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Synonyme wurden verwendet für: Flugmechanik
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    Determination of the profile drag of an airplane wing in flight at high Reynolds numbers

    Bicknell, J. | NTRS | 1939
    Schlagwörter: Aerodynamics

    Notes on the effect of surface distortions on the drag and critical Mach number of airfoils

    Allen, J. | NTRS | 1943
    Schlagwörter: Aerodynamics

    Flight investigation of boundary-layer control by suction slots on an NACA 35-215 low-drag airfoil at high Reynolds numbers

    Zalovcik, J. A. / Wetmore, J. W. / Vondoenhoff, A. E. | NTRS | 1944
    Schlagwörter: Aerodynamics

    Profile-drag coefficients of conventional and low-drag airfoils as obtained in flight

    Zalovcik, J. A. | NTRS | 1944
    Schlagwörter: Aerodynamics

    Investigation of the behavior of parallel two-dimensional air jets

    Corrsin, Stanley | NTRS | 1944
    Schlagwörter: Aerodynamics

    Flight tests of the high-speed performance of a P-51B airplane (AAF no. 43-12105)

    Voglewede, T. J. / Danforth, E. C. D. | NTRS | 1944
    Schlagwörter: Aerodynamics

    NACA Conference on Aerodynamics of High- speed Aircraft A compilation of the papers presented

    NTRS | 1953
    Schlagwörter: Aerodynamics , AERODYNAMICS

    A flight investigation of the practical problems associated with porous-leading-edge suction

    Hunter, P. A. / Johnson, H. I. | NTRS | 1954
    Schlagwörter: Aerodynamics

    A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers

    Garrick, I. E. / Watkins, C. E. | NTRS | 1954
    Schlagwörter: Aerodynamics

    PUBLIC OPINION AND SOCIAL EFFECTS OF SPACE ACTIVITY

    Goldsen, J. M. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Lift, Drag, and Pitching Moments of an Arrow Wing Having 80 Degree of Sweepback at Mach Numbers from 2.48 to 3.51 and Reynolds Numbers up to 11.0 Million

    Hopkins, Edward J. / Jillie, Don W. / Levin, Alan D. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Stability and control characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with outboard wing panels swept back 75 deg

    Foster, G. V. / Spearman, M. L. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Effects of three spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45 deg sweptback highly tapered wing at transonic speeds

    Mugler, J. P., Jr. | NTRS | 1959
    Schlagwörter: Aerodynamics

    The Wind-induced Loads on a Dynamically Scaled Model of a Large Missile in Launching Position

    Buell, D. A. / Kenyon, G. C. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing

    Keener, E. R. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86

    Driver, C. | NTRS | 1959
    Schlagwörter: Aerodynamics

    A wind-tunnel investigation of the carry loads and mutual interference effects of 1/40-scale models of the x-15 and b-52 airplanes in com- bination

    Alford, W. J., Jr. / Taylor, R. T. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Full-scale wind-tunnel investigation of the low-speed static aerodynamic characteristics of a model of a reentry capsule

    Scallion, W. I. | NTRS | 1959
    Schlagwörter: Aerodynamics

    Transonic and supersonic ejection release characteristics of six dynamically scaled external-store shapes from an 0.086-scale model of a current fighter airplane

    Hinson, W. F. | NTRS | 1959
    Schlagwörter: Aerodynamics

    An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics

    Doggett, R. V., Jr. / Morgan, H. G. / Rainey, A. G. | NTRS | 1959
    Schlagwörter: Aerodynamics

    An exploratory investigation of the low-speed aerodynamic characteristics of variable-wing- sweep airplane configurations

    Alford, W. J., Jr. / Henderson, W. P. | NTRS | 1959
    Schlagwörter: Aerodynamics

    EFFECTS OF WING VERTICAL LOCATION ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING

    Foster, G. V. | NTRS | 1959
    Schlagwörter: AERODYNAMICS

    Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing-sweep Airplane Configuration

    Alford, W. J., Jr. / Henderson, W. P. / Luoma, A. A. | NTRS | 1959
    Schlagwörter: Aerodynamics

