> Verlagsreihe
-
1389:
Characteristics of the langley 8-foot transonic tunnel with slotted test section by Ray H. Wright; Virgil S. Ritchie, and Albin O. Pearson
Washington: Gov. Print. Off., 1959
-
1387:
Full scale investigation of several jet engine noise reduction nozzles by Willard D. Coles and Edmund E. Callaghan
Washington, DC: Gov. Print. Off., 1959
-
1390:
Incompressible flutter characteristics of representative aircraft wings by Charles H. Wilts
Washington: Gov. Print. Off., 1959
-
1381:
A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at high supersonic speeds by H. Julian Allen and A. J. Eggers
Washington: Gov. Print. Off., 1959
-
1388:
NACA research on slurry fuels by M. L. Pinns
Washington: Gov. Print. Off., 1959
-
1383:
Survey of hydrogen combustion properties by Isadore L. Drell and Frank E. Belles
Washington: Gov. Print. Off., 1959
-
1345:
The response of an airplane to random atmospheric disturbances by Franklin W. Diederich
Washington, DC: Gov. Print. Off., 1959
-
1391:
Investigation of a nonlinear control system by I. Flügge-Lotz; C. F. Taylor, and H. E. Lindberg
Washington: Gov. Print. Off., 1959
-
1392:
Boron and zirconium from crucibile refractories in a complex heat resistant alloy by R. F. Decker; John P. Rowe, and J. W. Freeman
Washington: Gov. Print. Off., 1959
-
1382:
A comperative analysis of the performance of long range hypervelocity vehicles by Alfred J. Eggers; H. Julian Allen and Stanford E. Neice
Washington: Gov. Print. Off., 1959
-
1368:
Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds by James C. Emery
Washington, DC: Gov. Print. Off., 1959
-
1370:
Area suction boundary-layer control as applied to the trailing-edge flaps of a 35° swept-wing airplane by Woodrow L. Cook; Seth B. Anderson and George E. Cooper
Washington, DC: Gov. Print. Off., 1959
-
1372:
A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient by P. R. Hill
Washington, DC: Gov. Print. Off., 1959
-
1375:
A wind tunnel investigation of the aerodynamik characteristics of a full scale supersonic type three-blade propeller at mach numbers to 0.96 by Albert J. Evans and George Liner
Washington, DC: Gov. Print. Off., 1959
-
1359:
Thin airfoil theory based on approximate solution of the transonic flow equation by John R. Spreiter and Alberta Y. Alksne
Washington, DC: Gov. Print. Off., 1959
-
1363:
Origin and prevention of crash fires in turbojet aircraft by I. Irving Pinkel
Washington, DC: Gov. Print. Off., 1959
-
1364:
Measurement of static pressure on aircraft by William Gracey
Washington, DC: Gov. Print. Off., 1959
-
1374:
The similarity rules for second order subsonic and supersonic flow by Milton D. Van Dyke
Washington, DC: Gov. Print. Off., 1959
-
1379:
Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary prandtl number by Eli Reshotko and Ivan E. Beckwith
Washington, DC: Gov. Print. Off., 1959
-
1380:
An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed tip wings at supersonic speeds by William B. Boatright
Washington, DC: Gov. Print. Off., 1959
-
1366:
The mechanism of thermal gradient mass transfer in the sodium hydroxide nickel system by Charles E. May
Washington, DC: Gov. Print. Off., 1959
-
1369:
Blowling-type boundary-layer control as applied to the trailing-edge flaps of a 35° swept-wing airplane by Mark W. Kelly; Seth B. Anderson and Robert C. Innis
Washington, DC: Gov. Print. Off., 1959
-
1371:
Investigation of some wake vortex characteristics of an inclined ogivecylinder body at mach number 2 by Leland H. Jorgensen ans Edward W. Perkins
Washington, DC: Gov. Print. Off., 1959
-
1376:
Elliptic cones alone and with wings at supersonic speeds by Leland H. Jorgensen
Washington, DC: Gov. Print. Off., 1959
-
1377:
Measurements of free space oscillating pressures near propellers at flight mach numbers to 0.72 by Max C. Kurbjun and Arthur W. Vogeley
Washington, DC: Gov. Print. Off., 1959
-
1362:
Theoretical combustion performance of several high energy fuels for ramjet engines by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon
Washington, DC: Gov. Print. Off., 1959
-
1378:
A method for simulating the atmospheric entry of long range ballistic missils by A. J. Eggers
Washington: Gov. Print. Off., 1959
-
1343:
A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures by Elbridge Z. Stowell
