Unsteady transonic flow for a swept wing of moderate sweep is formulated in the small disturbance limit. Boundary conditions at the wing, the trailing vortex sheet, and the outer computatinal boundaries are given including the ventilated wall conditions. Shortcomings of the small disturbance hypothesis is reviewed, suggesting means to compensate for them. Viscous interactions are described together with procedures to incorporate their effects. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Formulation of the Three Dimensional Transonic Unsteady Aerodynamic Problem


    Beteiligte:
    H. Yoshihara (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    87 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Experience with Transonic Unsteady Aerodynamic Calculations

    J. W. Edwards / S. R. Bland / D. A. Seidel | NTIS | 1984


    Experience with transonic unsteady aerodynamic calculations

    Edwards, J. W. / Bland, S. R. / Seidel, D. A. | NTRS | 1984


    Experience with transonic unsteady aerodynamic calculations

    Edwards, J. W. / Bland, S. R. / Seidel, D. A. | NTRS | 1985


    Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows

    Kenneth C. Hall / Jeffrey P. Thomas / Earl H. Dowell | AIAA | 2000