1–9 von 9 Ergebnissen
|

    Approximate Method for Computing Convective Heating on Hypersonic Vehicles Using Unstructured Grids

    Hamilton, H. H. / Weilmuenster, K. J. / DeJarnette, F. R. | AIAA | 2014

    Switched Dynamical Systems for Reduced-Order Flow Modeling

    Hamilton, Howard H. / Kurdila, Andrew J. / Jammulamadaka, Anand K. | AIAA | 2008

    Flight stagnation-point heating calculations on Aeroassist Flight Experiment vehicle

    HAMILTON, H. H. / GUPTA, ROOP N. / JONES, JIM J. | AIAA | 1991

    Comparison of heating calculations with experimental data on a modified Shuttle Orbiter

    HAMILTON, H. H. / GREENE, FRANCIS A. / WEILMUENSTER, K. J. | AIAA | 1992

    Hypersonic aerodynamic characteristics of a proposed single-stage-to-orbit vehicle

    Weilmuenster, K. J. / Gnoffo, P. A. / Greene, F. A. et al. | AIAA | 1996

    X-33 Hypersonic Boundary-Layer Transition

    Scott A. Berry / Thomas J. Horvath / Brian R. Hollis et al. | AIAA | 2001

    Hypersonic Thermal Environment of a Proposed Single-Stage-to-Orbit Vehicle

    K. James Weilmuenster / P. A. Gnoffo / F. A. Greene et al. | AIAA | 1997

    X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data

    Brian R. Hollis / Thomas J. Horvath / Scott A. Berry et al. | AIAA | 2001

    X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography

    Thomas J. Horvath / Scott A. Berry / Brian R. Hollis et al. | AIAA | 2001