V. Kle'in-
hin idt.
Pairt 3. lE'f'te't of Strieamlhinci (C'-iinti for
l'rvv-,-;ir RM li:ifors-. B\ S. R. '.i .
t;2 IfTet't if A\ititule on I atili:ilmr Pcirfriiiinie.
B v \W S. J:1111-4 n d ,;nn RL I.i-i'. i Ff th1
.\Aiii:i11. 1019) ---------------------------- .10
63 IResult- ,I, Tc -,t' 1 ,n Rni liitor-.- fmr .\irvr:ft l'ii-
Si,-. I Flillli .I\I k [ 1 19 1 i. .. 10
P':irt 1. Il':it D)i--1,il ioln (f H iLitors. BY\
II. C D)ickiii..o W. V. .L1 iIIs, 1n1d R. V.
W rill-.1lllifilt.
Part 2. W;>aIr Filo\w tiroiifli R;adiator
Cr r-. Iy WV. S. J.:me-.
sNj Il ^Dprt i' ,. S[). 'i:tl i"' i ,f l;na liators. Bv
1%. i;. 1~r> iSi\th A 111111,l, 0 ` '- --------.. 10
S,7 l 'rf'rl (- f `6;1 1ir' Pi, rli,, r ,.,., }\\ S. l{. P'.'ir- l,( i- :inn l 1 V .
I, ll>'iii- ',iill S.S i\(10 A 1\ 1111:1l, 1 ),-------- 05
SS Plrc.--ir 1)rI> iln MR:li:ti,,r Air T'Uls. Bv S. It.
I' -.ii,-.. ,Sitl .\tiA ii 1 2I- --- -------------- .05
101 I'Th'( Cal, iil' :t1'dl P'rforitii 'icc If Airplanes I
1I (I ii ,pil \ it S. I Si tiip .'.riirlinI:l l iili7cs. \I
E *. U 1%'vm 1,1(-(. i Sixtli A iinim ]i, *'l' i... 15








ENGINES AND ACCESSORIES-Continued

No. Tit le Price

$102 Performance of a Liberty 12 Airplane Engine.
By S. WV. Sparrow and H. S. White. tSixth
Annual, 1920)----------------------------------
3103 Performance of a 300-horsepower Hispano-
Suiza Airplane Engine. By S. W. Sparrow
and H. S. White. (Sixth Annual, 1920)-----
106 Turbulence in the Air Tubes oif Radiators for
Aircraft Engines. By S. R. Parsons. (kSixth
Annual, 1920)---------------------------- -'0. 05
108 Some Factors of Airplane Engine Performance.
By Victor R. Gage. (Si\th Annual. 1920)---' 10
3 123 Simplified Theory of the Magneto. Bv F. B.
SSilsbee. (Seventh Annual, 19211_--------------
3134 Performance of Mavbach 300-horsepower Air-
Splane Engine. By S. WV. Sparrow. (Eighth
i Annual, 1922) -- --------------- --- -- -
135 Performance of B. M. W. 1S5-horsepower Air-
Splane Engine. By S. W. Sparrow. iEiihthi
I Annual, 1922' -------- -------------------- .05
3158 Mathematical Equationis for Head Conduction
in the Fins of Air-cooe-d Engine-. BY D. R.
Harper a',d WV. G. Bruwnn. ,Eiglith Annual,
S1922)------------- ------- ------------
3 159 Jet Propulsion for Airplanees. By Edgar Buck-
inghamni. (.Ninth A.nnual, 192:3)------------ ------
3 171 Engi;ie Performance and the Determination of
Absolute Ceiling. By Walter S. Diell.
(Ninth Annual, 1923)-------------------------
179 The Effect of Electrode Temperature on the
Sparking Voltage of Short Spark Gaps. By
F. B. Silsbee. (Ninth Annual, 1923) ------- .05
2 -'187 Flame Speed and Spark Intensity. By D. W.
Randolph and F. B. Silsbec. (Tenth Annual,
1924)- ------ -- ----- ------
2189 Relation of Fuel-air Ratio to LEngine Perform-
anlce. Bv Stari wood W. Sparrow. (Tenth
Annual, 1924) ------- ---.------ ----- ------.
190 Correcting Horsepower Measurements to a
Standard Temperat tire. By Stanwood W.
Sparrow. (Tenth Annual, 1924) ----------- .05
2 Out of print as a separate report. The annual volume cont.mni n this report
is still available.
. 3 Out of print. Available as a *ep:iratt rpiori ftor r f tillii li i:-n in thr 1 Ulfice of
Aeronautical Intelligence, N.iti'iil .\Al i-i)v, ('iim niii ht for .\rilliuTi (<.-.








