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  • 1
    Book
    Book
    Washington : Off. of Scient. and Technical Information, National Aeronautics and Space Administration
    UID:
    gbv_445616016
    Format: VII, 511 S. 8"
    Series Statement: (NASA SP-38)
    Language: Undetermined
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  • 2
    UID:
    gbv_412321475
    Format: II, 12 S , 4"
    Series Statement: Report / National Advisory Committee for Aeronautics 1062
    Language: English
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  • 3
    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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  • 4
    UID:
    gbv_754626873
    Format: Online-Ressource (1199 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. 11676
    Note: A biharmonic relaxation method for calculating thermal stress in cooled irregular cylinders, by Arthur G. Holms [No. 1059], p. 71 , A study of second-order supersonic flow theory, by Milton D. Van Dyke [No. 1081], p. 489 , A theoretical analysis of the effects of fuel motion on airplane dynamics, by Albert A. Sehy [No. 1080], p. 467 , Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow, by Charles E. Watkins and Julian H. Berman [No. 1099], p. 863 , Airfoil profiles for minimum pressure drag at supersonic velocities -- general analysis with application to linearized supersonic flow, by Dean R. Chapman [No. 1063], p. 129 , An empirically derived basis for calculating the area, rate, and distribution of water-drop impingement on airfoils, by Norman R. Bergrun [No. 1107], p. 1079 , An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer, by Arthur Earl Bryson, Jr. [No. 1094], p. 725 , An iterative transformation procedure for numerical solution of flutter and similar characteristic-value problems, by Myron L. Gossard [No. 1073], p. 303 , Analysis of temperature distribution in liquid-cooled turbine blades, by John N.B. Livingood and W. Byron Brown [No. 1066], p. 169 , Analysis of the effects of wing interference on the tail contributions to the rolling derivatives, by William H. Michael, Jr. [No. 1086], p. 569 , Automatic control systems satisfying certain general criterions on transient behavior, by Aaron S. Boksenbom and Richard Hood [No. 1068], p. 207 , Axisymmetric supersonic flow in rotating impellers, by Arthur W. Goldstein [No. 1083], p. 523 , Chordwise and compressibility corrections to slender-wing theory, by Harvard Lomax and Loma Sluder [No. 1105], p. 1049 , Comparison of high-speed operating characteristics of size 215 cylindrical-roller bearings as determined in turbojet engine and in laboratory test rig, by E. Fred Macks and Zolton N. Nemeth [No. 1084], p. 537 , Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume -- 2-alkylbiphenyl and the two isomeric 2-alkylbicyclohexyl series, by Irving A. Goodman and Paul H. Wise [No. 1065], p. 159 , Detailed computational procedure for design of cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello, Robert L. Cummings, and John T. Sinnette, Jr. [No. 1060], p. 91 , Discussion of boundary-layer characteristics near the wall of an axial-flow compressor, by Artur Mager, John J. Mahoney, and Ray E. Budinger [No. 1085], p. 549 , Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons, by Jack Fischel, Rodger L. Naeseth, John R. Hagerman, and William M. O'Hare [No. 1091], p. 649 , Effect of initial mixture temperature on flame speed of methane-air, propane-air and ethylene-air mixtures, by Gordon L. Dugger [No. 1061], p. 105 , Effects of compressibility on the performance of two full-scale helicopter rotors, by Paul J. Carpenter [No. 1078], p. 449 , Effects on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system, by Charles W. Mathews, Donald B. Talmadge, and James B. Whitten [No. 1076], p. 375 , Experimental aerodynamic derivatives of a sinusoidally oscillating airfoil in two-dimensional flow, by Robert L. Halfman [No. 1108], p. 1101 , Experimental determination of the effect of horizontal tail size, tail length, and vertical location on low-speed static longitudinal stability and damping in pitch of a model having 45 [degree] sweptback wing and tail surfaces, by Jacob H. Lichtenstein [No. 1096], p. 789 , Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities, by Dean R. Chapman, William R. Wimbrow, and Robert H. Kester [No. 1109], p. 1145 , Flight investigation a mechanical feel device in an irreversible elevator control system of a large airplane, by B. Porter Brown, Robert G. Chilton, and James B. Whitten [No. 1101], p. 919 , Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane, by John P. Campbell, Paul A. Hunter, Donald E. Hewes, and James B. Whitten [No. 1092], p. 697 , Generalization of boundary-layer momentum-integral equations to three-dimensional flows including those of rotating system, by Artur Mager [No. 1067], p. 191 , Generalized theory for seaplane impact, by Benjamin Milwitzky [No. 1103], p. 951 , Heat transfer to bodies in a high-speed rarified gas stream, by Jackson R. Stalder, Glen Goodwin and Marcus O. Creager [No. 1093] , Hydrodynamic impact of a system with a single elastic mode. I-- Theory and generalized solution with an application to an elastic airframe, by Wilbur L. Mayo [No. 1074], p. 349 , Hydrodynamic impact of a system with a single elastic mode. II - Comparison of experimental force and response with theory, by Robert W. Miller and Kenneth F. Merton [No. 1075], p. 367 , Inelastic column behavior, by John E. Duberg and Thomas W. Wilder, III [No. 1072], p. 286 , Internal-liquid-film-cooling experiments with airstream temperatures to 2000 [degrees] F in 2- and 4- inch diameter horizontal tubes, by George R. Kinney, Andrew E. Abramson and John L. Sloop [No. 1087], p. 581 , Investigation of wear and friction properties under sliding conditions of some materials suitable for cages of rolling-contact bearings, by Robert L. Johnson, Max A. Swikert, and Edmond E. Bisson [No. 1062], p. 117 , List of technical reports, p. III , Lubrication and cooling studies of cylindrical-roller bearings at high speeds, by E. Fred Macks and Zolton N. Nemeth [No. 1064], p. 143 , Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data, by James J. Donegan and Henry A. Pearson [No. 1070], p. 233 , Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data, by James C. Sivell and Gertrude C. Westrick [No. 1090], p. 623 , Method of analysis for compressible flow through mixed-flow centrifugal impellers of arbitrary design, by Joseph T. Hamrick, Ambrose Ginsburg, and Walter M. Osborn [No. 1082], p. 513 , On a solution of the nonlinear differential equation for transonic flow past a wave-shaped wall, by Carl Kaplan [No. 1069], p. 221 , On reflection of shock waves from boundary layers, by H.W. Liepmann, A. Roshko and S. Dhawan [No. 1100], p. 889 , Preliminary investigation of a new type of supersonic inlet, by Antonio Ferri and Louis M. Nucci [No. 1104], p. 1029 , Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment, by Harry L. Runyan [No. 1089], p. 615 , Some features of artificially thickened fully developed turbulent boundary layers with zero pressure gradient, by P.S. Klebanoff and Z.W. Diehl [No. 1110], p. 1165 , Sound from a two-blade propeller at supersonic tip speeds, by Harvey H, Hubbard and Leslie W. Lassiter [No. 1079], p. 457 , Stresses in a two-bay noncircular cylinder under transverse loads, by George E. Griffith [No. 1097], p. 811 , Summary of methods for calculating dynamic lateral stability and response and for estimating lateral stability derivatives, by John P. Campbell and Marion O. McKinney [No. 1098], p. 823 , Table of contents, p. II , The Langley annular transonic tunnel, by Louis W. Habel, James H. Henderson, and Mason F. Miller [No. 1106], p. 1069 , The linearized charateristics method and its application to practical nonlinear supersonic problems, by Antonio Ferri [No. 1102], p. 933 , Theoretical damping in roll and rolling moment due to differential wing incidence for slender cruciform wings and wing-body combinations, by Gaynor J. Adams and Duane W. Dugan [No. 1088], p. 603 , Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan forum at subsonic speeds, by John DeYoung [No. 1071], p. 245 , Transonic flow past a wedge profile with detached bow wave, by Walter G. Vincenti and Cleo B. Wagoner [No. 1095], p. 759 , Two- and three-dimensional unsteady lift problems in high-speed flight, by Harvard Lomax, Max A. Heaslet, Franklin B. Fuller and Loma Sluder [No. 1077], p. 393 , p. 715 , © 2008 by NewsBank, Inc. All rights reserved
    Language: English
    URL: Volltext  (Deutschlandweit zugänglich)
    Library Location Call Number Volume/Issue/Year Availability
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