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    Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

    Becker, John V | NTRS | 1940
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012 , AIRFOILS - NACA 0012 - CHARACTERISTICS , AIRFOILS - NACA 23012 - CHARACTERISTICS , PRESSURE DISTRIBUTION - AIRFOILS - NACA 23012 , SKIN FRICTION - AIRFOILS

    Flow of a compressible fluid past a symmetrical airfoil in a wind tunnel and in free air

    Emmons, Howard W | NTRS | 1948
    Schlagwörter: FLOW - AIRFOILS, SYMMETRICAL , AIRFOILS - NACA 0012 - ORDINATES , PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012

    Chordwise and spanwise loadings measured at low speed on a triangular wing having an aspect ratio of two and an NACA 0012 airfoil section

    Wick, Bradford H | NTRS | 1948
    Schlagwörter: LOAD DISTRIBUTION, WING-SPAN , AIRFOILS - NACA 0012 - CHARACTERISTICS , AIRFOILS - ASPECT RATIO, SMALL , CENTER OF PRESSURE - WINGS, DELTA , PRESSURE DISTRIBUTION - WINGS, DELTA

    Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall

    Daley, Bernard N / Hanna, Lillian E | NTRS | 1949
    Schlagwörter: PRESSURE DISTRIBUTION - AIRFOILS - NACA 0012 , AIRFOILS - NACA 66,2-215 - LOW-DRAG , WIND TUNNEL WALL INTERFERENCE - AIRFOILS , PHOTOGRAPHY - AIR FLOW - AIRFOILS - SCHLIEREN METHOD , AIR FLOW - AIRFOILS - 2-DIMENSIONAL , AIRFOILS - NACA 66,2-015 - LOW-DRAG

    Report on the special field "Interference" to the wind-tunnel committee in February 1945

    Schlichting, Hermann / Moller, Egon | NTRS | 1953
    Schlagwörter: PRESSURE DISTRIBUTION - FUSELAGE-WING COMBINATIONS , AIRFOILS - NACA 0012-0 825-40 , AIRFOILS - NACA 0010-0 825-40 , AIRFOILS - NACA 23012 , AIRFOILS - NACA 0015

    Experimental Investigation of the Perpendicular Vortex-Airfoil Interaction of Transonic Speeds

    D. R. Wilson / I. M. Kalkhoran / D. D. Seath | NTIS | 1987
    Schlagwörter: Airfoils , Pressure distribution , NACA-0012 airfoils