16

ENGINES AND ACCESSORIES-Continued

No. Title Price

202 The Sparking Voltage of Spark Plugs. By F.
B. Silsbee. (Tenth Annual, 1924) ---------- $0.05
205 The Effect of Changes in Compression Ratio
upon Engine Performance. By Stanwood
W. Sparrow. (Tenth Annual, 1924)--------- .10
222 Spray Penetration with a Simple Fuel Injection
Nozzle. Byv Harold E. Miller and Edward
G. Beardsley. (Eleventh Annual, 1925)----- 05
224 An Inve.tigation of tlie ('ueflficienit of Discharge
of Liquids Through Snmall 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. (Eleventlh Annual, 1925)... 10
239 Power Output andl Air Requirements of a Two-
stroke Cycle Engine for Aeronautical Use.
Bv C. i. Paton alnd Carlton Kemper.
(Twelfth Annual, 1926) --------------------. 10
241 Electrical Characteristics of Spark Generators
for Automotive Ignition. By R. B. Brode,
D. Wit Ranidolph, and F. B. Silsbee. (Twelfth
Annual,) 1926) ----------------------------. 15
243 A Preliminary Study of Fuel Injection and Cornm-
p)resiori Ignition as Applied to an Aircraft
Engine Cylinder. By Arthur W. Gardiner.
(Twelfth Annual, 1926)------------------- 10
250 Description of the N. A. C. A. Lliiversal Test
Engine and Some Test Results. By Marsden
Ware. (Twelfth Annual, 1926) -------------. 10
252 The Direct Meastiremnient of Engine Power on an
.Airplane in Flight with a Hub Type Dvna-
1 ,onieter. By WV. D. Gov\e and M. W. Green.
'Twvelfth Annual, 1927 ---------------- .10
258 S mne Faictors .'IfT(ctiiig the Rlprid)(Iticibility of
Pciitrati, andl the 'Cut-ciff ,f ( )il Sprays for
i Ful Innjection Engines. B1 -E. G. Beardslev.
(Tirtiet Axnmumal, 1927) ..-------------- -. 05
261 vR..-i-tan(c and (', ling I',,wer if \a rio s Ra(lia-
tors. B\ H. 11. .Smith. (Thirtcenuth Annual,
1927) ------------------------------------. 10
262 lFricti i of Aviiation Engine-. iBy S. \V. Spar-
row and l M. A.\. 'ThornC. Tlirt 1927, ........----------------------------------i 10










ENGINES AND ACCESSORIES-Continued

No. Title Price

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)------------------ $0. 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
276 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 Tem-
peratures. By Arthur W. Gardiner and Oscar
W. Schey. (Thirteenth Annual, 1927)----- 10
280 The Gaseous Explosive Reaction-The Effect of
Inert Gases. By F. W. Stevens. (Thirteenth
Annual, 1927)- ----------------------------. 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. Schev. (Fourteenth
Annual, 1928)---------------------------- 10