Washington, DC: U.S. Gov. Print. Off., 1958
-
1346:
Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades by John C. Houbolt and George W. Brooks
Washington, DC: US Gov. Print. Off., 1958
-
1347:
Ditching investigations of dynamic models and effects of design parameters on ditching characteristics by Lloyd J. Fisher and Edward L. Hoffman
Washington, DC: US Gov. Print. Off., 1958
-
1349:
A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition by Albert E. von Doenhoff and Elmer A. Horton
Washington, DC: US Gov. Print. Off., 1958
-
1350:
Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions by F. B. Gustafson and Robert J. Tapscott
Washington, DC: US Gov. Print. Off., 1958
-
1352:
Effect of fuel variables on carbon formation in turbojet-engine combustors by Edmund R. Jonash, Jerrold D. Wear and William P. Cook
Washington, DC: US Gov. Print. Off., 1958
-
1354:
Effect of chord size on weight and cooling characteristics of air-cooled turbine blades by Jack B. Esgar, Eugene F. Schum and Arthur N. Curren
Washington, DC: US Gov. Print. Off., 1958
-
1384:
A summary of preliminary investigations into the characteristics of combustion screech in ducted burners by Lewis Laboratory Staff
Washington, DC: US Gov. Print. Off., 1958
-
1385:
Drag minimization for wings and bodies in supersonic flow by Max A. Heaslet and Franklyn B. Fuller
Washington, DC: US Gov. Print. Off., 1958
-
1348:
Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality by B. Porter Brown
Washington, DC: US Gov. Print. Off., 1958
-
1301:
Linearzed lifting surface and lifting line evaluations of sidewash behind rolling triangular wings at supersonic speeds by Percy J. Bobbitt
Washington, DC: Gov. Print. Off., 1958
-
1307:
Lift and center of pressure of wing body tail combinations at subsonic, transonic, and supersonic speeds by William C. Pitts, Jack N. Nielsen and George E. Kaattari
Washington: Gov. Print. Off., 1958
-
1342:
A variational theorem for creep with apllications to plates and columns by J. Lyell Sanders, Harvey G. McComb and Floyd R. Schlechte
Washington, DC: U.S. Gov. Print. Off., 1958
-
1344:
A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver by Leonard Sternfield
Washington, DC: U.S. Gov. Print. Off., 1958
-
1351:
Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades by Robert P. Coleman and Arnold M. Feingold
Washington, DC: US Gov. Print. Off., 1958
-
1353:
An experimental investigation of sting support effects on drag and a comparsion with jet effects at transonic speeds by Maurice S. Cahn
Washington, DC: Gov. Print. Off., 1958
-
1300:
Basic considerations in the combustion of hydrocarbon fuels with air ed. by Henry C. Barnett
Washington, DC: Gov. Print. Off., 1958
-
1314:
Summary of scale model thrust reverser investigation by John H. Povolny; Fred W. Steffen and Jack G. McArdle
Washington, DC: Gov. Print. Off., 1958
-
1355:
A theoretical and experimental study of planing surfaces including effects of cross section and plan form by Charles L. Shuford
Washington, DC: US Gov. Print. Off., 1958
-
1317:
Cloud droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7 by Rinaldo J. Brun
Washington, DC: Gov. Print. Off., 1958
-
1319:
Induced velocities near a lifting rotor with nonuniform disk loading by Harry H. Heyson and S. Katzoff
Washington, DC: Gov. Print. Off., 1958
-
1356:
Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition by Dean R. Chapman; Donald M. Kuehn; Howard K. Larson
Washington, DC: US Gov. Print. Off., 1958
-
1358:
On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field by Vernon J. Rossow
Washington, DC: US Gov. Print. Off., 1958
-
1361:
Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses by Richard R. Heldenfels and Louis F. Vosteen
Washington, DC: US Gov. Print. Off., 1958
-
1339:
A summary and analysis of the low speed longitudinal characteristics of swept wings at the Reynolds number by G. Chester Furlong and James G. McHugh
Washington, DC: Gov. Print. Off., 1958
-
1360:
Growth of disturbances in a flame-generated shear region by Perry L. Blackshear
Washington, DC: US Gov. Print. Off., 1958
-
1357:
Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw by Lewis R. Fisher
Washington, DC: US Gov. Print. Off., 1958
