Use of thin, all movable control surfaces on aircraft and missiles indicates that divergence rather than flutter may be primary aeroelastic problem; chordwise divergence is treated with emphasis on slender delta wings; experimental and analytical results for wings having apex half-angles of 5, 10, 15 and 20°, including calculations based on small-aspect ratio theory, lifting surface theory, and strip theory.


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    Titel :

    Some divergence characteristics of low aspects ratio wings at transonic and supersonic speeds


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Woolston, D.S. (Autor:in) / Gibson, F.W. (Autor:in) / Cunningham, H.J. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :