NASTRAN computer program differential stiffness and static load analysis methods compared for aircraft tandem side opening canopies
NASTRAN Differential Stiffness Analysis of an Aircraft Canopy
1971-09-01
Miscellaneous
No indication
English
Structural analysis of light aircraft using NASTRAN
AIAA | 1974
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|AIAA-2001-1320 Fuzzy Structures Analysis of Aircraft Panels in NASTRAN
British Library Conference Proceedings | 2001
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