-
1275:
The proper combination of lift loadings for least drag on a supersonic wing by Frederick C. Grant
Washington, DC: Gov. Print. Off., 1957
-
1277:
Interaction of a free flame front with a turbulence field by Maurice Tucker
Washington, DC: Gov. Print. Off., 1957
-
1278:
Effect of interaction on landing gear behavior and dynamic loads in a flexible airplane structure by Francis E. Cook and Benjamin Milwitzky
Washington, DC: Gov. Print. Off., 1957
-
1279:
Theoretical analysis of incopressible flow through a radial-inlet centrifugal impeller at various weight flows by James J. Kramer, Vasily D. Prian and Chung-Hua Wu
Washington, DC: Gov. Print. Off., 1957
-
1283:
Extrapolation techniques applied to matrix methods in neutron diffusion problems by Robert R. McCready
Washington, DC: Gov. Print. Off., 1957
-
1303:
Wind tunnel investigation of a number of total pressure tubes at high angeles of attack subsonic, transonic, and supersonic speeds by William Gracey
Washington, DC: Gov. Print. Off., 1957
-
1308:
Investigation of the compressive strength and creep lifetime 2024-T3 aluminium-alloy plates at elevated temperatures by Eldon E. Mathauser and William D. Deveikis
Washington, DC: US Gov. Print. Off., 1957
-
1312:
Some effects of bluntness on boundary layer transition and heat transfer at supersonic speeds by W. E. Moeckel
Washington, DC: Gov. Print. Off., 1957
-
1289:
Contributions on the mechanics of boundary layer transition by G. B. Schubauer and P. S. Klebanoff
Washington, DC: Gov. Print. Off., 1957
-
1282:
A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds by Harvard Lomax and Max A. Heaslet
Washington, DC: Gov. Print. Off., 1957
-
1304:
Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes by William H. Philipps, Helmut A. Kuehnel and James B. Whitten
Washington, DC: US Gov. Print. Off., 1957
-
1306:
Bodies of revolution having minimum drag at high supersonic airspeeds by A. J. Eggers
Washington, DC: US Gov. Print. Off., 1957
-
1309:
Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers by Julian D. Maynard and Leland B. Salters
Washington, DC: US Gov. Print. Off., 1957
-
1294:
The compressible laminar boundary layer with heat transfer and arbitary pressure gradient by Clarence B. Cohen and Eli Reshotko
Washington, DC: Gov. Print. Off., 1957
-
1299:
Correlation, evaluation, and extension of linearized theories for tire motion and wheel shimmy by Robert F. Smiley
Washington, DC: US Gov. Print. Off., 1957
-
1272:
A reevaluation of data on atmospheric turbulence and airplane gust loads for application in spectral calculations by Harry Press, May T. Meadows and Ivan Hadlock
Washington, DC: Gov. Print. Off., 1957
-
1302:
On panel flutter and divergence of infinitely unstiffened and ring-stiffened thin-walled circular cylinders by Robert W. Leonard and John M. Hedgepeth
Washington, DC: US Gov. Print. Off., 1957
-
1284:
Theory of wing body drag at supersonic speeds by Robert T. Jones
Washington, DC: Gov. Print. Off., 1957
-
1291:
Lift hysteresis at stall as an unstead boundary layer phenomenon by Franklin K. Moore
Washington, DC: Gov. Print. Off., 1957
-
1293:
Similar solutions for the compressible laminar boundary layer with heat transfer and pressure gradient by Clarence B. Cohen and Eli Reshotko
Washington, DC: Gov. Print. Off., 1957
-
1297:
Nonlifting wing-body combinations with certain geometric restraints having minimum wave drag at low supersonic speeds by Harvard Lomax
Washington, DC: US Gov. Print. Off., 1957
-
1270:
Review of experimental investigations of liquid metal heat transfer by Bernard Lubarsky and Samuel J. Kaufman
Washington, DC: Gov. Print. Off., 1957
-
1280:
Theoretical investigation of flutter of two dimensional flat panels with one surface exposed to supersonic potential flow by Herbert C. Nelson and Herbert J. Cunningham
Washington, DC: Gov. Print. Off., 1957
-
1281:
Flight determination of drag of normal shock nose inlets with various cowling profiles at mach numbers from 0.9 to 1.5 by R. I. Sears, C. F. Merlet and L. W. Putland
Washington, DC: Gov. Print. Off., 1957
-
1267:
Plastic deformation of aluminium single crystals at elevated temperatures by R. D. Johnson, A. P. Young and A. D. Schwope
Washington, DC: Gov. Print. Off., 1957
-
1310:
