Equivalent Plate Analysis of Aircraft Wing with Discrete Source Damage-Reference-Cited by-同舟云学术

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Equivalent Plate Analysis of Aircraft Wing with Discrete Source Damage

Published:2006-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th
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Author:

Krishnamurthy Thiagarajan,Mason Brian

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. The 1989 Team

2. DimitriN.MavrisandWilliamT.Hayden,"Probabilistic AnalysisofanHSCT Modeledwith an EquivalentLaminated PlateWing,"AIAA-1997-5571,PresentedatAIAAandSAE,1997WorldAviation Congress,Anaheim,CA,Oct.13-16,1997.

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