3-D computation of parachute fluid-structure interactions - Performance and control
Author:
Affiliation:
1. U.S. Army, Soldier and Biological Chemical Command, Natick, MA
2. U.S. Army HPC Research Center; Rice Univ., Houston, TX
3. Fluent, Inc., Evanston, IL
4. Connecticut, Univ., Storrs
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1714
Reference20 articles.
1. A new strategy for finite element computations involving moving boundaries and interfaces—The deforming-spatial-domain/space-time procedure: I. The concept and the preliminary numerical tests
2. GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS
3. A 3-D finite element structural parachute model
4. Current 3-D structural dynamic finite element modeling capabilities
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