is

ENGINES AND ACCESSORIES-Coinu iied

No. Titie Price

24 1 Tlhe Cniparative Performance of Roots Type
.Aircrft Engine Sup)erchargers ac, Affected by
(iCliatge in Iml)-Iler Speed and Displacement.
I Bv Mar-dei \arv and Erne.-t E. Wilson.
I Ii',iirlte'lth Ai.al, 192s)--____-------. $0so. 10
294 The Mv1a.-iireiiient of M:xizinum Cylinder Pres-
1 inr-. By ClIeLt'r W. Hflicks. (Fourteenth
A.Iiia l. 192S) ---------------------------- 15
295 'TI' VaLriliti-i in Eni iiie Power \ith Altituide
DLOtIIIiiii1inl frOui i Measiircienicts with a Hub)
D n;vii.onitieter. Bv W. D. Guve. (Four-
t'enthl Aninual. 192S) --------------------- .10
303 XA-I iiIvestigatiol ,f ile I'Us of Dischlarge Valves
.an1d a'I Intake Control for Improving the Per-
Ifori4Ntitc of N. A. C. A. Roots Type Super-
chLarger. By O.:car W. Scliev and Ernest E.
Wilson. ( IFoirteenth Annual. 1928)......----- 10
313 Drag anId( Cmioliiig witl \'Various Forins of Cowl-
1tig for a '"Whirlwind" Radial Air-Cooled
Engine-T. By Fred E. Weick. (Fifteenth
.\| nual, 1929) ---------------------------- 15
314 Drag atmd Cooling with Various Forms of Cowl-
iug for a "'Whirlwind" Radial Air-Cooled
Engin(e-II. By Fred E. Weick. (Fifteenth
Annuuald, 1929)---------------------------- .20

FUELS

42 A New Proces.s for the Production of Aircraft-
engine Fuels. By Auguste Jean Paris, jr.,
awd W. Francklvn Paris. (Fourth Annual,
1918)---------------------------------- $0.05
47 Power Characteristics of Fuels for Aircraft
Enrigines. (Fourth Aninal, 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.










FUELS-Continued

No. Title Price

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)------------------------------------ $0.05
90 1 Comparison of Hector Fuel with Export Avia-
tion Gasoline. By H. C. Dickinson, V. R.
Gage and S. W. Sparrow. (Sixth Annual,
1920)----------------------------- ------ .05
232 Fuels for High-compression Engines. By Stan-
wood W. Sparrow. (Eleventh Annual, 1925)-- 10
305 The Gaseous Explosive Reaction-A Study of
the Kinetics of Composite Fuels. By F. W.
Stevens. (Fourteenth Annual, 1928) -------- .15

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
Annual, 1918)---------------------------- $0. 15
41 Testing of Balloon Gas. By Junius David
Edwards. (Fourth Annual, 1918)----------- .05

HELICOPTERS

S80 Stability of the Parachute and Helicopter. By
H. Bateman. (Fifth Annual, 1919)

INSTRUMENTS

1 2 Investigation of Pitot Tubes. (First Annual,
1915)----------------------------------------
Part 1. The Pitot Tube and Other Anemom-
eters for Airplanes. By W. H. Herschel.
Part 2. The Theory of the Pitot and Venturi
Tubes. By E. Buckingham.
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. Available as a separate report for reference or loan in the Office
of Aeronautical Intelligence, National Advisory Committee for Aeronautics.










INSTR U M ENTS-Cont inued

No. Title Price

1 8 General Specifications Covering Requirements
of Aeronautic Instruments. By the National
Advisory Committee for Aeronautics. (See-
ond Annual, 1916)------------------------
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 Acceleromcter Design. By F. II. 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 iM. D. Hersey, F. L. Hunt, and H. N.
Eaton. (Sixth Annual, 1920)----- ---------- .10
125 Aeronautiic Instruments: Section I-General
Classification of Instruments and Problems
Including Bibliography. Bv 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.
I Out of print. Annual vulmnc available for reference or loan in the Offlice of
AeronfnIr n(.cIl In:i1liiiwme, N' ilrtioal Advit;ory Committee for Aeronautics, Wash-
ington, D. C., unil in the li braries. of large cit ie;.










