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

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Online Access:	Online Access
Corporate Authors:	United States. Congress. Senate, United States. National Advisory Committee for Aeronautics
Other Authors:	Alksne, Alberta Y., Allen, H. Julian, Barmby, J. G., Barnett, Henry C., Barrett, Paul F., 1943-2004, Beck, Edgar B., Becker, John Vernon, 1913-, Bird, J. D., Braslow, Albert L., Burrows, Dale L., Chapman, Dean R., Cohen, Doris, Corrsin, Stanley, 1920-, Crate, Harold, Creager, Marcus O., Cunningham, Herbert J., Delano, James B. (James Benjamin), Desmon, Leland G., DeYoung, John, Diederich, Franklin W., Donegan, James J., Eckert, E. R. G. (Ernst Rudolf Georg), 1904-2004, Emery, James C., Erwin, John R., Ferri, Antonio, 1912-1975, Fischel, Jack, Freeman, J. W. (James W.), Fuller, Franklyn B., Garrick, I. E. (Isadore Edward), 1910-1981, Gates, Ordway B., Gendler, Selwyn, Godfrey, Douglas, Goin, Kennith L., Goodman, I. A., Goodwin, Glen, Gordon, Sanford, Heaslet, M. A. (Maxwell Alfred), 1907-, Heldenfels, Richard R., Horton, Elmer A., Houbolt, John C., Huff, Vearl N., Humble, Leroy V., Jackson, Thomas Woodrow, 1917-, Jaquet, Byron M., Jones, A. L. (Arthur Leslie), Kaplan, Carl, Klebanoff, P. S., Laufer, John, Lin, C. C. (Chia-Chʻiao), 1916-2013, Lo, Hsu, Loftin, Laurence K., Lomax, Harvard, Low, George M., 1926-1984, Lowdermilk, Warren H., Mayers, J. (Jerry), McGowan, William A., McKinney, Marion O., Mendelson, Alexander, Merten, Kenneth F., Mirels, Harold, Morrell, Virginia E., Oppenheimer, Frank L., Otto, Edward W., Pearson, Henry A. (Henry Adolph), 1906-, Perkins, Edward W., Queijo, M. J., Quinn, John H., Racisz, Stanley F., Reynolds, E. E., Scherrer, R., Schubauer, Galen B. (Galen Brandt), 1904-, Schwartz, Edward B., Scull, Wilfred E., Seide, Paul, Serijan, K. T., Stalder, Jackson R., Stein, Manuel, Sternfield, Leonard, Stowell, Elbridge Z., Taylor, Burt L., Tetervin, Neal, Trout, Arthur M., Uberoi, M. S. (Mahinder S.), Vincenti, Walter G. (Walter Guido), 1917-2019, Visconti, Fioravante, Watkins, Charles E., Watson, James M., Weeton, John W., White, A. E., Wilcox, E. Clinton, Wise, Paul H., Wolhart, Walter D., Wu, M. H. Lee
Format:	Government Document Electronic eBook
Language:	English
Published:	Washington, DC, 1952.
Series:	Senate document (United States. Congress. Senate) ; 82nd Congress, no. 93. United States congressional serial set ; serial set no. 11595.
Subjects:	United States. > National Advisory Committee for Aeronautics. Aeronautics. Aircraft engines. Aircraft parts. Airplanes. Transportation research.

