Analytical method, which can be used for performance, stress, and vibration studies of helicopters and VTOL aircraft; applications are given for helicopter in flight regime from 80 to 160 knots; sample problem is carried out at 150 knots; rapidly convergent iterative procedure, which takes into account blade stall, is used to put rotor in trim; blade elemental lifts and drags are computed using wind tunnel airfoil data; rotor blade dynamics are determined using set of complex equations based upon extension of N.O.Myklestad's analysis for rotating beams.


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    Titel :

    Analysis of helicopter aeroelastic characteristics in high-speed flight


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Gerstenberger, W. (Autor:in) / Wood, E.R. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 10


    Erscheinungsdatum :

    1963


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    White, Jr., R.P. / Trenka, A.R. | Engineering Index Backfile | 1962



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