INSTRUMENTS-Continued

No. Title Price

127 Aeronautic Instruments: Section III-Aircraft
SSpeed Instruments. By Bureau of Stand-
I ards. (Seventh Annual, 1921) -------------- $0. 10
Part 1. Air Speed Indicators.
Part 2. Testing of Air Speed Meters.
Part 3. Principles of Ground-speed In-
struments.
128 Aeronautic Instruments: Section IV-Direc-
tion Instruments. By Bureau of Standards.
(Seventh Annual, 1921) -------------------- 15
S Part 1. Inclinometers and Banking Indi-
I cators.
S 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-
Splant 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.
Part 4. Air-pressure and 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. Bv 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-II.
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
M. D. Hersey. (Ninth Annual, 1923)------ .10










INSTRUMENTS-Continued

No. Title Price

166 The Aerodynamic Plane Table. By A. F.
Zahm. (Ninth Annual, 1923) ----------- $0.05
176 A Constant-pressure Bomb. By F. W. Stevens.
(Ninth Annual. 192:3) ---------------------- .05
198 Astronomical Methods in Aerial Navigation.
By K. Hilding Beij. (Tenth Annual, 1924).-..
199 Interference Tests on an N. A. C. A. Pitot Tube.
Bv Elliott G. Reid. (Tenth Annual, 1924)__. .05
206 NXnnmeta'lic Diaphragms for Instrumnents. By
H. N. Eaton and C. T. Buckingham. (Tenth
SAnnual, 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. Bv Paul E.
Hemke. (Thirteenth Annual. 1927)--------- .10
299 Investigation of Damping Liquids for Aircraft
Instruments. By G. H. Keulegan. (Four-
teenth Annual, 1928)---------------------- 10
310 Pressure Element of Constant Logarithmic
Stiffness for Temperature Compensated Alti-
meter. By W. G. Brombacher and F.
Cord(lero. (Fifteenth Annual, 1929) --------- 10

MATERIALS

S5 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 Annmual, 1915)...
Part 1. Balloon and Airplane Fabrics. By
Willis A. Gibbons and Omnar H. Smith.
Part 2. Skin Friction of Various Surfaces
in Air. By Willis A. Gibbons.
I Out of print. Annual volume available for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics, Wash-
ington, U. C., and in the libraries of large cities.










MATERIALS-Continued

No. Title Price

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.
33 Self-luminous Materials. By N. E. Dorsev.
(Fourth Annual, 1918)--------------------- $0. 05
3 34 Aluminum and its Light Alloys. By Paul D.
Merica. (Fourth Annual, 1918)------------------
236 The Structure of Airplane Fabrics. By E.
Dean Walen. (Fourth Annual, 1918)------------
3 37 Fabric Fastenings. By E. Dean Walen and R.
T. Fisher. (Fourth Annual, 191S)---------------
3 38 Airplane Dopes and Doping. By W. H. Smith.
(Fourth Annual, 191S)-------------------------
39 The Testing of Ba]loon 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. Tienman. (Fifth Annual, 1919)-----'. 10
3 66 Glues Used in Airplane Parts. By S. W. Allen
and T. R. Truax. (Fifth Annunl, 1919)_ ------
367 Supplies and Production of Aircraft Woods.
By W. N. Sparhawk. (Fifth Annual. 1919)_------
68 The Effect of Kiln Drying on the Strength of
Airplane Woods. Bv T. R. C. Wilson. Fifth
Annual, 1919) ---------------------------- .15
I Out of print. Available as a separate report for reference or loan in the Office of
Aeronautical Intelligence, National Advisory Committee for Aeronautics.
I Not issued as a separate report. The annual volume containing this report is
still available.










MIATERIAI.S-Cunt inueil

No. Title Price

1 84 Data on the Design of Plywood for Aircraft.
By Armin Elmiendorf. c Sixth Annual, 1920)----
3 85 Moisture Resistant Finishes for Airplane Woods.
By. M. E1. Dunlap. ( Sixth Annual, 1920)--
3145 Internal Stresses in Laminated Construction.
By A. L. Heim, A. C. Knauss, and Louis Seut-
ter. (Eighth Annual, 1922)...- - - - -
248 The Corrosion of Iagncsihim and of the Mag- |
nc.iiumn Aluninuiim .llovs Containing Manga-
nese. By J.A. Boyer. (Twelfth Annual, 1926). $0. 20

