The structure is then optimized based on above methods, taking structure weight as objective function.
在此基础上,以壳体重量为目标函数对结构进行了优化设计。
The tests indicate that, the fuselage-missile compatibility can be met by structural improvement with minor weight penalty for the primary force-taking structure of thin shell without stringer.
试验表明对于轻型直升机薄壁无长桁主承力结构,只要以极小的重量代价改进结构设计,就能够满足机弹相容性要求。
Taking structure weight as objective function, the optimization model of overweight breech of a type of automatic weapon was established, and its structure topological optimization was performed.
以结构质量为目标函数,建立了某自动武器超重部件枪尾的优化模型,进行了结构拓扑优化。
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