An investigation of four wings of square plan forms at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel by Charles H. McLellan, Mitchel H. Bertram and John A. Moore
Washington, DC: US Gov. Print. Off., 1957
-
1311:
Determination of vortex paths by series expansion technique with application to cruciform wings by Alberta Y. Alksne
Washington, DC: US Gov. Print. Off., 1957
-
1290:
Development of craze and impact resistance in glazing plastics by multiaxial stretching by G. M. Kline
Washington, DC: Gov. Print. Off., 1957
-
1288:
Cooperative investigation of relationship between static and fatigue properties of wrought N-155 alloy at elevated temperatures by NACA subcommittee on power-plant materials
Washington, DC: Gov. Print. Off., 1957
-
1292:
Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet by James C. Laurence
Washington, DC: Gov. Print. Off., 1957
-
1296:
A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes by John R. Spreiter and Alvin H. Sacks
Washington, DC: Gov. Print. Off., 1957
-
1298:
An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane by Richard B. Skoog
Washington, DC: US Gov. Print. Off., 1957
-
1318:
Three-dimensional transonic flow theory applied to slender wings and bodies by Max A. Heaslet and John R. Spreiter, Ames Aeronautical Laboratory Moffett Field, Calif
Washington, DC: US Government Printing Office, 1957
-
1315:
On slender-body theory at transonic speeds by Keith C. Harder and E. B. Klunker
Washington, DC: US Gov. Print. Off., 1957
-
1313:
Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9 by Mitchel H. Bertram
Washington, DC: US Gov. Print. Off., 1957
-
1316:
Torsional stiffness of thin-walled shells having reinforced cores and rectangular, triangular, or diamond cross section by Harvey G. McComb jr
Washington, DC: US Gov. Print. Off., 1957
-
1320:
An evaluation of four experimental methods for measuring mean properties of a supersonic turbulent boundary layer by George J. Nothwang
Washington, DC: US Gov. Print. Off., 1957
-
1269:
Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow by M. J. Queijo
Washington, DC: US Gov. Print. Off., 1956
-
1273:
A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound by Richard T. Whitcomb
Washington, DC: US Gov. Print. Off., 1956
-
1245:
Analysis and calculation by integral methods of laminar compressible boundary layer with heat transfer and with and without pressure gradient by Morris Morduchow
Washington, DC: Gov. Print. Off., 1956
-
1252:
Quasi-cylindrical theory of wing body interference at supersonic speeds and comparison with experiment by Jack N. Nielsen
Washington, DC: Gov. Print. Off., 1956
-
1266:
Charts for estimating performance of high-performance helicopters by Alfred Gessow
Washington, DC: US Gov. Print. Off., 1956
-
1264:
A thermal equation for flame quenching by A. E. Potter and A. L. Berlad
Washington, DC: Gov. Print. Off., 1956
-
1286:
Propagation of a free flame in a turbulent gas stream by William R. Mickelsen and Norman E. Ernstein
Washington, DC: US Gov. Print. Off., 1956
-
1274:
Second-order subsonic airfoil theory including edge effects by Milton D. van Dyke
Washington, DC: US Gov. Print. Off., 1956
-
1258:
A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds by Benjamin H. Beam
Washington, DC: US Gov. Print. Off., 1956
-
1216:
Charts for estimating tail rotor contribution to helicopter directional stability and control in low speed flight by Kenneth B. Amer and Alfred Gessow
Washington, DC: Gov. Print. Off., 1956
-
1218:
Effect of ground interference on the aerodynamic and flow characteristics of a 42° sweptback wing at reynolds number up to 6.8 x 10 6 by G. Chester Furlong and Thomas V. Bollech
Washington, DC: Gov. Print. Off., 1956
-
1223:
Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates by A. F. Lietzke
Washington, DC: Gov. Print. Off., 1956
-
1217:
Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds by John R. Spreiter and Alberta Alksne
Washington, DC: Gov. Print. Off., 1956
-
1222:
A free flight wind tunnel for aerodynamic testing at hypersonic speeds by Alvin Seiff
Washington, DC: Gov. Print. Off., 1956
-
1224:
Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta wing model by Alex Goodman and David F. Thomas
Washington, DC: Gov. Print. Off., 1956
