Distributed Computing for Probabilistic Structural Integrity Analysis of Aircraft Structures-Reference-Cited by-同舟云学术

Distributed Computing for Probabilistic Structural Integrity Analysis of Aircraft Structures

Published:2010-04-12 Issue: Volume: Page:
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Container-title:51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th
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Author:

Singh Gulshan,Ocampo Joan,Acosta Carlos,Millwater Harry

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. Parallel Implementation of Structural Dynamic Analysis for Parachute Simulation

2. 4Ghidella, J., Wakefield, A., Silvina, G.F., Friedman, J., and Cherian, V. “Use of Computing Clusters and Automatic Code Generation to Speed Up Simulation Tasks,” AIAA Modeling and Simulation Technologies Conference and Exhibit, Hilton Head, South Carolina, USA, Aug.20-23,2007, pp. AIAA2007-6880.

3. 5Bhardwaj, M., Reese, G., Drissen, B., Alvin, K., and Day, D. “Salinas - An implicit Finite Element Structural Dynamic Code Developed for Massively Parallel Plateforms,” 41stAIAA Structures,Structural Dynamics, and Materials Conference Atlanta, GA,USA, 2000, pp. AIAA2000-1651.

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