Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

Medientyp: E-Book

Titel: Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

Körperschaft: United States, National Advisory Committee for Aeronautics

Erschienen: Washington, DC, 1952
Online-Ausg., Chester, Vt: NewsBank, inc, 2008

Umfang: Online-Ressource (1452 p); illustrations, tables

Sprache: Englisch

Reproduktionsreihe: U.S. Congressional Serial Set, 1817-1980

Art der Reproduktion: Online-Ausg.

Hersteller der Reproduktion: Chester, Vt: NewsBank, inc, 2008

Entstehung:

Anmerkungen: A comparison of theory and experiment for high-speed free-molecule flow, by Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager [No. 1032], p. 735
A general integral form of the boundary-layer equation for incompressible flow with an application to the calculation of the separation point of turbulent boundary layers, by Neal Tetervin and Chia Chiao Lin [No. 1046], p. 1067
A lift-cancellation technique in linearized supersonic-wing theory, by Harold Mirels [No. 1004], p. 65
A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions, by Richard R. Heldenfels [No. 1043], p. 1019
A recurrence matrix solution for the dynamic response of aircraft in gusts, by John C. Houbolt [No. 1010], p. 145
A small-deflection theory for curved sandwich plates, by Manuel Stein and J. Mayers [No. 1008], p. 129
A study of effects of viscosity on flow over slender inclined bodies of revolution, by H. Julian Allen and Edward W. Perkins [No. 1048.], p. 1103
A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results, by John D. Bird and Byron M. Jaquet [No. 1031], p. 709
A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow, by Arthur L. Jones and Alberta Alksne [No. 1052], p. 1211
A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane, by Leonard Sternfield and Ordway B. Gates, Jr. [No. 1018], p. 291
An analysis of base pressure at supersonic velocities and comparison with experiment, by Dean R. Chapman [No. 1051], p. 1187
Analysis of means of improving the uncontrolled lateral motions of personal airplanes, by Marion O. McKinney, Jr. [No. 1035], p. 795
Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range, by M.H. Lee Wu [No. 1021], p. 359
Analysis of the effects of boundary-layer control on the take-off and power-off landing performance characteristics of a liaison type of airplane, by Elmer A. Horton, Laurence K. Loftin, Jr., Stanley F. Racisz, and John H. Quinn, Jr. [No. 1057], p. 1353
Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection, by E. Clinton Wilcox and Arthur M. Trout [No. 1006], p. 97
Analysis of turbulent free-convection boundary layer on flat plate, by E.R.G. Eckert and Thomas W. Jackson [No. 1015], p. 255
Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions, by Alexander Mendelson and Selwyn Gendler [No. 1005], p. 77
Buckling of thin-walled cylinder under axial compression and internal pressure, by Hsu Lo, Harold Crate, and Edward B. Schwartz [No. 1027], p. 647
Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1024], p. 413
Comparison between theory and experiment for wings at supersonic speeds, by Walter G. Vincenti [No. 1033], p. 757
Comparison of theoretical and experimental heat-transfer characteristics of bodies of revolution at supersonic speeds, by Richard Scherrer [No. 1055], p. 1301
Compressive strength of flanges, by Elbridge Z. Stowell [No. 1029], p. 675
Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume, by P.H. Wise, K.T. Serijan, and I.A. Goodman [No. 1003], p. 55
Diffusion of chromium in alpha cobalt-chromium solid solutions, by John W. Weeton [No. 1023], p. 397
Dynamics of a turbojet engine considered as a quasi-static system, by Edward W. Otto and Burt L. Taylor, III [No. 1011], p. 177
Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow, by Charles E. Watkins [No. 1028], p. 657
Effect of tunnel configuration and testing technique on cascade performance, by John R. Erwin and James C. Emery [No. 1016], p. 263
Effects of wing flexibility and variable air lift wing bending moments during landing impacts of a small seaplane, by Kenneth F. Merten and Edgar B. Beck [No. 1013], p. 221
Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the mach lines, by Kennith L. Goin [No. 1041], p. 937
Experimental and theoretical studies of area suction for the control of the laminar boundary layer on an NACA 64A010 airfoil, by Albert L. Braslow, Dale L. Burrows, Neal Tetervin, and Fioravante Visconti [No. 1025], p. 433
Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 [degree] sweptback wing and tail surfaces, by M.J. Queijo and Walter D. Wolhart [No. 1049], p. 1117
Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a mach number of 1.5, by Dean R. Chapman and Edward W. Perkins [No. 1036], p. 805
Formulas for the supersonic loading, lift, and drag of flat swept-back wings with leading edges behind the mach lines, by Doris Cohen [No. 1050], p. 1146
General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions, by Vearl N. Huff, Sanford Gordon, and Virginia E. Morrell [No. 1037], p. 829
Horizontal tail loads in maneuvering flight, by Henry A. Pearson, William A. McGowan, and James J. Donegan [No. 1007], p. 117
Influence of chemical composition on rupture properties at 1200 [degrees] F. of forged chromium-cobalt-nickel-iron base alloys in solution-treated and aged condition, by E.E. Reynolds, J.W. Freeman, and A.E. White [No. 1058], p. 1385
Integrals and integral equations in linearized wing theory, by Harvard Lomax, Max A. Heaslet, and Franklyn B. Fuller [No. 1054], p. 1267
Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine, by Burt L. Taylor, III, and Frank L. Oppenheimer [No. 1017], p. 279
Investigation of fretting by microscopic observation, by Douglas Godfrey [No. 1009], p. 135
Investigation of separation of the turbulent boundary layer, by G.B. Schubauer and P.S. Klebanoff, National Bureau of Standards [No. 1030], p. 689
Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65 series wings equipped with full-span slotted flaps, by Jack Fischel and James M. Watson [No. 1034], p. 769
Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward mach numbers to 0.725 to determine the effects of camber and compressibility on performance, by James B. Delano [No. 1012], p. 189
Investigation of turbulent flow in a two-dimensional channel, by John Laufer, California Institute of Technology [No. 1053], p. 1247
Measurements of average heat-transfer and friction coefficients for subsonic flow of air in smooth tubes at high surface and fluid temperatures, by Leroy V. Humble, Warren H. Lowdermilk, and Leland G. Desmon [No. 1020], p. 343
NACA investigation of fuel performance in piston-type engines, by Henry C. Barnett [No. 1026], p. 453
On the particular integrals of the Prandtl-Busemann iteration equations for the flow of a compressible fluid, by Carl Kaplan [No. 1039], p. 909
Relation between inflammables and ignition sources in aircraft environments, by Wilfred E. Scull [No. 1019], p. 303
Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane, by Leonard Sternfield [No. 1042], p. 1009
Spectra and diffusion in a round turbulent jet, by Stanley Corrsin and Mahinder S. Uberoi, Johns Hopkins University [No. 1040], p. 915
Study of effects of sweep on the flutter of cantilever wings, by J.G. Barmby, H.J. Cunningham, and I.E. Garrick [No. 1014], p. 229
Supersonic flow around circular cones at angles of attack, by Antonio Ferri [No. 1045], p. 1055
Table of contents, p. II
Temperature distribution in internally heated walls of heat exchangers composed of non-circular flow passages, by E.R.G. Eckert and George M. Low [No. 1022], p. 381
The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack, by Antonio Ferri [No. 1044], p. 1039
The stability of the compression cover of box beams stiffened by posts, by Paul Seide and Paul F. Barrett [No. 1047], p. 1087
Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds, by John DeYoung [No. 1056], p. 1317
Wind-tunnel investigation of air inlet and outlet openings on a streamline body, by John V. Becker [No. 1038], p. 887
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