-
1215:
Impingement of cloud droplets on a cylinder and procedure for measuring liquid water content and droplet sizes in supercooled clouds by rotating multicylinder method by R. J. Brun
Washington, DC: Gov. Print. Off., 1956
-
1219:
Measurement and analysis of wing and tail buffeting loads on a fighter airplane by Wilber B. Huston and T. H. Skopinski
Washington, DC: Gov. Print. Off., 1956
-
1221:
Theoretical study of the tunnel boundary lift interference due to slotted walls in the presence of the trailing-vortex system of a lifting model by Clarence W. Matthews
Washington, DC: Gov. Print. Off., 1956
-
1247:
Characteristics of turbulence in a boundary layer with zero pressure gradient by P. S. Klebanoff
Washington, DC: Gov. Print. Off., 1956
-
1256:
Axially symmetric shapes with minimum wave drag by Max A. Heaslet and Franklyn B. Fuller
Washington, D.C.: U.S. Gov. Print. Off., 1956
-
1257:
On the kernel function of the integral equation relating the lift and downwash distributions of oscillating wings in subsonic flow by Charles E. Watkins and Julian H. Berman
Washington, DC: US Gov. Print. Off., 1956
-
1260:
Studies of the speed stability of a tandem helicopter in forward flight by Robert J. Tapscott and Kenneth B. Amer
Washington, DC: U.S. Gov. Print. Off., 1956
-
1261:
The near noise field of static jets and some model studies of devices for noise reduction by Leslie W. Lassiter and Harvey H. Hubbard
Washington, DC: U.S. Gov. Print. Off., 1956
-
1238:
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles by Eugene S. Love
Washington, DC: US Gov. Print. Off., 1956
-
1239:
Error in airspeed measurement due to the static pressure field ahead of an airplane at transonic speeds by Thomas C. O'Bryan, Edward C. B. Danforth, and J. Ford Johnston
Washington, DC: US Gov. Print. Off., 1956
-
1243:
High resolution autoradiography by George C. Towe, Henry J. Gomberg, and J. W. Freeman
Washington, DC: US Gov. Print. Off., 1956
-
1271:
On boattail bodies of revolution having minimum wave drag by Keith C. Harder and Conrad Rennemann
Washington, DC: US Gov. Print. Off., 1956
-
1248:
An experimental study of applied ground loads in landing by Benjamin Milwitzky, Dean C. Lindquist, and Dexter M. Potter
Washington, DC: Gov. Print. Off., 1956
-
1249:
A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution by A. J. Eggers and Raymond C. Savin
Washington, DC: Gov. Print. Off., 1956
-
1254:
Friction, wear, and surface damage of metals as affected by solid surface films by Edmond E. Bisson
Washington, DC: Gov. Print. Off., 1956
-
1259:
Some possibilities of using gas mixtures other than air in aerodynamic research by Dean R. Chapman
Washington, DC: US Gov. Print. Off., 1956
-
1265:
A theory for stability and Buzz pulsation amplitude in ram jets and an experimental investigation including scale effects by Robert L. Trimpi
Washington, DC: US Gov. Print. Off., 1956
-
1244:
Free stream boundaries of turbulent flows by Stanley Corrsin and Alan L. Kistler
Washington, DC: Gov. Print. Off., 1956
-
1285:
Summary of derived gust velocities obtained from measurements within thunderstorms by H. B. Tolefson
Washington, DC: US Gov. Print. Off., 1956
-
1228:
Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow by Franklin W. Diederich and Martin Zlotnick
Washington, DC: Gov. Print. Off., 1956
-
1229:
Exact solutions of laminar boundary layer equations with constant property values for porous wall with variable temperature by Patrick L. Donoughe and John N. B. Livingood
Washington, DC: Gov. Print. Off., 1956
-
1230:
Generalized indicial forces on deforming rectangular wings in supersonic flight by Harvard Lomax; Franklyn B. Fuller and Loma Sluder
Washington, DC: Gov. Print. Off., 1956
-
1231:
NACA transonic wind tunnel test sections by Ray H. Wright and Vernon G. Ward
Washington, DC: Gov. Print. Off., 1956
-
1236:
Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds by Morris D. Friedman and Doris Cohen
Washington, DC: Gov. Print. Off., 1956
-
1226:
A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds by Warren A. Tucker
Washington, DC: Gov. Print. Off., 1956
-
1235:
Standard atmosphere - tables and data for altitudes to 65,800 feet International Civil Aviation Organization
Washington, DC: Gov. Print. Off., 1956
-
1251:
Stress analysis of circular semimonocoque cylinders with cutouts by Harvey G. McComb
Washington, DC: Gov. Print. Off., 1956
-
1227:
An investigation of the maximum lift of wings at supersonic speeds by James J. Gallagher and James N. Mueller
Washington, DC: Gov. Print. Off., 1956
-
1233:
Shock turbulence interaction and the generation of noise by H. S. Ribner
Washington, DC: Gov. Print. Off., 1956
-
1212:
Analog study of interacting and non-interacting multiple-loop control systems for turbojet engines by George J. Pack and W. E. Phillips
Washington, DC: US Gov. Print. Off., 1955
-
1213:
Minimum drag ducted and pointed bodies of revolution based on linearized supersonic theory by Hermon M. Parker
Washington, DC: Gov. Print. Off., 1955
-
1214:
Statistical measurements of contact conditions of 478 transport-airplane landings during routine daytime operations by Norman S. Silsby
Washington, DC: US Gov. Print. Off., 1955
-
1211:
Experimental investigation of free convection heat transfer in vertical tube at large grashof numbers by E. R. G. Eckert and A. J. Diaguila
Washington, DC: Gov. Print. Off., 1955
-
615:
Column strength of tubes elastically restrained against rotation at the ends by William R. Osgood
Washington, DC: Gov. Print. Off., 1955
-
1210:
Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers by Robert G. Deissler
Washington, DC: Gov. Print. Off., 1955
-
824:
Summary of airfoil data by Ira H. Abbott, Albert E. von Doenhoff and Louis S. Stivers
Washington, DC: National Advisory Committee for Aeronautics, 1945
-
637:
Determination of boundary layer transition on three symmetrical airfoils in the NACA full scale wind tunnel by Abe Silverstein and John V. Becker
Washington, DC: Gov. Print. Off., 1939
-
649:
The "Pack" method for compressive tests of thin specimens of materials used in thin-wall structures by C. S. Aitchison and L. B. Tuckerman
Washington, DC: Gov. Print. Off., 1939
-
630:
A flight comparison of conventional ailerons on a recetangular wing and of conventional and floating wing-tip on a tapered wing by H. A. Soulé and W. Gracey
Washington, DC: Gov. Print. Off., 1939
-
657:
The influence of directed air flow on combustion in a spark ignition engine by A. M. Rothrock and R. C. Spencer
Washington, DC: Gov. Print. Off., 1939
-
674:
Cooling on the front of an air cooled engine cylinder in a conventional engine cowling by M. J. Brevoort and U. T. Joyner
Washington, DC: Gov. Print. Off., 1939
-
675:
Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontral tail surface by Harry J. Goett and J. P. Reeder
Washington, DC: Gov. Print. Off., 1939
-
676:
Surface heat transfer coefficients of finned cylinders by Herman H. Ellerbrock and Arnold E. Biermann
Washington, DC: Gov. Print. Off., 1939
-
664:
Wind tunnel investigation of an NACA 23012 airfoil with various arrangements of slotted flaps by Carl J. Wenzinger and Thomas A. Harris
Washington, DC: Gov. Print. Off., 1939
-
648:
Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings by Abe Silverstein and S. Katzoff
Washington, DC: Gov. Print. Off., 1939
-
652:
Air flow in the boundary layer of an elliptic cylinder by G. B. Schubauer
Washington, DC: Gov. Print. Off., 1939
-
667:
Determination of the profile drag of an airplane wing in flight at high reynolds numbers by Joseph Bicknell
Washington, DC: Gov. Print. Off., 1939
-
673:
Experimental verification of the theory of oscillating airfoils by Abe Silverstein and Upshur T. Joyner
Washington, DC: Gov. Print. Off., 1939
-
622:
A photographic study of combustion and knock in a spark ignition engine by A. M. Rothrock and R. C. Spencer
Washington, DC: Gov. Print. Off., 1938
-
633:
Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap by Carl J. Wenzinger and James B. Delano
Washington, DC: Gov. Print. Off., 1938
-
634:
Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing edge flaps by H. Julian Allen
Washington, DC: Gov. Print. Off., 1938
-
638:
The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts by Robert T. Jones
Washington, DC: Gov. Print. Off., 1938
-
629:
On some reciprocal relations in the theory of nonstationary flows by I. E. Garrick
Washington, DC: Gov. Print. Off., 1938
-
640:
