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- hypersonic flight test 高超声速飞行试验
- The core of airbreathing technology is scramjet and airframe/propulsion integrated hypersonic flight vehicle. 吸气式高超声速技术的核心是超燃冲压发动机技术和机体/推进一体化飞行器技术。
- Participate in the flight test procedures improvement. 参与试飞程序的完善。
- A ramjet airplane engine designed for hypersonic flight that burns fuel in the supersonic airstream produced by the plane. 超音速冲压喷气发动机:一种喷气式飞机发动机,设计用于极超音速飞行,燃料在由飞机产生的超音速气流中燃烧。
- The unsteady aerodynamic characteristics of waverider aircraft is one of the most important physical problems in hypersonic flight. 乘波飞行器运动过程中的非定常气动特性是高超声速飞行中的重要物理问题之一。
- To set up Multidisciplinary Design Optimization (MDO) software system of hypersonic flight vehicle, a kind of modeling method oriented to MDO was studied. 摘要为建立高超声速飞行器多学科设计优化软件系统,研究了一种面向多学科设计优化的建模方法。
- For it s excellent performance, Rocket-Based-Combined-Cycle (RBCC) should be the most competitive propulsion system of Hypersonic Flight Vehicle for martial and civil purpose. RBCC发动机性能分析模型在高超声速飞行器方案选择、总体设计以及RBCC发动机设计与性能分析等方面具有极其重要的作用。
- Research of JL8 aircraft stall and spin flight test is described in this paper. 叙述了JL8飞机失速尾旋试飞状态、试飞方法和试飞结果。
- Typical aerospace hypersonic vehicles(flight test bed EXPERT supported by ESTEC and potential re-entry demonstrator ARES-H proposed by EADS-ST) have been tested in the Mach and Reynolds number ranges corresponding to realistic flight conditions. 在与实际飞行条件相对应的Mach数和Reynolds数条件下对典型的高超声速航天飞行器进行了实验。
- Any flight test and wind tunnel correlation always suffers from a great number of unknowns. 在对飞行试验与风洞试验进行比较时总有大量的未知数。
- As a kind of new configuration waveriders have high lift to drag ratio (L/D) in hypersonic flight, which makes the study of waverider shapes an important trend of hypersonic air vehicles development. 乘波构形在高超声速条件下的高升阻比优势备受关注,使得对于它的设计研究成为高超声速飞行器外形设计的一个重要方向。
- This marks the second time the NLOS-LS CLU was used in a flight test of the PAM missile. NLOS-LS为指挥官提供即时、精确响应的火力,打击移动和静止的陆地、海上目标。
- The flight test monitor and command system is main part of flight test engineering. 试飞监控与指挥系统是飞行试验工程中的重要组成部分。
- Describe the basic progression of the first flight tests. 请描述一下首飞测试的基本过程。
- In addition, preliminary proof for the half system flight test program of SITAN algorithm was discussed. 此外还对SITAN系统半 系统试飞方案作了初步的论证工作。
- hypersonic flight aerothermodynamics 特超音速(飞行)气动热力学
- hypersonic flight environment simulator 高超音速飞行环境模拟器
- The poesend problems in evaluation antiship missile flight test are pcinted out. 指出现行反舰导弹飞行试验结果评定的命中域标准存在的问题。
- Hypersonic Flight Environmental Simulator 超高音速飞行环境仿真器