1–20 von 60 Ergebnissen
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    Analysis of a dual-mode scramjet combustor

    Abdel-Salam, T. / Tiwari, S. / Mohieldin, T. | AIAA | 2001

    A numerical study of hypervelocity flows through a scramjet combustor

    Krishnamurthy, R. / Rogers, R. / Tiwari, S. | AIAA | 1994

    CFD-based optimization of low Reynolds number rocket nozzles

    Shebalin, J.-P. / Tiwari, S. | AIAA | 1999

    Combustion of ethylene and propane in scramjet engines - Numerical study

    Taha, A. / Tiwari, S. / Mohieldin, T. | AIAA | 2001

    Dual-mode flowfield in scramjet combustor

    Abdel-Salam, T. / Tiwari, S. / Mohieldin, T. | AIAA | 2001

    Effects of ramp swept angle in supersonic mixing

    Abdel-Salam, T. / Tiwari, S. / Mohieldin, T. | AIAA | 2000

    Effects of scaling on numerical modeling of a transverse jet into supersonic cross flows

    Olynciw, M. / Mohieldin, T. / McClinton, C. et al. | AIAA | 1999

    Error analysis of the SAGE II water vapor data

    Larsen, J. / Tiwari, S. / Chu, W. | AIAA | 1997