1–8 von 8 Ergebnissen
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    Development of the wake of an airfoil with riblets

    Caram, J. M. / Ahmed, A. | NTRS | 1992

    Comparison of Space Shuttle Orbiter Wing Leading Edge Heating Rate Calculations with Experimental and Flight Data

    Wang, K. C. / Caram, J. M. / AIAA | British Library Conference Proceedings | 1994

    Comparison of Space Shuttle Orbiter Wing Leading Edge Heating Rate Calculations with Experimental and Flight Data

    Wang, K. C. / Caram, J. M. / AIAA | British Library Conference Proceedings | 1994

    Development of the wake of an airfoil with riblets

    CARAM, J. M. / NASA, Johnson Space Center / Houston, AHMED et al. | AIAA | 1992

    Isolated Roughness Induced Boundary-Layer Transition: Shuttle Orbiter Ground Tests and Flight Experience

    Bouslog, S. A. / Bertin, J. J. / Berry, S. A. et al. | British Library Conference Proceedings | 1997

    Boundary Layer Transition Due to Isolated Roughess: Shuttle Results from the LaRC 20-Inch Mach 6 Tunnel

    Berry, S. A. / Bouslog, S. A. / Brauckmann, G. J. et al. | British Library Conference Proceedings | 1997

    Aerothermodynamic Environment Definition For an X-23/X-24A Derived Assured Crew Return Vehicle

    Campbell, C. H. / Caram, J. M. / Li, C. P. et al. | British Library Conference Proceedings | 1996