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Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions
Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions
Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions
Karpov, Y. S. (Autor:in)
STRENGTH OF MATERIALS C/C OF PROBLEMY PROCHNOSTI ; 36 ; 570-581
01.01.2004
12 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
620.11
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