41–60 of 123 hits
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    Comparison of Optimal Entry Heat Shield Configurations for Lunar and Mars Return

    Johnson, Joshua / Lewis, Mark / Starkey, Ryan | AIAA | 2009

    Unsteady effects of a hypersonic type IV shock interaction

    Lind, Charles / Lewis, Mark | AIAA | 1994

    Comparison of Robust Optimization Methods Applied to Hypersonic Vehicle Design

    Ryan, Kevin M. / Lewis, Mark / Yu, Kenneth H. | AIAA | 2013

    A Design Comparison of Atmospheric Flight Vehicles for the Exploration of Titan

    Gasbarre, Joseph / Wright, Henry / Lewis, Mark | AIAA | 2005

    The Three Weak Solution Regimes of Supersonic Conical Flow and Their Impact on Engine Inlets

    Smith, Nathanial / Ramasubramanian, Vijay / Lewis, Mark | AIAA | 2010

    Corrected Shock-Based Design for Waverider Geometries

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

    Optimized mission-oriented waverider vehicles with base closure

    Takashima, Naruhisa / Lewis, Mark | AIAA | 1996

    Inverse Waverider Design for Inward Turning Inlets

    Barkmeyer, Daniel / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Extending the Flight Mach Number of the SR-71 Inlet

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