This paper introduces the trim aerodynamic characteristics of re - entry modules.

本文主要介绍小升阻比载人飞船返回舱的配平气动特性.

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The static aerodynamic characteristics for slender bodies at large angle of attack was analyzed.

研究分析了细长旋成体弹身类型气动外形的大攻角范围气动特性.

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This paper studies the effect of vectoring jet on the transverse aerodynamic characteristics of slender body.

采用测压方法研究了矢量喷流对细长旋成体大迎角非对称流动的影响特性.

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Now to develop a shape with good aerodynamic characteristics becomes a significant work.

设计在高超声速条件下具有良好气动特性的外形也成为一项关键性工作.

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