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LEADER 00000cam  22021611i 4500 
003    Readex 
005    20100422150806.8 
006    m        d         
007    cr cn |||||||| 
008    081210s1952    dcu      s   f000 0 eng d 
019    NB00000283756 
035    (Readex)1206209030981428 
040    Readex|cReadex 
110 1  United States.|bCongress.|bSenate. 
245 10 Thirty-seventh annual report of the National Advisory 
       Committee for Aeronautics. 1951. Including technical 
       reports nos. 1003 to 1058.|h[electronic resource] 
260    Washington, DC,|c1952 
300    1452 p. :|billustrations, tables. 
440  0 United States congressional serial set;|vserial set no. 
       11595 
490 1  Senate document / 82nd Congress, 2nd session. Senate ;
       |vno. 93 
500    Table of contents, p. II. 
500    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. 
500    A lift-cancellation technique in linearized supersonic-
       wing theory, by Harold Mirels [No. 1004], p. 65. 
500    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. 
500    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. 
500    Horizontal tail loads in maneuvering flight, by Henry A. 
       Pearson, William A. McGowan, and James J. Donegan [No. 
       1007], p. 117. 
500    A small-deflection theory for curved sandwich plates, by 
       Manuel Stein and J. Mayers [No. 1008], p. 129. 
500    Investigation of fretting by microscopic observation, by 
       Douglas Godfrey [No. 1009], p. 135. 
500    A recurrence matrix solution for the dynamic response of 
       aircraft in gusts, by John C. Houbolt [No. 1010], p. 145. 
500    Dynamics of a turbojet engine considered as a quasi-static
       system, by Edward W. Otto and Burt L. Taylor, III [No. 
       1011], p. 177. 
500    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. 
500    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.
500    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. 
500    Analysis of turbulent free-convection boundary layer on 
       flat plate, by E.R.G. Eckert and Thomas W. Jackson [No. 
       1015], p. 255. 
500    Effect of tunnel configuration and testing technique on 
       cascade performance, by John R. Erwin and James C. Emery 
       [No. 1016], p. 263. 
500    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. 
500    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. 
500    Relation between inflammables and ignition sources in 
       aircraft environments, by Wilfred E. Scull [No. 1019], p. 
       303. 
500    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. 
500    Analysis of plane-plastic-stress problems with axial 
       symmetry in strain-hardening range, by M.H. Lee Wu [No. 
       1021], p. 359. 
500    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. 
500    Diffusion of chromium in alpha cobalt-chromium solid 
       solutions, by John W. Weeton [No. 1023], p. 397. 
500    Calculation of the lateral control of swept and unswept 
       flexible wings of arbitrary stiffness, by Franklin W. 
       Diederich [No. 1024], p. 413. 
500    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.
500    NACA investigation of fuel performance in piston-type 
       engines, by Henry C. Barnett [No. 1026], p. 453. 
500    Buckling of thin-walled cylinder under axial compression 
       and internal pressure, by Hsu Lo, Harold Crate, and Edward
       B. Schwartz [No. 1027], p. 647. 
500    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. 
500    Compressive strength of flanges, by Elbridge Z. Stowell 
       [No. 1029], p. 675. 
500    Investigation of separation of the turbulent boundary 
       layer, by G.B. Schubauer and P.S. Klebanoff, National 
       Bureau of Standards [No. 1030], p. 689. 
500    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. 
500    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. 
500    Comparison between theory and experiment for wings at 
       supersonic speeds, by Walter G. Vincenti [No. 1033], p. 
       757. 
500    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. 
500    Analysis of means of improving the uncontrolled lateral 
       motions of personal airplanes, by Marion O. McKinney, Jr. 
       [No. 1035], p. 795. 
500    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. 
500    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. 
500    Wind-tunnel investigation of air inlet and outlet openings
       on a streamline body, by John V. Becker [No. 1038], p. 
       887. 
500    On the particular integrals of the Prandtl-Busemann 
       iteration equations for the flow of a compressible fluid, 
       by Carl Kaplan [No. 1039], p. 909. 
500    Spectra and diffusion in a round turbulent jet, by Stanley
       Corrsin and Mahinder S. Uberoi, Johns Hopkins University 
       [No. 1040], p. 915. 
500    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. 
500    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. 
500    A numerical method for the stress analysis of stiffened-
       shell structures under nonuniform temperature 
       distributions, by Richard R.    Heldenfels [No. 1043], p. 
       1019. 
500    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. 
500    Supersonic flow around circular cones at angles of attack,
       by Antonio Ferri [No. 1045], p. 1055. 
500    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. 
500    The stability of the compression cover of box beams 
       stiffened by posts, by Paul Seide and Paul F. Barrett [No.
       1047], p. 1087. 
500    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. 
500    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. 
500    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. 
500    An analysis of base pressure at supersonic velocities and 
       comparison with experiment, by Dean R. Chapman [No. 1051],
       p. 1187. 
500    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. 
500    Investigation of turbulent flow in a two-dimensional 
       channel, by John Laufer, California Institute of 
       Technology [No. 1053], p. 1247. 
500    Integrals and integral equations in linearized wing theory,
       by Harvard Lomax, Max A. Heaslet, and Franklyn B. Fuller 
       [No. 1054], p. 1267. 
500    Comparison of theoretical and experimental heat-transfer 
       characteristics of bodies of revolution at supersonic 
       speeds, by Richard Scherrer [No. 1055], p. 1301. 
500    Theoretical antisymmetric span loading for wings of 
       arbitrary plan form at subsonic speeds, by John DeYoung 
       [No. 1056], p. 1317. 
500    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. 
500    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. 
533    Electronic reproduction.|bChester, Vt.:|cNewsBank, inc.,
       |d2008.|nAvailable via the World Wide Web.|nAccess 
       restricted to Readex U.S. Congressional Serial Set 
       subscribers. 
540    Copyright 2008 by NewsBank, Inc. All rights reserved. 
655 07 Aeronautics.|2Readex congressional thesaurus 
655 07 Aircraft engines.|2Readex congressional thesaurus 
655 07 Aircraft parts.|2Readex congressional thesaurus 
655 07 Airplanes.|2Readex congressional thesaurus 
655 07 Transportation research.|2Readex congressional thesaurus 
655  7 Annual Reports.|2Readex congressional thesaurus 
655  7 Monographs.|2Readex congressional thesaurus 
700 1  Alksne, Alberta. 
700 1  Allen, H. Julian. 
700 1  Barmby, J.G. 
700 1  Barnett, Henry C. 
700 1  Barrett, Paul F. 
700 1  Beck, Edgar B. 
700 1  Becker, John V. 
700 1  Bird, John D. 
700 1  Braslow, Albert L. 
700 1  Burrows, Dale L. 
700 1  Chapman, Dean R. 
700 1  Cohen, Doris. 
700 1  Corrsin, Stanley. 
700 1  Crate, Harold. 
700 1  Creager, Marcus O. 
700 1  Cunningham, Herbert J. 
700 1  Delano, James B. 
700 1  Desmon, Leland G. 
700 1  DeYoung, John. 
700 1  Diederich, Franklin W. 
700 1  Donegan, James J. 
700 1  Eckert, E.R.G.,|q(Ernst Rudolf Georg) 
700 1  Emery, James C. 
700 1  Erwin, John R. 
700 1  Ferri, Antonio. 
700 1  Fischel, Jack. 
700 1  Freeman, J.W.,|q(John W.) 
700 1  Fuller, Franklyn B. 
700 1  Garrick, I.E. 
700 1  Gates, Ordway B.,|cJr. 
700 1  Gendler, Selwyn. 
700 1  Godfrey, Douglas. 
700 1  Goin, Kennith L. 
700 1  Goodman, I.A. 
700 1  Goodwin, Glen. 
700 1  Gordon, Sanford. 
700 1  Heaslet, Max A. 
700 1  Heldenfels, Richard R. 
700 1  Horton, Elmer A. 
700 1  Houbolt, John C. 
700 1  Huff, Vearl N. 
700 1  Humble, Leroy V. 
700 1  Jackson, Thomas W. 
700 1  Jaquet, Byron M. 
700 1  Jones, Arthur L. 
700 1  Kaplan, Carl. 
700 1  Klebanoff, P.S.,|q(Philip S.) 
700 1  Laufer, John. 
700 1  Lin, Chia Chiao. 
700 1  Lo, Hsu. 
700 1  Loftin, Laurence K.,|cJr. 
700 1  Lomax, Harvard. 
700 1  Low, George M. 
700 1  Lowdermilk, Warren H. 
700 1  Mayers, J. 
700 1  McGowan, William A. 
700 1  McKinney, Marion O.,|cJr. 
700 1  Mendelson, Alexander. 
700 1  Merten, Kenneth F. 
700 1  Mirels, Harold. 
700 1  Morrell, Virginia E. 
700 1  Oppenheimer, Frank L. 
700 1  Otto, Edward W. 
700 1  Pearson, Henry A. 
700 1  Perkins, Edward W. 
700 1  Queijo, M.J. 
700 1  Quinn, John H.,|cJr. 
700 1  Racisz, Stanley F. 
700 1  Reynolds, E.E. 
700 1  Scherrer, Richard. 
700 1  Schubauer, Galen B.,|q(Galen Brandt) 
700 1  Schwartz, Edward B. 
700 1  Scull, Wilfred E. 
700 1  Seide, Paul. 
700 1  Serijan, K.T. 
700 1  Stalder, Jackson R. 
700 1  Stein, Manuel. 
700 1  Sternfield, Leonard. 
700 1  Stowell, Elbridge Z. 
700 1  Taylor, Burt L.,|cIII. 
700 1  Tetervin, Neal. 
700 1  Trout, Arthur M. 
700 1  Uberoi, Mahinder S. 
700 1  Vincenti, Walter G. 
700 1  Visconti, Fioravante. 
700 1  Watkins, Charles E. 
700 1  Watson, James M. 
700 1  Weeton, John W. 
700 1  White, A.E. 
700 1  Wilcox, E. Clinton. 
700 1  Wise, P.H. 
700 1  Wolhart, Walter D. 
700 1  Wu, M.H. Lee. 
710 1  United States.|bNational Advisory Committee for 
       Aeronautics. 
830  0 Senate document (United States. Congress. Senate) ;|v82nd 
       Congress, no. 93 
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