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    Comparison of Turbine-Based Combined-Cycle Engine Flowpaths

    Clough, Joshua / Lewis, Mark | AIAA | 2003

    Aerodynamic Stability of Reentry Heat Shield Shapes for a Crew Exploration Vehicle

    Joshua Johnson / Ryan Starkey / Mark Lewis | AIAA | 2006

    Axisymmetric Inlet Design for Combined-Cycle Engines

    Jesse Colville / Ryan Starkey / Mark Lewis | AIAA | 2006

    Investigation of Two-Stage-to-Orbit Airbreathing Launch-Vehicle Configurations

    Adam Dissel / Ajay Kothari / Mark Lewis | AIAA | 2006

    Performance of Various Truncation Strategies Employed on Hypersonic Busemann Inlets

    Ramasubramanian, Vijay / Lewis, Mark / Starkey, Ryan | AIAA | 2009

    Navier-Stokes computations of a viscous optimized waverider

    TAKASHIMA, NARUHISA / LEWIS, MARK | AIAA | 1992

    Corrected Waverider Design for Inlet Applications

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

    Coupled Entry Heat Shield/Trajectory Optimization for Lunar Return

    Johnson, Joshua / Lewis, Mark / Starkey, Ryan | AIAA | 2008

    Entry Heat Shield Optimization for Mars Return

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

    Inverse Design of Hypersonic Star Inlets

    Colville, Jesse / Lewis, Mark | AIAA | 2003

    Velocity Profile Modification in High-Speed Flows

    Barkmeyer, Daniel / Lewis, Mark | AIAA | 2003

    Comparison of Optimal Entry Heat Shield Configurations for Lunar and Mars Return

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

    A re-evaluation of the waverider design process

    BURNETT, DAVID / LEWIS, MARK | AIAA | 1993

    Component Matching for the Air Turborocket

    Clough, Joshua / Lewis, Mark | AIAA | 2004

    Analysis of Optimal Earth Entry Heat Shield/Trajectory Configurations

    Johnson, Joshua / Lewis, Mark / Starkey, Ryan | AIAA | 2008

    Computational Fluid Dynamic Solutions of Optimized Heat Shield Designs for Earth Entry

    Meeroff, Jamie / Lewis, Mark / Starkey, Ryan | AIAA | 2009