Fluid-structure interaction modeling of the Orion spacecraft parachutes
The Team for Advanced Flow Simulation and Modeling (T☆AFSM) at Rice University has been developing the Stabilized Space--Time Fluid--Structure Interaction core technologies in conjunction with an array of special techniques to overcome the complexities present in modeling ringsail parachute...
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| Format: | Others |
| Language: | English |
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2011
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| Online Access: | http://hdl.handle.net/1911/61979 |