This report summarizesthe theoretical and experimental investigations that were conducted to evaluate the potential of aeroelastic and mass-elastic couplings in an aeroelastic conformable rotor (ACR) that will improve the performance and vibratory charactersitics of helicopter rotor systems without creating instabilities. ACR parameters were identified and a baseline rotor system was selected. An ACR blade concept was investigated by altering the characteristics of the base-line and using automated analysis techniques. (DePo)


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    Titel :

    Wind-tunnel evaluation of an aeroelastically conformable rotor


    Weitere Titelangaben:

    Windkanalpruefung eines aeroelastischen Hubschrauberrotors


    Beteiligte:
    Sutton, L.W. (Autor:in) / White, R.P. jun. (Autor:in) / Marker, R.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1982


    Format / Umfang :

    87 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch




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