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person:(Lewis, Mark)

    Extending the Flight Mach Number of the SR-71 Inlet

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

    Numerical Simulations of Busemann Hypersonic Inlets At Finite Flight Angles

    Ramasubramanian, Vijay / Starkey, Ryan / Lewis, Mark | AIAA | 2008

    Investigation of Two-Stage-to-Orbit Air-Breathing Launch Vehicle Configurations

    Dissel, Adam / Kothari, Ajay / Lewis, Mark | AIAA | 2005

    An analytical solution of the type IV shock interaction

    Frame, Michael / Lewis, Mark | AIAA | 1996

    A stagnation point streamtube model for power law bodies

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

    Weight Growth Study of Reusable Launch Vehicle Systems

    Dissel, Adam / Kothari, Ajay / Lewis, Mark | AIAA | 2005

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

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

    Optimization of heat transfer in a high energy booster rocket

    Tarpley, Christopher / Lewis, Mark | AIAA | 1992