Computational Challenges in Simulating Powered Flight of the Orion Launch Abort Vehicle (Invited)
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3339
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1. A parallel multilevel method for adaptively refined Cartesian grids with embedded boundaries
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5. High Resolution Aerospace Applications Using the NASA Columbia Supercomputer
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1. CFD Simulations of the Space Launch System Ascent Aerodynamics and Booster Separation;53rd AIAA Aerospace Sciences Meeting;2015-01-03
2. Effects of the Orion Launch Abort Vehicle Plumes on Aerodynamics and Controllability;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
3. Modeling Powered Aerodynamics for the Orion Launch Abort Vehicle Aerodynamic Database (Invited);29th AIAA Applied Aerodynamics Conference;2011-06-27
4. Rocket Plume Scaling for Orion Wind Tunnel Testing (Invited);29th AIAA Applied Aerodynamics Conference;2011-06-27
5. Overflow Simulation Guidelines for Orion Launch Abort Vehicle Aerodynamic Analyses (Invited);29th AIAA Applied Aerodynamics Conference;2011-06-27
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