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
Pages
12
From page
570
To page
581
Keywords
laminated composite - aircraft panel - strength criterion - load
Journal title
Strength of Materials
Serial Year
2004
Journal title
Strength of Materials
Record number
343781
Link To Document