大家都搜：
高超声速再入
1、reentry shock───再入激波
1、paper, plasma wake flow of hypersonic reentry vehicle and radar scattering characteristics have been studied.───入飞行器等离子体尾迹及其雷达散射特性进行了分析、研究和大量的计算。
2、Numerical study of heat transfer predictionsfor hypersonic reentry bodies───声速再入体表面热流数值模拟研究
3、A novel guidance law is devised for developing the guidance technology of optimal glide of a hypersonic reentry vehicle.───针对高超声速再入飞行器最远距离滑翔制导关键技术，设计了一种新型制导律。
4、novel guidance law is devised for developing the guidance technology of optimal glide of a hypersonic reentry vehicle.───声速再入飞行器最远距离滑翔制导关键技术，设计了一种新型制导律。
5、Numerical studies of non-equilibrium flow-fields over a capsule-type hypersonic reentry vehicle───带座舱飞船高超声速再入非平衡流场的数值研究
6、Predicting Heating Distributions for Hypersonic Reentry Bodies───高超声速再入体表面热流计算
7、Numerical study of aeroheating predictions for hypersonic reentry bodies───高超声速再入钝头体表面热流计算
8、Variable bend tail concept may be one of the possible approaches for satisfying the maneuvering requirement of hypersonic reentry vehicle.───可变弯尾飞行器的气动方案是高超声速机动的潜在可行方案。