Static and Dynamic Structural Response of an Aircraft Wing with Damage Using Equivalent Plate Analysis
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American Institute of Aeronautics and Astronautics
Reference9 articles.
1. Giles, G. L. "Equivalent Plate Modeling for Conceptual Design of Aircraft Wing Structures," AIAA1995-3945, Presented at 1stAIAA Aircraft Engineering, Technology and Operations Congress, Los Angeles,CA,Sept.19-21,1995.
2. Mason, B. H., Stroud, W., Krishnamurthy, T., Spain, C., and Naser, A. "Probabilistic Design of a Wind Tunnel Model to Match the Response of a Full-Scale Aircraft," AIAA-2005-2185, Presented at 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 13th AIAA/ASME/AHSAdaptiveStructures Conference,Austin,Texas,Apr.18-21,2005.
3. Equivalent plate analysis of aircraft wing box structures with general planform geometry
4. The 1989 Team
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