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1·The thermal environment of the wedge leading edge is rigorous in hypersonic flow.

高超声速气流条件下，尖楔前缘的热环境非常恶劣。

2·The steady hypersonic flow of air over a sphere is studied numerically using CFD-FASTRAN softwares.

利用CFD软件数值模拟高超声速空气绕流球体的层流流场。

3·Through ground test and hypersonic flow research, he made great progress in air-breathing hypersonic technology.

通过地面试验和高超声速非平衡流的研究，取得了再入突防气动物理的重要进展。

4·The results of numerical simulation of the hypersonic flow around a plate with a sharp leading edge are presented.

本文描述绕锐前缘平板高超声速流动的数值模拟结果。

5·The results showed that the method meets the requirements of sophisticated simulation of supersonic/hypersonic flow.

研究结果表明，该方法满足精细求解超声速/高超声速复杂流场要求。

6·This paper presents a numerical analysis of inviscid equilibrium and nonequilibrium hypersonic flow past blunt-nosed slender cones.

本文给出钝头细长锥无粘、平衡和非平衡高超声速绕流流场的数值分析。

7·It's necessary to recognize the different vortices, when aero-optical distortion caused by hypersonic flow is studied using vortex structure as the turbulence model.

利用涡结构对光波通过高速流场的光学传输特性进行建模，就必须进行涡结构的识别。

8·Numerical methods for hypersonic flow with chemical non-equilibrium reactions on the unstructured grid are used to analyze the drag induction of channel-configurations.

在非结构网格上对二维高超声速化学非平衡粘性绕流进行了数值模拟，并应用此方法对涵道构型高超声速减阻特性进行了数值分析。

9·Numerical methods for hypersonic flow with chemical non-equilibrium reactions on the unstructured grid are used to analyze the drag induction of channel-configurations.

在非结构网格上对二维高超声速化学非平衡粘性绕流进行了数值模拟 ，并应用此方法对涵道构型高超声速减阻特性进行了数值分析。

10·An engineering formula for estimating turbulent base heat transfer of hypersonic flow is given on the basis of flight data and the experimental results in shock tunnel.

本文综合飞行数据和激波风洞中的实验结果，给出了一个计算湍流底部热的工程方法。