Format:
Online-Ressource (1660 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. 12096
Note:
A second-order shock-expansion method applicable to bodies of revolution near zero lift, by Clarence A Syvertson and David H. Dennis, NACA [No. 1328], p. 1127
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A summary and analysis of the low-speed longitudinal characteristics of swept wings at high Reynolds numbers, by G. Chester Furlong and James G. McHugh, NACA [No. 1339], p. 1390
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A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes, by John R. Spreiter and Alvin H. Sacks, NACA [No. 1296], p. 81
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Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers, by Julian D. Maynard and Leland B. Salters, Jr., NACA [No. 1309], p. 651
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An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane, by Richard B. Skoog, NACA [No. 1298], p. 125
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An evaluation of four experimental methods for measuring mean properties of supersonic turbulent boundary layer, by George J. Nothwang, NACA [No. 1320], p. 939
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An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel, by Charles M. McLellan, Mitchel H. Bertram, and John A. Moore, NACA [No. 1310], p. 675
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An investigation of single- and duel-rotation propellers at positive and negative thrust, and in combination with an NACA 1-Series D-Type cowling at mach numbers up to 0.84, by Robert M. Reynolds, Robert I. Sammonds, and John H. Walker, NACA [No. 1336], p. 1269
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Attention in shock tube due to unsteady-boundary-layer action, by Harold Mirels, NACA [No. 1333], p. 1227
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Average properties of compressible laminar boundary layer on flat plate with unsteady flight velocity, by Franklin K. Moore and Simon Ostrach, NACA [No. 1325], p. 1037
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Basic considerations in the combustion of hydrocarbon fuels with air, by Propulsion Chemistry Division, Lewis Flight Propulsion Laboratory, NACA [No. 1300], p. 187
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Bodies of revolution having minimum drag at high supersonic airspeeds, by A.J. Eggers, Jr., Meyer M. Resnikoff, and David H. Dennis, NACA [No. 1306], p. 555
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Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7, by Rinaldo J. Brun, NACA [No. 1317], p. 785
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Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data, by James J. Donegan and Carl R. Huss, NACA [No. 1324], p. 1023
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Correlation, evaluation, and extension of linearized theories for tire motion and wheel shimmy, by Robert F. Smiley, NACA [No. 1299], p. 137
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Determination of longitudinal stability and control characteristics from free-flight model tests with results at transonic speeds for three airplane configurations, by Clarence L. Gillis and Jess L. Mitchell, NACA [No. 1337], p. 1327
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Determination of vortex paths by series expansion technique with application to cruciform wings, by Alberta Y. Alksne, NACA [No. 1311], p. 693
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Experimental and predicted longitudinal and lateral-directional response characteristics of a large flexible 35 [degree] swept-wing airplane at an altitude of 35,000 feet, by Henry A. Cole, Jr., Stuart C. Brown, and Euclid C. Holleman, NACA [No. 1330], p. 1165
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Exploratory investigation of boundary-layer transition on a hollow cylinder at a mach number of 6.9, by Mitchel H. Bertram, NACA [No. 1313], p. 723
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Far noise-field of air jets and jet engines, by Edmund E. Callaghan and Willard D. Coles, NACA [No. 1329], p. 1147
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Flight and analytical methods for determining the coupled vibration response of tandem helicopters, by John E. Yeates, Jr., George W. Brooks, and John C. Houbolt, NACA [No. 1326], p. 1049
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Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes, by William H. Phillips, Helmut A. Kuehnel and James B. Whitten, NACA [No. 1304], p. 505
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Induced velocities near a lifting rotor with nonuniform disk loading, by Harry H. Heyson and S. Katzoff, NACA [No. 1319], p. 850
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Influence of alloying upon grain-boundary creep, by F.N. Rhines, W.E. Bond, and M.A. Kissel, Carnegie Institute of Technology, [No. 1331], p. 1205
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Influence of hot-working conditions on high-temperature properties of a heat-resistant alloy, by John F. Ewing and J.W. Freeman, University of Michigan, [No. 1341], p. 1599
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Investigation of downwash, sidewash, and Mach number distribution behind a rectangular wing at a mach number of 2.41 by David Adamson and William B. Boatright, NACA [No. 1340], p. 1541
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Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures, by Eldon E. Mathauser and William D. Deveikis, NACA [No. 1308], p. 637
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Investigation of the laminar aerodynamic heat-transfer characteristics of a hemisphere-cylinder in the Langley 11-inch hypersonic tunnel at Mach number 6.8, by Davis H. Crawford and William D. McCauley, NACA [No. 1323], p. 1001
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Lift and center of pressure of wing-body-tail combination at subsonic, transonic, and supersonic speeds, by William C. Pitts, Jack N. Nielsen, and George E. Kaatari, NACA [No. 1307], p. 567
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Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings a supersonic speeds, by Percy J. Bobitt, NACA [No. 1301], p. 455
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List of technical reports, p. III
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Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall, by A. Gerald Rainey, NACA [No. 1305], p. 520
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Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow, by Harry L. Runyan and Donald S. Woolston, NACA [No. 1321], p. 971
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Minimum wave drag for arbitrary arrangements of wings and bodies, by Robert T. Jones, NACA [No. 1335], p. 1263
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Near noise field of a jet-engine exhaust, by Walton L. Howes, Edmund E. Callaghan, Willard D. Coles, and Harold R. Mull, NACA [No. 1338], p. 1355
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Nonlifting wing-body combinations with certain geometric restraints having minimum wave drag at low subsonic speeds, by Harvard Lomax, NACA [No. 1297], p. 113
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On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders, by Robert W. Leonard and John M. Hedgepeth, NACA [No. 1302], p. 475
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On slender-body theory at transonic speeds, by Keith C. Harder and E.B. Klunker, NACA [No. 1315], p. 765
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Relation of turbojet and ramjet combustion efficiency to second-order reaction kinetics and fundamental flame speed, by J. Howard Childs, Thaine W. Reynolds, and Charles C. Graves, NACA [No. 1334], p. 1249
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Seat design for crash worthiness, by I. Irving Pinkel and Edmund G. Rosenberg, NACA [No. 1332], p.1211
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Some effects on bluntness on boundary-layer transition and heat transfer at supersonic speeds, by W.E. Moeckel, NACA [No. 1312], p. 709
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Summary of scale-model thrust-reverser investigation, by John H. Povolny, Fred W. Steffen and Jack G. McArdle, NACA [No. 1314], p. 751
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Table of contents, p. II
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Theoretical calculation for the power spectra of the rolling and yawing moments of a wing in random turbulence, by John M. Eggleston and Franklin W. Diederich, NACA [No. 1321], p. 951
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Three-dimensional transonic flow theory applied to slender wings and bodies, by Max A. Heaslet and John R. Spreiter, NACA [No. 1318], p. 820
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Torsional stiffness of thin-walled shells having reinforcing cores and rectangular, triangular, or diamond cross section, by Harvey G. McComb, Jr., NACA [No. 1316], p. 771
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Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack - subsonic, transonic, and supersonic speeds, by William Gracey, NACA [No. 1303], p. 495
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theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tables of vortex-induced velocities, by William J. Alford, Jr., NACA [No. 1327], p. 1083
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