51–100 von 123 Ergebnissen
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    Comparison of Robust Optimization Methods Applied to Hypersonic Vehicle Design

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

    Optimized mission-oriented waverider vehicles with base closure

    Takashima, Naruhisa / Lewis, Mark | AIAA | 1996

    Hypersonic missile requirements and operational tradeoff studies

    Stuckey, Richard / Lewis, Mark | AIAA | 1999

    Performance optimization of a SCRAM accelerator projectile

    Sabean, John / Lewis, Mark | AIAA | 1996

    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

    Aerodynamics for Optimal Engine-Integrated Airbreathing Launcher Configurations

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

    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

    The effect of high lift to drag ratio on aerobraking

    Crouse, Patrick / Lewis, Mark | NTRS | 1993

    Aerodynamic Stability of Re-Entry Heat Shield Shapes for a Crew Exploration Vehicle

    Johnson, Joshua / Starkey, Ryan / Lewis, Mark | AIAA | 2005

    Optimization of low-perigee spacecraft aerodynamics

    Bowman, D. / Lewis, Mark / Manzer, Dominic | AIAA | 2001

    DSMC of Power-Law Leading Edge Ionization for Hypersonic Telemetry Applications

    Hoult, Daniel / Starkey, Ryan / Lewis, Mark | AIAA | 2003

    Integrated Propulsion and Power Modeling for Bimodal Nuclear Thermal Rockets

    Clough, Joshua / Starkey, Ryan / Lewis, Mark et al. | AIAA | 2007

    Development of a Tool to Recreate the Mars Science Laboratory Entry Aerothermal Environment

    Beerman, Adam / Lewis, Mark / Santos, Jose et al. | AIAA | 2010

    Reactor Modeling for Bimodal Nuclear Thermal Rockets

    Clough, Joshua / Starkey, Ryan / Lewis, Mark et al. | AIAA | 2006

    Functional Fault Modeling Conventions and Practices for Real-Time Fault Isolation

    Ferrell, Bob / Brown, Barbara / Lewis, Mark et al. | AIAA | 2010

    Comparison of HTHL and VTHL Airbreathing and Rocket Systems for Access to Space

    Dissel, A. / Kothari, Ajay / Raghavan, V. et al. | AIAA | 2004

    Damage Detection Sensor System for Aerospace and Multiple Applications

    Williams, Martha / Lewis, Mark / Gibson, Tracy L. et al. | NTRS | 2017

    Subsonic experiments using the LoFlyte hypersonic waverider vehicle

    Blankson, Isaiah / Lewis, Mark / Pap, Robert | AIAA | 1998

    The University of Maryland Hypersonics Center - Status report

    Lewis, Mark / Pines, Darryll / Gupta, Ashwani | AIAA | 1998

    System Analysis of Launch Transportation Options for Crew Exploration Vehicle

    Dissel, Adam / Kothari, Ajay / Raghavan, Venkat et al. | AIAA | 2005