The aerodynamic characteristics of full scale propellers having 2, 3, and 4 blades of clark y and RAF 6 airfoil sections by Edwin P. Hartmann and David Biermann
Washington, DC: Gov. Print. Off., 1938
-
645:
Correction of temperatures of air cooled engine cylinders for variation in engine and cooling conditions by Oscar W. Schey, Benjamin Pinkel and Hermann H. Ellerbrock
Washington, DC: Gov. Print. Off., 1938
-
635:
Theoretical stability and control characteristics of wings with various amounts of taper and twist by Henry A. Pearson and Robert T. Jones
Washington, DC: US Gov. Print. Off., 1938
-
534:
Aerodynamic characteristics of a wing [with fowler flaps] including flap loads, downwash, and calculated effect on take-off by Robert C. Platt
[Washington, DC]: US Gov. Print. Off., 1935
-
468:
The interference between struts in various combinations by David Biermann and William H. Herrnstein
Washington, DC: NACA, 1933
-
418:
Preliminary investigation of modifications to conventional airplanes to give nonstalling and short landing characteristics by Fred E. Weick
Washington, DC: US Gov. Print. Off., 1932
-
402:
Effect of orifice length diameter ration on fuel sprays for compression ignition engines by A. G. Gelalles
Washington, DC: US Gov. Print. Off., 1932
-
434:
Lift and drag characteristics and gliding performance of an autogiro as determined in flight by John B. Wheatley
Washington, DC: US Gov. Print. Off., 1932
-
414:
The effect on airplane performance of the factors that must be considered in applying low drag cowling to radial engines by William H. MacAvoy; Oscar W. Schey and Alfred W. Young
Washington, DC: US Gov. Print. Off., 1932
-
419:
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 1 Ordinary ailerons on rectangular wings / by Fred E. Weick and Carl J. Wenzinger
Washington, D.C.: US Gov. Print. Off., 1932
-
379:
Rolling moments due to rolling and yaw for four wing models in rotation by Montgomery Knight and Carl J. Wenzinger
Washington, DC: US Gov. Print. Off., 1931
-
380:
Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight by Richard V. Rhode and Eugene E. Lundquist
Washington, DC: US Gov. Print. Off., 1931
-
382:
Elastic instability of members having sections common in aircraft construction by George W. Trayer and H. W. March
Washington, DC: US Gov. Print. Off., 1931
-
387:
The vertical wind tunnel of the national advisory committee for aeronautics by Carl J. Wenzinger and Thomas A. Harris
Washington, DC: US Gov. Print. Off., 1931
-
388:
Investigation of the diaphragm type pressure cell by Theodore Theodorsen
Washington, DC: US Gov. Print. Off., 1931
-
390:
The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level by Oscar W. Schey and Arnold E. Biermann
Washington, DC: US Gov. Print. Off., 1931
-
371:
Present status of aircraft instruments
Washington, DC: US Gov. Print. Off., 1931
-
377:
A method of flight measurement of spins by Hartley A. Soulé and Nathan F. Scudder
Washington, DC: US Gov. Print. Off., 1931
-
381:
Static, drop, and flight tests on Musselman type airwheels by William C. Peck and Albert P. Besard
Washington, DC: US Gov. Print. Off., 1931
-
384:
The comparative performance of superchargers by Oscar W. Schey
Washington, DC: US Gov. Print. Off., 1931
-
386:
Maneuverability investigation of an F6C-4 fighting airplane by C. H. Dearborn and H. W. Kirschbaum
Washington, DC: US Gov. Print. Off., 1931
-
369:
Maneuverability investigation of the F6C-3 airplane with special flight instruments by C. H. Dearborn and H. W. Kirschbaum
Washington, DC: US Gov. Print. Off., 1931
-
374:
The automotive ignition coil by T. H. Darnell
Washington, DC: US Gov. Print. Off., 1931
-
389:
The effect of small angles of yaw and pitch on the characteristics of airplane propellerss by Hugh B. Freeman
Washington, DC: US Gov. Print. Off., 1931
-
395:
A new principle of sound frequency analysis by Theodore Theodorsen
Washington, DC: US Gov. Print. Off., 1931
-
401:
Combustion in a high speed compression ignition engine by A. M. Rothrock
Washington, DC: US Gov. Print. Off., 1931
-
334:
The torsion of members having sections common in aircraft construction by George W. Trayer and H. W. March
Washington, DC: US Gov. Print. Off., 1930
-
128:
Direction instruments in four parts
Washington, DC: Gov. Print. Off., [1929?]
