Pages that link to "Item:Q1654950"
From MaRDI portal
The following pages link to Dual boundary element analysis of fatigue crack growth, interaction and linkup (Q1654950):
Displaying 10 items.
- Boundary element simulation of fatigue crack growth in multi-site damage (Q463491) (← links)
- Approximate methods for analyzing the growth of large cracks in fatigue damaged aircraft sheet material and lap joints (Q671733) (← links)
- A two-parameter model for crack growth simulation by combined FEM-DBEM approach (Q1008904) (← links)
- Residual strength of aircraft panels with multiple site damage (Q1315902) (← links)
- The multiple fatigue crack propagation modelling in nonhomogeneous structures using the DBEM (Q1634659) (← links)
- An exact and efficient X-FEM-based reanalysis algorithm for quasi-static crack propagation (Q1984904) (← links)
- Multiscale aircraft fuselage fatigue analysis by the dual boundary element method (Q2420299) (← links)
- Analytical prediction of crack coalesce in multiple site damaged structures (Q2576481) (← links)
- (Q4273940) (← links)
- Molecular Dynamics Simulation of Crack Growth in Mono-Crystal Nickel With Voids and Inclusions (Q6173030) (← links)