Pages that link to "Item:Q1953617"
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The following pages link to Free vibration and buckling response of hat-stiffened composite panels under general loading (Q1953617):
Displaying 5 items.
- Buckling analysis of stringer-stiffened laminated cylindrical shells with nonuniform eccentricity (Q363623) (← links)
- A genetic algorithm optimization of ring-stiffened cylindrical shells for axial and radial buckling loads (Q364791) (← links)
- Dynamic near three-to-one internal resonance in composite stiffened panels (Q366700) (← links)
- Formulation and evaluation of a finite element model for the linear analysis of stiffened composite cylindrical panels (Q1351485) (← links)
- A numerical approach for limit analysis of orthotropic composite laminates (Q3587857) (← links)