Umfang:
Online-Ressource (1386 p)
,
illustrations, tables
Ausgabe:
Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980
Serie:
United States congressional serial set serial set no. 11917
Anmerkung:
A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form, by John B. McDevitt, NACA [No. 1253], p. 1355
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A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds, by Seth B. Anderson and Richard S. Bray, NACA [No. 1237], p. 843
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A free-flight wind tunnel for aerodynamic testing at hypersonic speeds, by Alvin Seiff, NACA [No. 1222], p. 381
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A method for the design of swept-back wings warped to produce specified flight characteristics at supersonic speeds, by Warren A. Tucker, NACA [No. 1226], p. 459
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A theoretical and experimental investigation of the lift and drag characteristics of hydrofoils at subcritical and supercritical speeds, by Kenneth L. Wadlin, Charles L. Shuford, Jr., and John R. McGehee, NACA [No. 1232], p. 661
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A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution, by A.J. Eggers, Jr., and Raymond C. Savin, NACA [No. 1249], p. 1189
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An experimental study of applied ground loads in landing, by Benjamin Milwitzky, Dean C. Lindquist, and Dexter M. Potter, NACA [No. 1248], p. 1155
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An investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61, by K.R. Czarnecki and Archibald R. Sinclair, NACA [No. 1240], p. 929
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An investigation of the maximum lift of wings at supersonic speeds, by James J. Gallagher and James N. Mueller, NACA [No. 1227], p. 477
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Analog study of interacting and non-interacting multiple-loop control systems for turbojet engines, by George J. Pack and W.E. Philips, Jr., NACA [No. 1212], p. 97
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Analysis and calculation by integral methods of laminar compressible boundary layer with heat transfer and with and without pressure gradient, by Morris Morduchow, Polytechnic Institute of Brooklyn, [No. 1245], p. 1065
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Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers, by Robert G. Diessler, NACA [No. 1210], p. 69
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Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds, by Morris D. Friedman and Doris Cohen, NACA [No. 1236], p. 835
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Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow, by Franklin W. Diederich and Martin Zlotnick, NACA [No. 1228], p. 505
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Calculation of laminar heat transfer around cylinders of arbitrary cross section and transpiration-cooled walls with application to turbine blade cooling, by E.R.G. Eckert and J.N.B. Livingood, NACA [No. 1220], p. 339
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Characteristics of turbulence in a boundary layer with zero pressure gradient, by P.S. Klebanoff, National Bureau of Standards, [No. 1247], p. 1135
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Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight, by Kenneth B. Amer and Alfred Gessow, NACA [No. 1216], p. 185
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Determination of lateral -stability derivatives and transfer-function coefficients from frequency-response data for lateral motions, by James J. Donegan, Samuel W. Robinson, Jr., and Ordway B. Gates, Jr., NACA [No. 1225], p. 439
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Effect of ground interference on aerodynamic and flow characteristics of a 42 [degree] sweptback wing Reynolds numbers up to 6.8X10(6), by G. Chester Furlong and Thomas V. Bollech, NACA [No. 1218], p. 251
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Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model, by Alex Goodman and David F. Thomas, NACA [No. 1224], p. 407
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Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds, by Thomas C. O'Bryan, Edward C.B. Danforth, and J. Ford Johnston, NACA [No. 1239], p. 915
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Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature, by Patrick L. Donoughe and John N.B. Livingood, NACA [No. 1229], p. 573
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Experimental investigation of free-convection heat transfer in vertical tube at large Grashof numbers, by E.R.G. Eckert and A.J. Diaguila, NACA [No. 1211], p. 83
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Free-stream boundaries of turbulent flows, by Stanley Corrsin and Alan L. Kistler, The Johns Hopkins University, [No. 1244], p. 1033
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Generalized indicial forces on deforming rectangular wings in supersonic flight, by Harvard Lomax, Franklyn B. Fuller, and Loma Sluder, NACA [No. 1230], p. 595
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High-resolution autoradiography, by George C. Towe, Henry J. Gomberg, and J.W. Freeman, University of Michigan, [No. 1243], p. 979
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Impingement of cloud droplets on a cylinder and procedure for measuring liquid-water content and droplet sized in supercooled clouds by rotating multicylinder method, by R.J. Brun, W. Lewis, P.J. Perkins, and J.S. Serafini, NACA [No. 1215], p. 139
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Investigation at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, by Eugene S. Love, NACA [No. 1238], p. 855
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List of technical reports, p. III
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Measurement and analysis of wing and tail buffeting loads on fighter airplane, by Wilber B. Huston and T.H. Skopinski, NACA [No. 1219], p. 311
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Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory, by Hermon M. Parker, NACA [No. 1213], p. 111
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NACA transonic wind-tunnel test sections, by Ray H. Wright and Vernon G. Ward,NACA [No. 1231], p. 623
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On the kernel function of the integral equation relating the lift of downwash distributions of oscillating finite wings in subsonic flow, by Charles E. Watkins, Harry L. Runyan, and Donald S. Woolston, NACA [No. 1234], p. 703
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Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment, by Jack N. Nielsen, NACA [No. 1252], p. 1299
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Shock-turbulence interaction and the generation of noise, by H.S. Ribner, NACA [No. 1233], p. 682a
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Standard atmosphere - tables and data for altitudes to 65,800 feet, by International Aviation Organization and NACA, [No. 1235], p. 719
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Statistical measurements on contact conditions of 478 transport-airplane landings during routine daytime operations, by Norman S. Silsby, NACA [No. 1214], p. 121
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Stress-analysis of circular semimonocoque cylinders with cutouts, by Harvey G. McComb, NACA [No. 1251], p. 1243
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Table of contents, p. II
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The dynamic-response characteristics of a 35 [degree] swept-wing airplane as determined from flight measurements, by William C. Triplett, Stuart C. Brown, and G. Allan Smith, NACA [No. 1250], p. 1217
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The hydrodynamic characteristics of modified rectangular flate plates having aspect rations of 1.00, 0.25, and 0.125 and operating near a free water surface, by Kenneth L. Wadlin, John A. Ramsen, and Victor L. Vaughan, Jr., NACA [No. 1246], p. 1085
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Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control, by Howard J. Curfman, Jr., NACA [No. 1241], p. 941
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Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates, by A.F. Lietzke, NACA [No. 1223], p. 399
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Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds, by John R. Spreiter and Alverta Alksne, NACA [No. 1217], p. 207
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Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing -vortex system of the lifting model, by Clarence W. Matthews, NACA [No. 1221], p. 361
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Transonic flow past cone cylinders, by George E. Solomon, California Institute of Technology, [No. 1222], p. 963
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