-
310:
Pressure element of constant logarithmic stiffness for temperature compensated altimeter by W. G. Brombacher and F. Cordero
Washington, DC: US Gov. Print. Off., 1929
-
311:
Aerodynamic theory and test of strut forms 1 by R. H. Smith
Washington, DC: US Gov. Print. Off., 1929
-
332:
The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine by Oscar W. Schey and Arnold E. Biermann
Washington, DC: US Gov. Print. Off., 1929
-
124:
Aerodynamic characteristics of aerofoils 2 Continuation of report no. 93
Washington, DC: Gov. Print. Off., 1928
-
126:
Altitude instruments in four parts
Washington, DC: Gov. Print. Off., [1922]
-
129:
Power plant instruments in five parts
Washington, DC: Gov. Print. Off., [1922?]
-
131:
Aerial navigation and navigating instruments by H. N. Eaton
Washington, DC: Gov. Print. Off., [1922]
-
132:
Recent developments and outstanding problems by F. L. Hunt
Washington, DC: Gov. Print. Off., 1922
-
127:
Aircraft speed instruments in three parts by F. L. Hunt and H. O. Stearns
Washington, DC: Gov. Print. Off., [1922?]
-
130:
Oxygen instruments by F. L. Hunt
Washington, DC: Gov. Print. Off., [1922]
-
123:
Simplified theory of the magneto by F. B. Silsbee
Washington, DC: Gov. Print. Off., [1921]
-
101:
The calculated performance of airplanes equipped with supercharging engines in two parts by E. C. Kemble
Washington, DC: Gov. Print. Off., 1921
-
106:
Turbulence in the air tubes of radiators for aircraft engines by S. R. Parsons
Washington, DC: Gov. Print. Off., 1921
-
107:
A high speed engine pressure indicator of the balanced diaphragm type by H. C. Dickinson and F. B. Newell
Washington, DC: Gov. Print. Off., 1921
-
108:
Some factors of airplane engine performance by Victor R. Gage
Washington, DC: Gov. Print. Off., 1921
-
109:
Experimental research on air propellers 4 By W. F. Durand and E. P. Lesley
Washington, DC: Gov. Print. Off., 1921
-
110:
The altitude effect on air speed indicators in two parts by Mayo D. Hersey, Franklin L. Hunt, and Herbert N. Eaton
Washington, DC: Gov. Print. Off., 1921
-
125:
General classification of instruments and problems including bibliography by Mayo D. Hersey
Washington, DC: Gov. Print. Off., [1921?]
-
84:
Data on the design of plywood for aircraft by Armin Elmendorf
Washington, DC: Gov. Print. Off., [ca. 1920]
-
86:
Properties of special types of radiators by S. R. Parsons
Washington, DC: Gov. Print. Off., [ca. 1920]
-
87:
Effects of nature of cooling surface on radiator performance by S. R. Parsons and R. V. Kleinschmidt
Washington, DC: Gov. Print. Off., 1920
-
88:
Pressure drop in radiator air tubes by S. R. Parsons
Washington, DC: Gov. Print. Off., 1920
-
89:
Comparison of alcogas aviation fuel with export aviation gasoline by V. R. Gage, S. W. Sparrow, and D. R. Harper
Washington, DC: Gov. Print. Off., 1920
-
90:
Comparison of Hecter fuel with export aviation gasoline by H. C. Dickinson, V. R. Gage, and S. W. Sparrow
Washington, DC: Gov. Print. Off., 1920
-
91:
Nomenclature for aeronautics
Washington, DC: Gov. Print. Off., 1920
-
92:
Analysis of wing truss stresses incl. the effect of redundancies by E. P. Warner and R. G. Miller
Washington, DC: Gov. Print. Off., 1920
-
94:
The efficiency of small bearings in instruments of the type used in aircraft by F. H. Norton
Washington, DC: Gov. Print. Off., 1920
-
104:
Torsion of wing trusses at diving speeds by Roy G. Miller
Washington, DC: Gov. Print. Off., 1920