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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Formulation of the Three Dimensional Transonic Unsteady Aerodynamic Problem


    Contributors:

    Publication date :

    1979


    Size :

    87 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    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