Dietze's method for solution of Possio's integral equation used to determine chordwise distribution of lift on oscillating airfoil with simple hinged flap in two-dimensional compressible flow (subsonic); results of these calculations used to prepare tables of aerodynamic coefficients for lift, pitching moment and flap hinge moment for Mach number of 0.7.


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    Title :

    Aerodynamic coefficients for oscillating airfoil with hinged flap, with tables for Mach number of 0.7


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    46 pages


    Remarks:

    Tables, Graphs


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :