| 1. | The flow over the geimini afterbody is separated .
双子星座后体处于分离状态。 |
| 2. | Influence of empennage on flow over upswept after - body
尾翼对民机后体流动特性的影响 |
| 3. | A man who s been ill , and isn t strong
“他是一个病后体弱的人！ |
| 4. | Numerical simulation of internal flow of contra - rotating axial flow fan
飞行器后体一体化数值模拟 |
| 5. | Tunnel - stern afterbody
隧道式后体 |
| 6. | Effect of ligustrazine on somatosensory evoked potential of rats with spinal cord injury
川芎嗪对大鼠脊髓损伤后体感诱发电位的影响 |
| 7. | Finally , the seven - hole probe experiment was made on the wake flow of the fuselage with empennage and engine cabins
并应用微型总压管进行了后体的边界层测量实验，得到了边界层平均速度分布。 |
| 8. | The research was made on the afterbody flow field of civil aircraft . the numerical simulation and aerodynamic experiments have all been executed in this paper
本文运用计算与实验相结合的研究方法对民机机身后体流场进行了研究。 |
| 9. | In divergent duct , adding heat can substitute the usage of geometry structure whatever mach number is . from force and thermodynamic cycle aspects , the effect of every components on engine performance was discussed
结果认为，对于后体为纯扩张构型的引射火箭，不论发动机通道内的马赫数是多少，都可以通过加热(改变加热位置)代替常规几何构型所起的作用。 |
| 10. | Based on the parametric design of aircraft shape , analyzing waverider design parameters , and combining with the aircraft forbody / inlet - aftbody / nozzle integral design , a conceptual study on the waverider aircraft was mainly presented
摘要基于飞行器外形参数化设计，通过分析乘波构型外形设计参数，结合飞行器前体进气道?后体喷管一体化设计思想，进行了乘波机的概念设计研究。 |
