Pages that link to "Item:Q1371550"
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The following pages link to Post-buckling behaviour of graphite/epoxy stiffened panels with initial imperfections subjected to eccentric biaxial compression loading (Q1371550):
Displaying 5 items.
- Postbuckling of imperfect rectangular composite plates under inplane shear closed-form approximate solutions (Q364757) (← links)
- Comments on ``Buckling behavior of a graphite/epoxy composite plate under parabolic variation of axial loads'' [Int. J. Mech. Sci. 45, No. 6-7, 1135--1147 (2003)] (Q986260) (← links)
- Buckling of biaxially compressed anisogrid stiffened composite cylindrical panel with clamped edges (Q2224631) (← links)
- Axisymmetric free and forced vibrations of initially stressed circular nanoplates embedded in an elastic medium (Q2392851) (← links)
- POSTBUCKLING OF COMPRESSIVELY LOADED IMPERFECT COMPOSITE PLATES: CLOSED-FORM APPROXIMATE SOLUTIONS (Q3002028) (← links)