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person:(Lewis, Mark)

    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

    Alternative to Nitric Acid Passivation

    Lewis, Pattie L. / Kolody, Mark / Curran, Jerry | NTRS | 2013

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

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

    Lagrangian Coherent Structures & Their Role in Jet Noise Generation

    Gonzalez, David R. / Gaitonde, Datta V. / Lewis, Mark J. | AIAA | 2017

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

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

    Navier-Stokes computation of a viscous optimized waverider

    Takashima, Naruhisa / Lewis, Mark J. | AIAA | 1994

    Corrected Shock-Based Design for Waverider Geometries

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

    Inverse Waverider Design for Inward Turning Inlets

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

    Optimized mission-oriented waverider vehicles with base closure

    Takashima, Naruhisa / Lewis, Mark | AIAA | 1996

    Bow shock matching with viscous effects on hypersonic forebodies

    LEWIS, MARK / HASTINGS, DANIELE. | AIAA | 1989