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    Nomogram for correcting drag and angle of attack of an airfoil model in an air stream of finite diameter

    NTRS | 1924
    Schlagwörter: AIRFOILS - ANGLE OF ATTACK - WIND TUNNEL CORRECTION

    Air forces and air-force moments at large angles of attack and how they are affected by the shape of the wing

    Fuchs, Richard / Schmidt, Wilhelm | NTRS | 1930
    Schlagwörter: ANGLE OF ATTACK, LARGE WINGS - DESIGN

    The Effect of Split Trailing-edge Wing Flaps on the Aerodynamic Characteristics of a Parasol Monoplane

    Wallace, Rudolf, N | NTRS | 1933
    Schlagwörter: GLIDING ANGLE - MONOPLANES - EFFECT OF SPLIT WING FLAPS , MONOPLANES, PARASOL - EFFECT OF WING FLAPS , WINGS, HIGH LIFT , TAKE-OFF & LANDING - EFFECT OF WING FLAPS

    Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube

    Humphreys, Milton D | NTRS | 1945
    Schlagwörter: PRESSURE-EFFECT OF COMPRESSIBILITY & ANGLE OF YAW , WIND TUNNEL TESTS-NACA-HIGH-SPEED (18 INCHES X 4 INCHES)

    Systematic Wind-Tunnel Measurements on Missiles

    O. Walchner | NTIS | 1947
    Schlagwörter: Angle of attack

    Application of Lifting-Surface Theory to the Prediction of Angle-of- Attack Hinge-Moment Parameters for Aspect Ratio 4.5 Wings

    A. L. Jones / M. G. Flanagan / L. Sluder | NTIS | 1947
    Schlagwörter: Angle of attack

    Effect of Compressibility on the Distribution of Pressures over a Tapered Wing of NACA 230-series Airfoil Sections

    Pearson, E O , Jr | NTRS | 1947
    Schlagwörter: EFFECT OF COMPRESSIBILITY , WIND TUNNEL TESTS - NACA - HIGH-SPEED (16') , AIRFOILS - ANGLE OF ATTACK , PRESSURE DISTRIBUTION - WINGS, TAPERED-EFFECT OF COMPRESSIBILITY

    An Application of Lifting-surface Theory to the Prediction of Angle-of-attack Hinge-moment Parameters for Aspect Ratio 4.5 Wings

    Jones, Arthur L / Flanagan, Mildred G / Sluder, Loma | NTRS | 1947
    Schlagwörter: AIRFOILS - ANGLE OF ATTACK

    Two-dimensional unsteady lift problems in supersonic flight

    Heaslet, Max A / Lomax, Harvard | NTRS | 1948
    Schlagwörter: AIRFOILS - ANGLE OF ATTACK , AIR FLOW VELOCITY, HIGH - SUPERSONIC

    Stability Derivatives of Triangular Wings at Supersonic Speeds

    H. S. Ribner / F. S. Malvesstuto | NTIS | 1948
    Schlagwörter: Angle of attack