最小重量和强度将确保使用真空袋建设。
Minimum weight and strength will be ensured by using a vacuum-bag construction.
在已知的不同质心位置下求得相应的最小重量机翼外形。
Wing shapes with minimum weight corresponding to variant center-of-gravity positions were obtained.
研究了应力约束下最小重量悬臂梁桁架结构的拓扑优化设计。
Topology optimization design of minimum weight cantilever trusses subjected to stress constraints is studied.
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