21–40 of 76 hits
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    A stagnation point streamtube model for power law bodies

    O'Brien, Timothy / Lewis, Mark | AIAA | 1998

    Comparison of HTHL and VTHL Airbreathing and Rocket Systems for Access to Space

    Dissel, A. / Kothari, Ajay / Raghavan, V. et al. | AIAA | 2004

    Comparison of Turbine-Based Combined-Cycle Engine Flowpaths

    Clough, Joshua / Lewis, Mark | AIAA | 2003

    Component Matching for the Air Turborocket

    Clough, Joshua / Lewis, Mark | AIAA | 2004

    Configurational Analysis of the SHARP-L1 Reentry Vehicle

    Starkey, Ryan / Reuster, James / Lewis, Mark et al. | AIAA | 2003

    Corrected Shock-Based Design for Waverider Geometries

    Chauffour, Marie-Laure / Lewis, Mark | AIAA | 2003

    Corrected Waverider Design for Inlet Applications

    Chauffour, Marie-Laure / Lewis, Mark | AIAA | 2004

    DSMC of Power-Law Leading Edge Ionization for Hypersonic Telemetry Applications

    Hoult, Daniel / Starkey, Ryan / Lewis, Mark | AIAA | 2003

    Extending the Flight Mach Number of the SR-71 Inlet

    Colville, Jesse / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Horizontal Launch Vehicle Weight Modeling for Future Lunar Exploration-Class Payloads

    Scott, Christopher / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Hypersonic aerodynamics test facility using the external propulsion accelerator

    Rom, Joseph / Lewis, Mark / Gupta, Ashwani et al. | AIAA | 1995

    Hypersonic Airplane Space Tether Orbital Launch (HASTOL) system - Interim study results

    Bogar, Thomas / Bangham, Michal / Forward, Robert et al. | AIAA | 1999

    Hypersonic missile requirements and operational tradeoff studies

    Stuckey, Richard / Lewis, Mark | AIAA | 1999