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    2019 IRTD Final Report Summary

    Wright, Maria C. / Montgomery, Eliza L. / Manuel, Michele V. et al. | NTRS | 2019

    Accuracy of Recorded Driver Inputs in Toyota Part 563 EDR

    Hare, Barry / Webster, Greg / Clyde, Harold et al. | SAE Technical Papers | 2014

    A Comparison Between CFD Predictions and Measurements of Inlet Port Discharge Coefficient and Flow Characteristics

    Tang, Allen / Tillock, Brad / Rubenstein, Brandon et al. | SAE Technical Papers | 1999

    Adapting Temperature-Sensitive Paint Technology for Use in AEDC Hypervelocity Wind Tunnel 9

    Norris, Joseph / Hamner, Marvine / Lafferty, John et al. | AIAA | 2004

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

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

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

    Gasbarre, Joseph F. / Wright, Henry S. / Lewis, Mark J. | NTRS | 2005

    Aerodynamic Heating Performance of Power Law Leading Edges in Rarefied Hypersonic Flow

    Santos, Wilson / Lewis, Mark | AIAA | 2003

    Aerodynamics for Optimal Engine-Integrated Airbreathing Launcher Configurations

    Lewis, Mark / Boyd, I. / Cockrell, Charles | AIAA | 2004

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

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

    Aerodynamic testing for HSCT - A shock tube design study

    Lewis, Mark | AIAA | 1996

    Aerogravity Assist Maneuvers: Coupled Trajectory and Vehicle Shape Optimization

    Roberto Armellin / Michele Lavagna / Ryan Starkey et al. | AIAA | 2007

    Aero-Gravity Assist Maneuvers: Coupled Trajectory and Vehicle Shape Optimization

    Armellin, Roberto / Lavagna, Michele / Starkey, Ryan P. et al. | AIAA | 2006

    Aerothermodynamic Optimization of Reentry Heat Shield Shapes for a Crew Exploration Vehicle

    Joshua Johnson / Ryan Starkey / Mark Lewis | AIAA | 2007

    Aerothermodynamic Optimization of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle

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

    Aerothermodynamic Performance Analysis of Hypersonic Flow on Power Law Leading Edges

    Wilson F. Santos / Mark Lewis | AIAA | 2005

    Aerothermodynamics of a Parashield Re-Entry Vehicle

    Harry K. Magazu / Mark J. Lewis / David L. Akin | AIAA | 1998

    A Hypersonic Propulsion Airframe Integration Overview (Invited)

    Lewis, Mark | AIAA | 2003

    Air cleaning method and air cleaning array combined for improving anti-pollution effect

    Freier Zugriff
    WENGER STEPHAN / POLYZOIS CHRISTOPHER A / LEWIS MARK D | Europäisches Patentamt | 2022

    Aircraft passageway storage units

    Freier Zugriff
    CUDDY NATHANIAL C / MCINELLY CHRIS GREN / MAIR ROLAND et al. | Europäisches Patentamt | 2016

      AIRCRAFT PASSAGEWAY STORAGE UNITS

      Freier Zugriff
      CUDDY NATHANIAL C / MCINELLY CHRIS GREN / MAIR ROLAND et al. | Europäisches Patentamt | 2019

    AIRCRAFT PASSAGEWAY STORAGE UNITS

    Freier Zugriff
    CUDDY NATHANIEL C / MCINELLY CHRIS GREN / MAIR ROLAND et al. | Europäisches Patentamt | 2016

    Aircraft receptacle

    Freier Zugriff
    LEWIS BRIAN / WHITEMAN BRUCE M / ALLEY CHRISTOPHER MARK | Europäisches Patentamt | 2019

      Aircraft Receptacle

      Freier Zugriff
      LEWIS BRIAN / WHITEMAN BRUCE M / ALLEY CHRISTOPHER MARK | Europäisches Patentamt | 2016

    A joint American-Australian university hypersonic research program

    Lewis, Mark / Paull, Allan | AIAA | 1998

    Alternative to Nitric Acid Passivation

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

    An AJAX technology advanced SSTO design concept

    Chase, R. / Boyd, R. / Czysz, P. et al. | AIAA | 1998

    An AJAX Technology Advanced SSTO Design Concept

    Froning, H. D. / McKinney, L. E. / Lewis, Mark et al. | SAE Technical Papers | 1998

