Pages that link to "Item:Q2310681"
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The following pages link to Transverse shear stress relaxed zigzag theory for cylindrical bending of laminated composite and piezoelectric panels (Q2310681):
Displaying 2 items.
- Assessment of improved zigzag and smeared theories for smart cross-ply composite cylindrical shells including transverse normal extensibility under thermoelectric loading (Q396166) (← links)
- Finite element model with continuous transverse shear stress for composite laminates in cylindrical bending (Q1277779) (← links)