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  • 1
    UID:
    gbv_754750167
    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 , 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 , 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 , 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 , A thermal equation for flame quenching, by A.E. Potter, Jr., and A.L. Berlad, NACA [No. 1264], p. 287 , 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 , 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 , Axially symmetric shapes with minimum wave drag, by Max. A. Heaslet and Franklyn B. Fuller, NACA [No. 1256], p. 131 , Charts for estimating performance of high-performance helicopters, by Alfred Gessow and Robert J. Tapscott, NACA [No. 1266], p. 319 , Contributions on the mechanics of boundary-layer-transition, by G.B. Schubauer and P.S. Kelbanoff, National Bureau of Standards, [No. 1289], p. 853 , 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 , 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 , 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 , Extrapolation techniques applied to matrix methods in neutron diffusion problems, by Robert R. McCready, NACA [No. 1283], p. 747 , 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 , 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 , Interaction of a free flame front with a turbulence field, by Maurice Tucker, NACA [No. 1277], p. 599 , 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 , Lift hysteresis at stall as an unsteady boundary-layer phenomenon, by Franklin K. Moore, NACA [No. 1291], p. 881 , List of technical reports, p. III , On boattail bodies of revolution having minimum wave drag, by Keith C. Harder and Conrad Rennemann, Jr., NACA [No. 1271], p. 479 , 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 , 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 , Propagation of free flame in a turbulent gas stream, by William R. Mickelsen and Norman E. Ernstein, NACA [No. 1286], p. 773 , Review of experimental investigations of liquid-metal heat transfer, by Bernard Lubarsky and Samuel J. Kaufman, NACA [No. 1270], p. 445 , Second-order subsonic airfoil theory including edge effects, by Milton D. Van Dyke, NACA [No. 1274], p. 541 , Some possibilities of using gas mixtures other than air in aerodynamic research, by Dean R. Chapman, NACA [No. 1259], p. 179 , Spark ignition of flowing gases, by Clyde C. Swett, Jr., NACA [No. 1287], p. 799 , 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 , Summary of derived gust velocities obtained from measurements within thunderstorms, by H.B. Tolefson, NACA [No. 1285], p. 765 , Table of contents, p. II , 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 , The proper combination of lift loading for least drag on a supersonic wing, by Frederick C. Grant, NACA [No. 1275], p. 565 , 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 , 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 , 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 , 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 , 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 , Theory of wing-body drag at supersonic speeds, by Robert T. Jones, NACA [No. 1284], p. 757 , 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 , © 2008 by NewsBank, Inc. All rights reserved
    Language: English
    URL: Volltext  (Deutschlandweit zugänglich)
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  • 2
    UID:
    almafu_9958352942402883
    Format: 1 online resource (1024 p.)
    ISBN: 9781400875030
    Series Statement: Princeton Legacy Library ; 2421
    Content: Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods.Originally published in 1961.The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
    Note: Frontmatter -- , FOREWORD -- , PREFACE -- , CONTENTS -- , PART ONE. HIGH SPEED PROBLEMS OF AIRCRAFT -- , SECTION A. METHODS OF PERFORMANCE CALCULATION AT HIGH SPEED -- , SECTION B. STABILITY AND CONTROL OF HIGH SPEED AIRCRAFT -- , SECTION C. AERO ELASTICITY AND FLUTTER -- , PART TWO. WIND TUNNEL TECHNIQUES -- , SECTION D. PRINCIPLES OF MODEL TESTING -- , SECTION E. INTRODUCTORY DISCUSSION OF HIGH SPEED TEST TECHNIQUES -- , SECTION F. TRANSONIC WIND TUNNELS -- , SECTION G. SUPERSONIC TUNNELS -- , SECTION H. HYPERSONIC EXPERIMENTAL FACILITIES -- , SECTION I. LOW DENSITY WIND TUNNELS -- , SECTION J. THE SHOCK TUBE -- , SECTION K. WIND TUNNEL MEASUREMENTS -- , PART THREE. FREE FLIGHT TECHNIQUES -- , SECTION L. OBJECTIVES OF FREE FLIGHT RESEARCH -- , SECTION M. INSTRUMENTED MODELS IN FREE FLIGHT -- , SECTION N. PILOTED AIRCRAFT TESTING -- , SECTION O. FREE FLIGHT RANGE METHODS -- , INDEX , In English.
    Language: English
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