The following pages link to (Q4316161):
Displaying 11 items.
- Remaining life prediction of cracked stiffened panels under constant and variable amplitude loading (Q882190) (← links)
- 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)
- Fracture analysis of cracked orthotropic skin panels with riveted stiffeners (Q1573197) (← links)
- Crack propagation analysis of welded thin-walled joints using boundary element method. (Q1582020) (← links)
- Fracture mechanics analysis of curved stiffened panels using BEM. (Q1871060) (← links)
- An object oriented system for damage tolerance design of stiffened panels (Q1961173) (← links)
- An accurate Ritz approach for analysis of cracked stiffened plates (Q1984979) (← links)
- Boundary element method in dynamic analysis of structures with cracks (Q2486438) (← links)
- DBEM and FEM analysis on non-linear multiple crack propagation in an aeronautic doubler-skin assembly (Q2489077) (← links)
- Boundary element analysis of cracked panels repaired by mechanically fastened composite patches (Q5945894) (← links)