Pages that link to "Item:Q622597"
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The following pages link to Optimization methods for advanced design of aircraft panels: a comparison (Q622597):
Displaying 7 items.
- Optimization of aircraft structural components by using nature-inspired algorithms and multi-fidelity approximations (Q1037371) (← links)
- 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)
- Optimization in aircraft engineering including approximate structural evaluations by support vector machines (Q2954911) (← links)
- (Q3126654) (← links)
- Preliminary design optimization of stiffened panels using approximate analysis models (Q4446709) (← links)
- A two-level procedure for the global optimum design of composite modular structures -- application to the design of an aircraft wing (Q5970621) (← links)
