Static and Dynamic Structural Response of an Aircraft Wing with Damage Using Equivalent Plate Analysis
49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 16th AIAA/ASME/AHS Adaptive Structures Conference,10th AIAA Non-Deterministic Approaches Conference, 9th AIAA Gossamer Spacecraft Forum, 4th AIAA Multidisciplinary Design Optimization Specialists Conference ; 2008 ; Schaumburg , IL
2008-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Nonlinear Dynamic Response Structural Optimization of a Joined-Wing Using Equivalent Static Loads
Online Contents | 2009
|AIAA-2006-2218 Equivalent Plate Analysis of Aircraft Wing with Discrete Source Damage
British Library Conference Proceedings | 2006
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