FINITE ELEMENT MODELING AND OPTIMIZATION OF AEROSPACE STRUCTURES.

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作者：
Dwyer, Walter J.
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Technical Report AFFDL-TR - Air Force Flight Dynamics Laboratory (United States) | 1972年
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摘要：
Description of the results of a study of the optimization of typical aircraft structural components using the previously described Automated Structural Optimization Program (ASOP). The structures examined were a fuselage structure for a proposed space shuttle orbiter and a wing structure for the same vehicle. Examples are given of practical finite element modeling of these structures.
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