Pages that link to "Item:Q622597"

The following pages link to Optimization methods for advanced design of aircraft panels: a comparison (Q622597):

Displaying 4 items.

• System-based approaches for structural optimization of flexible mechanisms (Q1787401) (← links)
• Convergence of the direct limit analysis design method for discrete topology optimization (Q2138282) (← links)
• (Q3126654) (← links)
• A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing (Q5970621) (← links)