The application and assessment of the recently developed CAP-TSD transonic small-disturbance code for flutter prediction is described. The CAP-TSD code has been developed for aeroelastic analysis of complete aircraft configurations and was previously applied to the calculation of steady and unsteady pressures with favorable results. Generalized aerodynamic forces and flutter characteristics are calculated and compared with linear theory results and with experimental data for a 45 deg sweptback wing. These results are in good agreement with the experimental flutter data which is the first step toward validating CAP-TSD for general transonic aeroelastic applications. The paper presents these results and comparisons along with general remarks regarding modern wing flutter analysis by computational fluid dynamics methods.


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    Titel :

    Modern wing flutter analysis by computational fluid dynamics methods


    Beteiligte:

    Erscheinungsdatum :

    1988-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Modern wing flutter analysis by computational fluid dynamics methods

    Cunningham, Herbert J. / Batina, John T. / Bennett, Robert M. | NTRS | 1987


    Modern wing flutter analysis by computational fluid dynamics methods

    Cunningham, Herbert J. / Batina, John T. / Bennett, Robert M. | NTRS | 1988


    Modern wing flutter analysis by computational fluid dynamics methods

    Cunningham, H.J. / Batino, J.T. / Bennett, R.M. | Tema Archiv | 1987


    Modern wing flutter analysis by computational fluid dynamics methods

    CUNNINGHAM, HERBERT J. / BATINA, JOHN T. / BENNETT, ROBERT M. | AIAA | 1988


    Flutter Analysis of an Aircraft Wing Using Computational Fluid Dynamics

    Kumar Sinha, Anjani ;Ananda Kumar, Eriki ;Johnrajan, A. | Trans Tech Publications | 2015