| 1. | Numerical simulation of 3d hypersonic thermochemical nonequilibrium flow
高超声速三维热化学非平衡流场的数值模拟 |
| 2. | Model reduction method based on optimization shaping for aero - engine controller
高超声速机的固定阶鲁棒控制器的设计 |
| 3. | Hypersonic shock tube
高超声速激波管 |
| 4. | The paper provides an description of stage separaton of hypersonic vechicle
本文简述了高超声速飞行器飞行过程中的分离问题。 |
| 5. | Numerical method on unstructured hybrid grid for hypersonic flows with magnetic fields
非结构混合网格高超声速绕流与磁场干扰数值模拟 |
| 6. | On the mathematical simulation of non - equilibrium hypersonic flow around the flying vehicle
关于飞行器高超声速不平衡气体绕流的数值模拟 |
| 7. | Discussion on integrated environment control thermal management system concepts for hypersonic vehicle
高超声速飞行器综合热管理系统方案探讨 |
| 8. | The application of uniform experimental design to configuration design of hypersonic aircraft
均匀试验设计法在高超声速飞行器外形设计中的应用 |
| 9. | Back pressure propagation mode and maximum working back pressure of hypersonic inlet isolator
高超声速进气道隔离段反压的前传模式及最大工作反压 |
| 10. | Hypersonic propulsion test facility is important for the scramjet ground tests
摘要高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。 |
