Paper derives generalized aerodynamic forces for aircraft on basis of slender body theory; configurations are considered which are spanwise flexible; slender wing-body problem is reduced to simple body and modified slender wing problem; integral solution of latter is obtained, using circle theorem and solution of airfoil equation for double interval; conformal mapping techniques are not necessary and solution obtained is valid for arbitrary spanwise downwash distributions; aerodynamic forces are derived for spanwise flexible wing-body configurations.


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    Titel :

    Unsteady aerodynamic forces on slender supersonic aircraft with flexible wings and bodies


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Yates, J.E. (Autor:in) / Zeydel, E.F.E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 2


    Erscheinungsdatum :

    1963


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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