Pages that link to "Item:Q1654703"
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The following pages link to Boundary element analysis of stiffened panels with repair patches (Q1654703):
Displaying 13 items.
- Analysis of patched and stiffened cracked panels using the boundary element method (Q1204987) (← links)
- Analysis of cracks in aging aircraft structures, with and without composite-patch repairs (Q1207273) (← links)
- Analysis of bonded and fastened repairs by the \(p\)-version of the finite-element method (Q1827203) (← links)
- An object oriented system for damage tolerance design of stiffened panels (Q1961173) (← links)
- Single lap joint strength prediction using the radial point interpolation method and the critical longitudinal strain criterion (Q2301627) (← links)
- Nonlinear analysis of a composite panel with a cutout repaired by a bonded tapered composite patch (Q2385912) (← links)
- DBEM and FEM analysis on non-linear multiple crack propagation in an aeronautic doubler-skin assembly (Q2489077) (← links)
- The boundary element analysis of cracked stiffened sheets, reinforced by adhesively bonded patches (Q4216465) (← links)
- (Q4316161) (← links)
- Boundary element analysis of curved cracked panels with adhesively bonded patches (Q4446772) (← links)
- Analysis of Cracked Body Strengthened by Adhesively Bonded Patches by BEM-FEM Coupling (Q4987325) (← links)
- Boundary element analysis of cracked panels repaired by mechanically fastened composite patches (Q5945894) (← links)
- Boundary element method for bending-extension coupling shear deformable laminated composite plates with multiple stiffeners (Q6577996) (← links)