METEOROLOGY

1 4 Preliminary Report on the Problem of the At-
nmosphelre in Relation to Aeronautics. By
Prof. Charles F. Marvin. (First Annual,
1915)---------------------------------------
13 IMeteorology and Aeronautics. By Win. R.
Blair. (Third Annual, 1917) -------------- $0. 10
Part 1. Phyvsical Properties and Dynamics
of the Atmniosphere.
Part 2. Topographic and Climatic Factors
in Relation to Aeronaultics.
Part 3. Current Meteorology and Its Use.
147 Standard Atlmosphliere. By Willis Ray Gregg.
(Eighth Annual, 1.122)1 -- --_------ .05
2216G Thie Reduction of Airplane Flight-test Data to
Standard Atmosphere Condlitions. B'y Wa-
ter S. I)iell and E. P. Lesley. (Elevent i n-
minual, 1925 .-..-----------..---..-----------
218 StaLInlard. Atmlosp.iere lTailes and Data. By
Walter S. Dielil. (E:leve ith Annimal, 1925)- . 10
245 I vete Ir, l rgical I Condlitionis along Airwavs. By
W. R. (;regg. (Twelfth Annual, 1926) ----- 10
246 Tald1.s fur (C'alilr:Lting Altinmetters and Com-
pulting Altitudls lBased on the Standard At-
1 losplvire. By \W (i. G Broumichecr. (Twelfth
1 Annual, 192(i) ------- --------------- 10

I OuIt (f iriinl. A k111111.i1 \,'iiii :i\f:l:ilih for rwft'ni rce or loin in lile office of
A rriiii; l .ic:il IrilllieLr iii-.. N:iliii.il .\uvi'i.-.ir. (C' iiiilIll c' for Aeruonautis', W ash-
invlti l, I). C"., 1i ll In Ilir lilhr.ll-r of hlri.p rIlnv.:
a Out ior prilnt as a sL|.iiitod ri-purt. Th, niniual volunm' cuntnining this report
IS Still riV ll:lh,.
A Out (iof print A i;mill'Ih ar i: seii:i ttiP r" 'i r ri, r r efr cii' or lonn in thile Office
of AeTr,,nti u i l i Inl t llitince, N:!itli uii Ailv'.siry ((',nilitt for Aeronautics.








25


MISCELLANEOUS


Title


Price


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

NOMENCLATURE


89


2 15


' 25


91


2157


240


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)------------------
Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Sixth Annual, 1920) ----------------------
Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Eighth Annual, 1922)--------------------
Nomenclature for Aeronautics. By the Na-
tional Advisory Committee for Aeronautics.
(Twelfth Annual, 1926)--------------------
NOTE.-Reports 9, 15, 25, 91, 157 are obso-
lete.


$0. 15


.20


PARACHUTES


8 80 Stability of the Parachute and Helicopter. By
H. Bateman. (Fifth Annual, 1919)---------------

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.Aeronauticnl Intelligence, National Advisory Committee for Aeronautics.


No.


308








26

PROPELLERS

No. Title Price

2 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.
1 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 Wm. F. Durand and E. P. Lesley.
(Fourth Annual, 1918)--------------------------
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 Cornm-
1)utation. By Edward P. Warner. (Fifth
Annual, 1919)-------------------- ------- .05
2s109 Experimental Research on Air Propellers-IV.
By Win. F. Durand andlI E. P. Leslcv. (Sixth
Annual, 1920)--------------------------------
113 Tests on Air Propellers in Yaw. By Wm. F.
Duiranmd and E.P. Leslcy. (Seventh Annual,
1921)------------------------------------ .10
2 Out of print as a sepi.Lraitl report. The :tini:il volume containing this report Is
*t lll !lV~ll tl(h..
I Out of print. Av. ilihli,' : :i speimrath' repoiL for rft'irc1ne or loan in the Office
-of Atroriiut ical Iflnt ligyiriic, N.lirim;l Altvisljry (,Commt iltt'e for Aeronautics.










