1–20 von 28 Ergebnissen
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    A self-adaptive-grid method with application to airfoil flow

    NAKAHASHI, K. / DEIWERT, G. | AIAA | 1985

    A three-dimensional adaptive grid method

    NAKAHASHI, K. / DEIWERT, G. | AIAA | 1985

    Three-dimensional adaptive grid method

    NAKAHASHI, K. / DEIWERT, G. S. | AIAA | 1986

    Classification of Aerodynamic and Aerothermodynamics Issues and Problems

    Deiwert, G. S. | British Library Online Contents | 1996

    Importance of real gas effects in entry technology

    Deiwert, G. S. | British Library Online Contents | 1995

    Theoretical analysis of aircraft afterbody flow

    DEIWERT, G. / ANDREWS, A. / NAKAHASHI, K. | AIAA | 1984

    Three-dimensional adaptive grid method

    Nakahashi, K. / Deiwert, G. S. | NTRS | 1986

    Real-Gas Effects

    Deiwert, G. S. / Pandolfi, M. | British Library Online Contents | 1996

    Transonic flow about a thick circular-arc airfoil

    MCDEVITT, J. / LEVY, JR., L. / DEIWERT, G. | AIAA | 1975

    Hypersonic combustor model inlet CFD simulations and experimental comparisons

    Venkatapathy, E / Tokarcik-Polsky, S / Deiwert, G | AIAA | 1995