Description
Item Description:	Table of contents, p. II. 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], page 55. A lift-cancellation technique in linearized supersonic-wing theory, by Harold Mirels [No. 1004], page 65. Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions, by Alexander Mendelson and Selwyn Gendler [No. 1005], page 77. 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], page 97. Horizontal tail loads in maneuvering flight, by Henry A. Pearson, William A. McGowan, and James J. Donegan [No. 1007], page 117. A small-deflection theory for curved sandwich plates, by Manuel Stein and J. Mayers [No. 1008], page 129. Investigation of fretting by microscopic observation, by Douglas Godfrey [No. 1009], page 135. A recurrence matrix solution for the dynamic response of aircraft in gusts, by John C. Houbolt [No. 1010], page 145. Dynamics of a turbojet engine considered as a quasi-static system, by Edward W. Otto and Burt L. Taylor, III [No. 1011], page 177. 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], page 189. 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], page 221. Study of effects of sweep on the flutter of cantilever wings, by J.G. Barmby, H.J. Cunningham, and I.E. Garrick [No. 1014], page 229. Analysis of turbulent free-convection boundary layer on flat plate, by E.R.G. Eckert and Thomas W. Jackson [No. 1015], page 255. Effect of tunnel configuration and testing technique on cascade performance, by John R. Erwin and James C. Emery [No. 1016], page 263. 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], page 279. 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], page 291. Relation between inflammables and ignition sources in aircraft environments, by Wilfred E. Scull [No. 1019], page 303. 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], page 343. Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range, by M.H. Lee Wu [No. 1021], page 359. 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], page 381. Diffusion of chromium in alpha cobalt-chromium solid solutions, by John W. Weeton [No. 1023], page 397. Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1024], page 413. 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], page 433. NACA investigation of fuel performance in piston-type engines, by Henry C. Barnett [No. 1026], page 453. Buckling of thin-walled cylinder under axial compression and internal pressure, by Hsu Lo, Harold Crate, and Edward B. Schwartz [No. 1027], page 647. 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], page 657. Compressive strength of flanges, by Elbridge Z. Stowell [No. 1029], page 675. Investigation of separation of the turbulent boundary layer, by G.B. Schubauer and P.S. Klebanoff, National Bureau of Standards [No. 1030], page 689. 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], page 709. A comparison of theory and experiment for high-speed free-molecule flow, by Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager [No. 1032], page 735. Comparison between theory and experiment for wings at supersonic speeds, by Walter G. Vincenti [No. 1033], page 757. 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], page 769. Analysis of means of improving the uncontrolled lateral motions of personal airplanes, by Marion O. McKinney, Jr. [No. 1035], page 795. 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], page 805. 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], page 829. Wind-tunnel investigation of air inlet and outlet openings on a streamline body, by John V. Becker [No. 1038], page 887. On the particular integrals of the Prandtl-Busemann iteration equations for the flow of a compressible fluid, by Carl Kaplan [No. 1039], page 909. Spectra and diffusion in a round turbulent jet, by Stanley Corrsin and Mahinder S. Uberoi, Johns Hopkins University [No. 1040], page 915. 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], page 937. 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], page 1009. A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions, by Richard R. Heldenfels [No. 1043], page 1019. The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack, by Antonio Ferri [No. 1044], page 1039. Supersonic flow around circular cones at angles of attack, by Antonio Ferri [No. 1045], page 1055. 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], page 1067. The stability of the compression cover of box beams stiffened by posts, by Paul Seide and Paul F. Barrett [No. 1047], page 1087. A study of effects of viscosity on flow over slender inclined bodies of revolution, by H. Julian Allen and Edward W. Perkins [No. 1048.], page 1103. 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], page 1117. 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], page 1146. An analysis of base pressure at supersonic velocities and comparison with experiment, by Dean R. Chapman [No. 1051], page 1187. A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow, by Arthur L. Jones and Alberta Alksne [No. 1052], page 1211. Investigation of turbulent flow in a two-dimensional channel, by John Laufer, California Institute of Technology [No. 1053], page 1247. Integrals and integral equations in linearized wing theory, by Harvard Lomax, Max A. Heaslet, and Franklyn B. Fuller [No. 1054], page 1267. Comparison of theoretical and experimental heat-transfer characteristics of bodies of revolution at supersonic speeds, by Richard Scherrer [No. 1055], page 1301. Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds, by John DeYoung [No. 1056], page 1317. 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], page 1353. 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], page 1385.
Physical Description:	1,452 pages : illustrations, tables.
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