    Analysis of experimental results on a Mach 14 waverider with blunt leading edges

    Gillum, Michael / Lewis, Mark | AIAA | 1996

    Analysis of Highly Unsteady and Quasi-steady Shocks in Hypersonic Inlets Based on the Principle of Minimum Entropy Production

    Bussey, Gillian / Lewis, Mark | AIAA | 2012

    Analysis of Optimal Earth Entry Heat Shield/Trajectory Configurations

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

    Analysis of the Near-Field of an Asymmetrically Controlled Supersonic Round Jet

    Gonzalez, David R. / Gaitonde, Datta V. / Lewis, Mark J. | AIAA | 2015

    Analysis of the Near-Field of an Asymmetrically Controlled Supersonic Round Jet (AIAA 2015-1037)

    Gonzalez, David R. / Gaitonde, Datta V. / Lewis, Mark J. | British Library Conference Proceedings | 2015

    Analytical and computational study of unsteady shock motion on hypersonic forebodies

    LEWIS, MARK J. / SURLINE, YVETTE / ANDERSON, JOHN D. | AIAA | 1991

    Analytical modeling of jet unsteadiness in hypersonic type IV shock interactions

    Frame, Michael / Lewis, Mark | AIAA | 1998

    Analytical Model of Unsteady Shock Motion on Hypersonic Forebodies

    Sowmyalatha Jayaraman / Mark J. Lewis | AIAA | 1997

    Analytical off-design L/D analysis for hypersonic waveriders with planar shocks

    Starkey, Ryan / Lewis, Mark | AIAA | 1999

    Analytical Off-Design Lift-to-Drag-Ratio Analysis for Hypersonic Waveriders

    Ryan P. Starkey / Mark J. Lewis | AIAA | 2000

    Analytical Solution of the Type IV Shock Interaction

    Michael J. Frame / Mark J. Lewis | AIAA | 1997

    Analytical solutions of hypersonic type IV shock-shock interactions on noncircular bodies

    Frame, Michael / Lewis, Mark | AIAA | 1996

    An Euler Numerical Study of Busemann and Quasi-Busemann Hypersonic Inlets at On- and Off-Design Speeds

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

    Apache Science Data Analytics Platform

    Chaowei, Yang / Worley, Steve J. / Wilson, Brian et al. | NTRS | 2018

    Application of Compound Compressible Flow to a Boundary Layer in a Hypersonic Three-Dimensional Inlet

    Bussey, Gillian / Lewis, Mark | AIAA | 2011

    Application of Compound Compressible Flow to Hypersonic Three-Dimensional Inlets

    Bussey, Gillian / Lewis, Mark | AIAA | 2009

    Application of compound compressible flow to nonuniformities in hypersonic propulsion systems

    LEWIS, MARK J. / HASTINGS, DANIEL E. | AIAA | 1989

    Application of waverider-based configurations to hypersonic vehicle design

    LEWIS, MARK | AIAA | 1991

    A rapid method of calculating the orbital radiation environment

    GATES, MICHELE / LEWIS, MARK | AIAA | 1991

    A re-evaluation of the waverider design process

    BURNETT, DAVID / LEWIS, MARK | AIAA | 1993

    ARTEMIS operations - Experiences and lessons learned

    Bester, Manfred / Cosgrove, Daniel / Frey, Sabine et al. | IEEE | 2014

    A simple analytical model for parametric studies of hypersonic waveriders

    Starkey, Ryan / Lewis, Mark | AIAA | 1998

    A SOLAR POWER SATELLITE SENDING A 1 MW INFRARED BEAM FROM GEO TO CONCENTRATING SOLAR POWER MODULES ON THE GROUND

    Fraas, Lewis / O'Neill, Mark J. | TIBKAT | 2020

    Assessment of a Surface Water Transportation System Concept for ISRU Operations on Mars

    Congiardo, Jared / Buckles, Bradley / Felt, Amy et al. | AIAA | 2024

    A stagnation point streamtube model for power law bodies

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

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