Problems of Transient lift on two- and three-dimensional wings flying at high speeds discussed as boundary value problem for classical wave equation; Kirchhoff's formula is applied so that analysis is reduced, just as in steady state, to investigation of sources and doublets. Supersedes NACA -- Tech Notes 2403 and 2387.


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    Title :

    Two- and three-dimensional unsteady lift problems in high-speed flight


    Additional title:

    NACA -- Report


    Contributors:
    Lomax, H. (author) / Heaslet, M.A. (author) / Fuller, F.B. (author) / Sluder, L. (author)


    Publication date :

    1952


    Size :

    55 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Three-dimensional, unsteady-lift problems in high-speed flight -- Basic concepts

    Lomax, H. / Heaslet, M.A. / Fuller, F.B. | Engineering Index Backfile | 1950



    Three-dimensional unsteady lift problems in high-speed flight -- Triangular wing

    Lomax, H. / Heaslet, M.A. / Fuller, F.B. | Engineering Index Backfile | 1951


    Three-dimensional, unsteady-lift problems in high-speed flight - basic concepts

    Lomax, Harvard / Heaslet, Max A. / Fuller, Franklyn B. | TIBKAT | 1950


    Three-dimensional, unsteady-lift problems in high-speed flight : basic concepts

    Lomax, Harvard / Heaslet, Max A / Fuller, Franklyn B | NTRS | 1950