UID:
(DE-602)gbv_754808181
Format:
Online-Ressource (1503 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 12180
Note:
A comparative analysis of the performance of long-range hypervelocity vehicles, by Alfred J. Eggers, Jr., H. Julian Allen, and Stanford E. Neice, NACA [No. 1382], p. 1141
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A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts, by C.C. Shufflebarger, Chester B. Payne, and George L. Cahen, NACA [No. 1365], p. 669
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A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary layer transition, by Albert F. Von Doenhoff and Elmer A. Horton, NACA [No. 1349], p. 239
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A method for simulating the atmospheric entry of long-range ballistic missiles, by A.J. Eggers, Jr., NACA [No. 1378], p. 1009
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A method of computing the transient temperature of thick walls form arbitrary variation of adiabatic-wall temperature and heat-transfer coefficient, by P.R. Hill, NACA [No. 1372], p. 877
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A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures, by Elbridge Z. Stowell, NACA [No. 1343], p. 125
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A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver, by Leonard Sternfield, NACA [No. 1344], p. 131
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A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at hight supersonic speeds, by H. Julian Allen and A.J. Eggers, Jr. NACA [No. 1381], p. 1125
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A summary of preliminary investigations into the characteristics of combustion screech in ducted burners, by Lewis Laboratory Staff, NACA [No. 1384], p. 1195
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A theoretical and experimental study of planing surfaces including effects of cross section and plan form, by Charles L. Shuford, Jr., NACA [No. 1355], p. 373
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A variational theorem for creep with applications to plates and columns, by J. Lyell Sanders, Jr., Harvey G. McComb, Jr., and Floyd R. Schlechte, NACA [No. 1342], p. 117
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A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96, by Albert J. Evans and George Liner, NACA [No. 1375], p. 933
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An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed-tip wings at supersonic speeds, by William B. Boatright, NACA [No. 1380], p. 1067
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An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds, by Maurice S. Cahn, NACA [No. 1353], p. 327
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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, NACA [No. 1361], p. 593
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Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35 [degree] swept-wing airplane, by Woodrow L. Cook, Seth B. Anderson, and George E. Cooper, NACA [No. 1370], p. 823
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Blowing-type boundary-layer control as applied to the trailing-edge flaps of a 25 [degree] swept-wing airplane, by Mark W. Kelly, Seth B. Anderson, and Robert C. Innis, NACA [No. 1369], p. 799
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Boron and zirconium from crucible refractories in a complex heat-resistant alloy, by R.F. Decker, John P. Rowe, and J.W. Freeman, University of Michigan, [No. 1392], p. 1457
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Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine, by Leslie W. Lassiter and Robert W. Hess, NACA [No. 1367], p. 703
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Characteristics of the Langley 8-foot transonic tunnel with slotted test section, by Ray H. Wright, Virgil S. Ritchie, and Albin O. Pearson, NACA [No. 1389], p. 1297
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Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number, by Eli Reshotku and Ivan E. Beckwith, NACA [No. 1379], p. 1016
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Differential equations of motion for combined flapwise vending, chordwise bending, and torsion of twisted non-uniform rotor blades, by John C. Houbolt and George W. Brooks, NACA [No. 1346], p. 179
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Ditching investigations of dynamic models and effects of design parameters on ditching characteristics, by Lloyd J. Fisher and Edward L. Hoffman, NACA [No. 1347], p. 197
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Drag minimization for wings and bodies in supersonic flow, by Max A. Heaslet and Franklyn B. Fuller, NACA [No. 1385], p. 1213
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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, NACA [No. 1354], p. 359
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Effect of fuel variables on carbon formation in turbojet-engine combustors, by Edmund R. Jonash, Jerrold D. Wear, and William P. Cook, NACA [No. 1352], p. 309
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Elliptic cones alone and with wings at supersonic speeds, by Leland H. Jorgensen, NACA [No. 1376], p. 975
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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, NACA [No. 1357], p. 461
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Full-scale investigation of several jet-engine noise-reduction nozzles, by Willard D. Coles and Edmund E. Callaghan, NACA [No. 1387], p. 1249
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Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality, by B. Porter Brown, NACA [No. 1348], p. 225
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Growth of disturbances in a flame-generated shear region, by Perry L. Blackshear, Jr., NACA [No. 1360], p. 546
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Incompressible flutter characteristics of representative aircraft wings, by C.H. Wilts, California Institute of Technology, [No. 1390], p. 1385
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Investigation of a nonlinear control system, by I. Flugge-Lotz, C.F. Taylor, and H.E. Lindberg, Stanford University, [No. 1391], p. 1423
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Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, by Dean R. Chapman, Donald M. Kuehn, and Howard K. Larson, NACA [No. 1356], p. 419
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Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2, by Leland H. Jorgensen and Edward W. Perkins, NACA [No. 1371], p. 857
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Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4, by Edward W. Perkins, Leland H. Jorgensen, and Simon C. Sommer, NACA [No. 1386], p. 1231
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List of technical reports, p. III
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Measurement of static pressure on aircraft, by William Gracey, NACA [No. 1364], p. 643
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Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72, by Max C. Kurbjun and Arthur W. Vogeley, NACA [No. 1377], p. 999
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Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions, by F.B. Gustafson and Robert J. Topscott, NACA [No. 1350], p. 255
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NACA Research on slurry fuels, by M.L. Pinns, W.T. Olson, H.C. Barnett, and R. Breitwieser, NACA [No. 1388], p. 1273
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On flow of electrically conducting fluids over a flat plate in presence of a transverse magnetic field, by Vernon J. Rossow, NACA [No. 1358], p. 489
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Origin and prevention of crash fires in turbojet aircraft, by I. Irving Pinkel, Solomon Weiss, G. Merritt Preston, and Gerard J. Pesman, NACA [No. 1363], p. 623
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Survey of hydrogen combustion properties, by Isadore L. Drell and Frank E. Belles, NACA [No. 1383], p. 1161
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Systemic two-dimensional cascade tests of NACA 65-Series compressor blades at low speeds, by James C. Emery, L. Joseph Herrig, John R. Erwin, and A. Richard Felix, NACA [No. 1368], p. 713
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Table of contents, p. II
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The mechanism of thermal-gradient mass transfer in the sodium hydroxide - nickel system, by Charles E. May, NACA [No. 1366], p. 683
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The response of an airplane to random atmospheric disturbances, by Franklin W. Diederich, NACA [No. 1345], p. 142
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The similarity rules for second-order subsonic and supersonic flow, by Milton D. Van Dyke, NACA [No. 1374], p. 925
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Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus- and liner cross-sectional areas, by Charles C. Graves and Jack S. Grobman, NACA [No. 1373], p. 899
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Theoretical combustion performance of several high-energy fuels for ramjet engines, by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon, NACA [No. 1362], p. 605
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Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades, by Robert P. Coleman and Arnold M. Feingold, NACA [No. 1351], p. 267
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Thin airfoil theory based on approximate solution of the transonic flow equation, by John R. Spreiter and Alberta Y. Alksne, NACA [No. 1359], p. 509
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