Title of article :
Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions
Author/Authors :
Ya. S. Karpov ، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2004
Keywords :
laminated composite - aircraft panel - strength criterion - load
Journal title :
Strength of Materials
Journal title :
Strength of Materials
