Development and application of method of analysis for calculating response of flexible wing in airstream to oscillating disturbing force and treating such aeroelastic instabilities as flutter and divergence; aerodynamic coefficients derived on basis of lifting surface theory for subsonic compressible flow using method given in N ASA Tech Report R-48, indexed in Engineering Index 1959 p 25.


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    Titel :

    Use of subsonic kernal function in influence-coefficient method of aeroelastic analysis and some comparisons with experiment


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Sewall, J.L. (Autor:in) / Herr, R.W. (Autor:in) / Watkins, C.E. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    86 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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