在飞行器的初步设计中,快速而有经济地估计出飞行器结构设计中的各种气动特性是非常必要的。
In flight vehicle preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of flight vehicle configuration designs.
这些飞行器上的油箱位置是相对轴向载荷作最佳结构设计来选择的。
The tank location for these vehicles is chosen for optimum airframe design for axial loads.
这些飞行器上的油箱位置是相对轴向载荷作最佳结构设计来选择的。
The tank location for these vehicles is chosen for optimum airframe design for axial loads .
掌握热防护系统(TPS)中热结构超合金蜂窝面板在热环境下的传热隔热特性,是飞行器防热结构设计的先决条件。
Knowledge of the thermal performance of Ni-based honeycomb sandwich panels in a thermal protection structure (TPS) is a prerequisite for the design of metal thermal protection structures(MTPS).
进行临近空间飞行器防空反导预警系统体系结构设计时,面临的主要问题之一是设计模拟对象的模型体系。
This paper is of great reference value to the design of air defense and anti-missile warning system.
进行临近空间飞行器防空反导预警系统体系结构设计时,面临的主要问题之一是设计模拟对象的模型体系。
This paper is of great reference value to the design of air defense and anti-missile warning system.
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