1–9 von 9 Ergebnissen
|

    Boundary layer transition due to isolated roughness - Shuttle results from the LaRC 20-inch Mach 6 tunnel

    Berry, Scott / Bouslog, Stanley / Brauckmann, Gregory et al. | AIAA | 1997

    Emittance measurements of Space Shuttle Orbiter Reinforced Carbon-Carbon

    CARAM, JOSE / BOUSLOG, STANLEY / CUNNINGTON, JR., GEORGE | AIAA | 1993

    Aerothermodynamic environment definition for an X-23/X-24A derived assured crew return vehicle

    Campbell, Charles / Caram, Jose / Li, Chien et al. | AIAA | 1996

    Effect of isolated roughness elements on boundary-layer transition for Shuttle Orbiter

    Bertin, John / Stetson, Kenneth / Bouslog, Stanley et al. | AIAA | 1996

    An overview of X-38 Hypersonic Wind Tunnel data and comparison with numerical results

    Campbell, Charles / Caram, Jose / Berry, Scott et al. | AIAA | 1997