A summary of the work performed under NASA grant NCC3-605 is presented. More details can be found in the cited references. This grant led to the development of relatively faster aeroelastic analyses methods for predicting flutter and forced response in fans, compressors, and turbines using computational fluid dynamic (CFD) methods.


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    Titel :

    Aeroelastic Stability & Response of Rotating Structures


    Beteiligte:

    Erscheinungsdatum :

    01.03.2001


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aeroelastic Stability and Response of Rotating Structures

    Keith, Theo G., Jr. / Reddy, T. S. R. | NTRS | 1998


    Aeroelastic Stability and Response of Rotating Structures

    Keith, Theo G., Jr. / Reddy, Tondapu | NTRS | 2004


    Aeroelastic Stability of Rotating Blade

    Petkevicius, K. / Bekampis, E. / Kaunas University of Technology | British Library Conference Proceedings | 2012


    Aeroelastic Stability of Cylindrical Shells Subjected to a Rotating Flow

    E.H. DOWELL / A.V. SRINASAN / J.D. MCLEAN AND J. AMBROSE | AIAA | 1974