By combined use of A. BUSEMANN second order approximation theory for pressure distribution over two-dimensional airfoil with straight leading edge and theory for loss in lift at tips of rectangular airfoil in supersonic flow, expressions for lift, drag, and moment coefficients and center of pressure are derived for rectangular type of wing. (See also - discussion n 6, 7, June p 335-6, July p 409-10, 432)


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    Title :

    Aerodynamic characteristics of rectangular wings at supersonic speeds


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1947


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Aerodynamic Characteristics of Wings at Supersonic Speeds

    R. M. Snow / E. A. Bonney | NTIS | 1947



    Aerodynamic performance of Delta wings at supersonic speeds

    Puckett, A.E. / Stewart, H.J. | Engineering Index Backfile | 1948


    Aerodynamic performance of Delta wings at supersonic speeds

    Puckett, A.E. / Stewart, H.J. | Engineering Index Backfile | 1948


    Aerodynamic performance of Delta wings at supersonic speeds

    Puckett, A.E. / Stewart, H.J. | Engineering Index Backfile | 1947