    ECONOMY OF SPACE FLIGHT

    Huber, W. G. / Koelle, H. H. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Preliminary Full-Scale Power-Off Drag of the X-15 Airplane for Mach Numbers from 0.7 to 3.1

    Saltzman, Edwin J. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Transonic Aerodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane Designed for Supersonic Flight

    Wornom, Dewey E. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Free-spinning-tunnel Investigation of a 1/30 Scale Model of a Twin-jet-swept-wing Fighter Airplane

    Bowman, James S., Jr. / Healy, Frederick M. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Aerodynamic Characteristics at Mach Number 2.05 of a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber

    Carlson, Harry W. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Talk given at huntsville, alabama during engineers week

    Mitchell, E. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Force, moment, and flow-field characteristics of two wing-body-nacelle combinations at mach numbers 2 and 3

    Hill, W. A., Jr. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Effects of wing incidence on the longitudinal trim characteristics of a cambered 70 deg delta-wing configuration at mach numbers 3.0 to 5.0

    Ahtye, W. F. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Theoretical and Experimental Studies of Cambered and Twisted Wings Optimized for Flight at Supersonic Speeds

    Brown, C. E. / Klunker, E. B. / Mc Lean, F. E. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-sweep Wings

    Foster, G. V. / Morris, O. A. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Aerodynamic characteristics in pitch, including effects of horizontal-tail negative dihedral angle, of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds

    Olstad, W. B. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 deg delta wing

    Driver, C. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Measurements of the Mach number and pressure on the afterbody of a blunt-nosed model in free flight at Mach numbers from 6.5 to 14

    Sommer, S. C. | NTRS | 1960
    Schlagwörter: Aerodynamics

    A Wind-tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 at Angles of Attack to 90 Deg

    Smith, F. M. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Transonic aerodynamic characteristics of a variable-sweep airplane configuration having a 12-percent-thick wing and an inboard pivot location

    Bielat, R. P. / Pierpont, P. K. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Investigation of aerodynamic characteristics at high subsonic speeds of two supersonic- cruise airplane configurations having tail surfaces outboard of the wing tips

    Fournier, P. G. / Sleeman, W. C., Jr. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 deg

    Foster, G. V. / Morris, O. A. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Effects of boundary-layer suction and spoilers on transonic flutter derivatives for a midspan control surface on an upswept wing

    Dannenberg, R. E. / Gambucci, B. J. / Sorenson, R. M. et al. | NTRS | 1960
    Schlagwörter: Aerodynamics

    The effects of wing-tip droop on the aerodynamic characteristics of a delta-wing aircraft at supersonic speeds

    Petersen, R. H. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds

    Olstad, W. B. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5

    Bright, L. G. / Peterson, V. L. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep

    Alford, W. J., Jr. / Luoma, A. A. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Pressure Distribution of a 0.0667-Scale Model of the X-15 Airplane for an Angle-Of-Attack Range of 0 deg To 28 deg at Mach Numbers of 2.30, 2.88, and 4.65

    Burbank, P. B. / Hodge, B. L. | NTRS | 1960
    Schlagwörter: AERODYNAMICS

    Wind-tunnel investigation at high subsonic speeds to determine stability and control characteristics of antitank missiles with ram-pressure jet controls on a ring tail

    Vogler, R. D. | NTRS | 1960
    Schlagwörter: Aerodynamics

    Theoretical Stability Derivatives for the X-15 Research Airplane at Supersonic and Hypersonic Speeds Including a Comparison with Wind-tunnel Results

    Walker, H. J. / Wolowicz, C. H. | NTRS | 1960
    Schlagwörter: Aerodynamics

    A Simplified Method for Estimating Subsonic Lift-Curve Slope at Low Angles of Attack for Irregular Planform Wings

    Spencer, Bernard, Jr. | NTRS | 1961
    Schlagwörter: Aerodynamics

    An Investigation of the Influence of Body Size and Indentation Asymmetry of the Effectiveness of Body Indentation in Combination with a Cambered Wing

    Patterson, James C., Jr. / Loving, Donald L. | NTRS | 1961
    Schlagwörter: Aerodynamics

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