PROPELLERS-Continued

No. Title Price

141 Experimental Research on Air Propellers-V.
By Win. F. Durand and E. P. Lesley. (Eighth
Annual, 1922)---------------------------- $0.15
S168 The General Efficiency Curve for Air Propellers.
By Walter S. Diehl. (Ninth Annual, 1923)------
8 175 Analysis of W. F. Durand's and E. P. Lesley's
Propeller Tests. By Max M. Munk. (Ninth
Annual, 1923)----------------------------------
3177 The Effect of Slip-stream Obstructions on Air
Propellers. By E. P. Lesley and B. M.
Woods. (Ninth Annual, 1923)-------------------
3 178 Relative Efficiency of Direct and Geared Drive
Propellers. By Walter S. Diehl. (Ninth
Annual, 1923)----------------------------------
183 The Analysis of Free-flight Propeller Tests and i
Its Application to Design. By Max M.
Munk. (Ninth Annual, 1923)--------------- .05
2186 Application of Propeller-test Data to Design
and Performance Calculations. By Walter
S. Diehl. (Tenth Annual, 1924)------------------
196 Comparison of Model Propeller Tests with the
Airfoil Theory. By W. F. Durand and E. P.
Lesley. (Tenth Annual, 1924)-------------- .10
220 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
2235 Interaction between Air Propellers and Airplane
Structures. By W. F. Durand. (Twelfth
Annual, 1926)---------------------------------
237 Tests on Thirteen Navy Type Model Propellers.
By W. F. Durand. (Twelfth Annual, 1926)-- .10
259 Characteristics of Propeller Sections Tested in
the Variable Density Wind Tunnel. By East-
man N. Jacobs. (Thirteenth Annual, 1927)--, .10
292 Characteristics of Five Propellers in Flight.
By J. W. Crowley, jr., and R. E. Mixson.
(Fourteenth Annual, 1928)----------------- 15
2 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.








28


PROPELLERS-Coutinued

No. Title Price

301 Full Scale Tests of Wood Propellers on a VE-7
SAirplane in the Propeller Research Tunnel.
By Fred E. Weick. (Fourteenth Annual,
1928)------------------------------------ $0. 15
302 Full Scale Tests on a Thin Metal Propeller at
SVarious Tip Speeds. By Fred E. Weick.
(Fourteenth Annual. 1928) ------------------ 10
306 Full Scale Wind Tunnel Tests of a Series of
Metal Propellers on a VE-7 Airplane. By
Fred E. Weick. (Fourteenth Annual, 1928)' 10


SEAPLANES

209 Characteristics of a Single-float Seaplane during
Take-off. By J. W. Crowley, jr., and K. M.
Ronan. (Tenth Annual, 1924)-- ---------- $0.05
226 Characteristics of a Boat-type Seaplane during
Take-off. By J. W. Crowley, jr., and K. M.
IRonan. (Eleventh Annual, 1925)----------- 05
242 Characteristics of a Twin-float Seaplane during
Take-off. By John W. Crowley, jr., and K.
M. Ronan. (Twelfth Annual, 1926)-------- 10
290 Water-Pressure Distribution on a Seaplane
Float. (Fourteenth Annual, 1928)---------- 10

STABILITY AND CONTROL

Sl1 Report on Behavior of Airplanes in Gusts.
(First Annual, 1915)-----------------------------
Part 1. Experimental Analysis of Inherent
Longitudinal Stability for a Typical Bi-
l)lane. By J. C. Hinsakcr.
Part 2. Theory of an Airplane Encounter-
ing Gusts. By E. B. Wilson.
I Out of print. Anniil vnliumeo availaItle for reference nr loan in the Office of
Aeronautical Intelligence, National Adv'isory ('ominittece fur Aeronautics, Wash-
Ington, D. C'., ariii inl tlie lii rarnies of large cities.










STABILITY AND CONTROL-Continued

No. Title Price

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
SRolling. By E. B. Wilson. (Fourth Annual,
1918)------------------------------------------
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-
man. (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)-__ $0. 10
2120 Practical Stability and Controllability of Air-
planes. By F. H. Norton. (Seventh An-
nual, 1921) -----------------------------------
'153 Controllability and Maneuverability of Air-
planes. By F. H. Norton and WX. G. Brown.
(Eighth Annual, 1922) -------------
172 Dynamic Stability as Affected by the Longitu-
dinal Moment of Inertia. By Edwin B.
Wilson. (Ninth Annual, 1923)------------- .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

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.








