Nonlinear unsteady aerodynamic loads on rectangular and delta wings in an incompressible flow are calculated by using an unsteady vortex-lattice model. Examples include flows past fixed wings in unsteady uniform streams and flows past wings undergoing unsteady motions. The unsteadiness may be due to gusty winds or pitching oscillations. The present technique establishes a reliable approach which can be utilized in the analysis of problems associated with the dynamics and aeroelasticity of wings within a wide range of angles of attack.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Nonlinear, unsteady aerodynamic loads on rectangular and delta wings


    Beteiligte:
    Atta, E. H. (Autor:in) / Kandil, O. A. (Autor:in) / Mook, D. T. (Autor:in) / Nayfeh, A. H. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1977 ; Los Angeles, CA


    Erscheinungsdatum :

    1977-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Nonlinear, unsteady aerodynamic loads on rectangular and delta wings

    ATTA, E. / KANDIL, O. / MOOK, D. et al. | AIAA | 1977


    Unsteady Aerodynamic Effects of Trailing Edge Controls on Delta Wings

    Pilkington, D. J. / Wood, N. J. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1994




    Unsteady Aerodynamic Effects of Trailing Edge Controls on Delta Wings

    Pilkington, D. J. / Wood, N. J. | British Library Online Contents | 1994