Format:
Online-Ressource (1011 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. 12003
Note:
A reevaluation of data on atmospheric turbulence and airplane gust loads for application in spectral calculations, by Harry Press, May T. Meadows, and Ivan Hadlock, NACA [No. 1272], p. 489
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A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds, by Harvard Lomax and Maz A. Heaslet, NACA [No. 1282], p. 709
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A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound, by Richard T. Whitcomb, NACA [No. 1273], p. 519
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A theory for stability and buzz pulsation amplitude in ram jets and an experimental investigation including scale effects, by Robert L. Trimpi, NACA [No. 1265], p. 295
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A thermal equation for flame quenching, by A.E. Potter, Jr., and A.L. Berlad, NACA [No. 1264], p. 287
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A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds, by Benjamin H. Beam, NACA [No. 1258], p. 165
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An analysis of the stability and ultimate compressive strength of short sheet-stringer panels with special reference to the influence of the riveted connection between sheet and stringer, by Joseph W. Semonian and James P. Peterson, NACA [No. 1255], p. 113
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Axially symmetric shapes with minimum wave drag, by Max. A. Heaslet and Franklyn B. Fuller, NACA [No. 1256], p. 131
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Charts for estimating performance of high-performance helicopters, by Alfred Gessow and Robert J. Tapscott, NACA [No. 1266], p. 319
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Contributions on the mechanics of boundary-layer-transition, by G.B. Schubauer and P.S. Kelbanoff, National Bureau of Standards, [No. 1289], p. 853
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Cooperative investigation of relationship between static and fatigue properties of wrought N-155 alloy at elevated temperatures, by NACA Subcommittee on Power-Plant Materials, [No. 1288, p. 817
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Development of craze and impact resistance in glazing plastics by multiaxial stretching, by G.M. Kline, I. Wolock, B.M. Axilrod, M.A. Sherman, D.A. George, and V. Cohen, National Bureau of Standards, [No. 1290], p. 865
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Effect of interaction on landing-gear behavior and dynamic leads in a flexible airplane structure, by Francis E. Cook and Benjamin Milwitzky, NACA [No. 1278], p. 619
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Extrapolation techniques applied to matrix methods in neutron diffusion problems, by Robert R. McCready, NACA [No. 1283], p. 747
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Flight determination of drag of normal-shock nose inlets with various cowling profiles at Mach numbers from 0.9 to 1.5, by R.I. Sears, C.F. Merlet, and L.W. Putland, NACA [No. 1281], p. 689
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Friction, wear, and surface damage of metals as affected by solid surface films, by Edmond E. Bisson, Robert L. Johnson, Max A. Swikert and Douglas Godfrey, NACA [No. 1254], p. 91
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Interaction of a free flame front with a turbulence field, by Maurice Tucker, NACA [No. 1277], p. 599
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Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 [degrees], by Richard E. Kuhn and John W. Draper, NACA [No. 1263], p. 247
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Lift hysteresis at stall as an unsteady boundary-layer phenomenon, by Franklin K. Moore, NACA [No. 1291], p. 881
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List of technical reports, p. III
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On boattail bodies of revolution having minimum wave drag, by Keith C. Harder and Conrad Rennemann, Jr., NACA [No. 1271], p. 479
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On the kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow, by Charles E. Watkins and Julian H. Berman, NACA [No. 1287], p. 147
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Plastic deformation of aluminum single crystals at elevated temperatures, by R.D. Johnson, A.P. Young, and A.D. Schwope, Battelle Memorial Institute, [No. 1267], p. 353
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Propagation of free flame in a turbulent gas stream, by William R. Mickelsen and Norman E. Ernstein, NACA [No. 1286], p. 773
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Review of experimental investigations of liquid-metal heat transfer, by Bernard Lubarsky and Samuel J. Kaufman, NACA [No. 1270], p. 445
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Second-order subsonic airfoil theory including edge effects, by Milton D. Van Dyke, NACA [No. 1274], p. 541
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Some possibilities of using gas mixtures other than air in aerodynamic research, by Dean R. Chapman, NACA [No. 1259], p. 179
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Spark ignition of flowing gases, by Clyde C. Swett, Jr., NACA [No. 1287], p. 799
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Studies of the speed stability of a tandem helicopter in forward flight, by Robert J. Tapscott and Kenneth B. Amer, NACA [No. 1260], p. 201
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Summary of derived gust velocities obtained from measurements within thunderstorms, by H.B. Tolefson, NACA [No. 1285], p. 765
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Table of contents, p. II
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The near noise field of static jets and some model studies of devises for noise reduction, by Leslie W. Lassiter and Harvey H. Hubbard, NACA [No. 1261], p. 213
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The proper combination of lift loading for least drag on a supersonic wing, by Frederick C. Grant, NACA [No. 1275], p. 565
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Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows, by James J. Kramer, Vasily D. Prian, and Chung-Hua Wu, NACA [No. 1279], p. 649
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Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow, by Harry L. Runyan, Donald S. Woolston, and A. Gerald Rainey, NACA [No. 1262], p. 225
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Theoretical calculations of the pressures, forces, and moments at supersonic speeds due to various lateral motions actin on thin isolated vertical tails, by Kenneth Margolis and Percy J. Bobbitt, NACA [No. 1268], p. 385
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Theoretical investigation of flutter of two-dimensional flat panels with one surface exposed to supersonic potential flow, by Herbert C. Nelson and Herbert J. Cunningham, NACA [No. 1280], p. 665
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Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow, by M.J. Queijo, NACA [No. 1269], p. 429
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Theory of wing-body drag at supersonic speeds, by Robert T. Jones, NACA [No. 1284], p. 757
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Wind-tunnel and flight investigations of the use of leading-edge area suction for the purpose of increasing the maximum lift coefficient of a 35 [degree] swept-wing airplane, by Curt A. Helzhauser and Richard S. Bray, NACA [No. 1276], p. 575
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