30

STRENGTH OF CONSTRUCTION

Nn. Title ,Price

.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)------------------------
35 The Strength of One-piece, Solid, Built-up, and
Laminated Wood Airplane Wing Beams.
By John H. Nelson. (Fourth Annual, 1918)_ ------
76 Analysis of Fuselage Stresses. By Edward P.
W\arner and Roy G. Miller. (Fifth Annual,
1919)-------- ------------------------------
3 S2 Airplane Stress Analysis. By A. F. Zahm.
(Fifth Annual, 1919)------------------------
3 92 Analysis of Wing Truss Stresses. By Edward
P. Warner and Roy G. Miller. (Sixth 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. Zahmi, R. H.
Smith, and G. C. HIill. (Eighth Annual, 1922)_. .05
140 Lift and Drag Effects on Wing Tip-rake. By
A. F. Zahmi, R. M. Bear, and G. C. Hill.
(Eighth annuall 1922)--------------------I .05
S143 Analysis of Stresses in German Ai:irplanes. By
Wilhelmn Hoff. (Eighth Annual, 1922)------------
161 The Distribution of Lift Over Wing Tips and
Ailerons. B" David L. Bacon. (Ninth
Annual, 1923)-------------------------- 10
S180 The Influtence of the Form of a Wooden Beam
on Its Stiffness and Strength-I: Deflection of
Beams with Special Reference to Shear Def-
ormatiotis. By J. A. Newlin and G. W.
Tr:LNr. (Ninth Annual, 1923) ---------------
1Sl1 The Influreenc of tlie Form of a Wooden Beam
on Its Stiffness and Strength-Il: Form
Factors of Beams Subjected to Transverse
Loading Only. Bl J. A. Newlin and G. W.
Traver. (Ninth Annual, 1923---------- ------
I Out of print. Annual volume avnilahle for reference or loan in the Office of
Aerrnauticaril Intelligence. National Advisory Committee [or Aeronautics, Wash-
ington, D. C'., anrl in the librarie' i)f large cities.
Out of print. Available as a e'pairate report for reference or loan in the Office
of Aeronautitici Intelligence. Nat nrmul Advisory Commnittee for Aeronautics.










STRENGTH OF CONSTRUCTION-Continued

No. Title Prica

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) -------- ..--.


WIND TUNNELS AND LABORATORIES


44 The Altitude Laboratory for the Testing of
Aircraft Engines. By H. C. Dickinson and
H. G. Boutell. (Fourth Annual, 1918)------ $0. 11i
72 Wind-tunnel Balances. By Edward P. Warner
and F. H. Norton. (Fifth Annual, 1919)___ 19
3 73 The Design of Wind Tunnels and Wind-tunnel
Propellers. By Edward P. Warner and F.
H. Norton. (Fifth Annual, 1919)----------------_
3 74 Construction of Models for Tests in Wind tun- i
nels. By F. H. Norton. (Fifth Annual,
1919)-------------------------------------
98 Design of Wind Tunnels and Wind-tunnel
Propellers-II. By F. H. Norton and Ed-
ward P. Warner. (Sixth Annual, 1920)------ -. l1
146 The Six-component Wind Balance. By A. F.
Zahm. (Eighth Annual, 1922) ------------- o05
195 Standardization Tests of N. A. C. A. No. 1
Wind Tunnel. By Elliott G. Reid. (Tenth
Annual, 1924)------------------- .---------- 10
227 The Variable-density Wind Tunnel of the
National Advisory Committee for Aeronau-
tics. By Max M. Munk and Elton W. Miller.
(Eleventh Annual, 1925)------------------- 10
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.










WIND TUNNELS AND LABORATORIES-Continued

No. Title Price

231 Investigation of Turbulence in Wind Tunnels by
a Study of the Flow About Cylinders. By I
H. L. Dryden and R. H. Heald. (Eleventh
Annual, 1925)--------------------------- $0. 10
275 The Effect of the Walls in Closed Type Wind
Tunnels. Bv 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









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