A summary of the work performed under NASA grant is presented. More details can be found in the cited references. This grant led to the development of relatively faster aeroelastic analysis methods for predicting flutter and forced response in fans, compressors, and turbines using computational fluid dynamic (CFD) methods. These methods are based on linearized two- and three-dimensional, unsteady, nonlinear aerodynamic equations. During the period of the grant, aeroelastic analysis that includes the effects of uncertainties in the design variables has also been developed.


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    Titel :

    Aeroelastic Stability and Response of Rotating Structures


    Beteiligte:

    Erscheinungsdatum :

    01.01.2004


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aeroelastic Stability & Response of Rotating Structures

    Keith, Theo G., Jr. / Reddy, T. S. R. | NTRS | 2001


    Aeroelastic Stability and Response of Rotating Structures

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


    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