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- A new method of quickly generating hypersonic waverider forebody configurations was developed. 发展了一种基于分析法的高超声速乘波构型飞行器前体设计方法。
- In this paper we develop a wedge-elliptical cone waverider configuration method, study on front body-scramjet engine integration design, and create a hypersonic waverider. 本文提出了一种变楔角楔/椭圆锥乘波体构型方法,并基于前体/进气道一体化设计思想,生成了高超声速乘波飞行器构型。
- Trajectory Characteristics of Hypersonic Waverider Missile with Rocket Extended Range 火箭增程乘波外形导弹弹道特性研究
- Parellel Numerical Simulation of the Three-dimensional Flow Field around the Hypersonic Waverider Shape Vehicle 高超声速乘波飞行器三维流场的并行数值模拟
- hypersonic waverider 高超声速乘波飞行器
- hypersonic waverider vehicle 高超声速乘波体飞行器
- 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。
- Hypersonic waveriders 高超声速乘波体
- FEM FCT is used to solve three dimensional hypersonic inviscid flow. 从Euler方程出发，利用流量修正有限元法（FEM?FCT）求解三维无粘流动的高速流场。
- 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。
- A conceptual design of the hypersonic civil transport is introduced here. 介绍了高超声速民用运输机的概念设计方案。
- 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。
- Investigation of waverider configuration in hypersonic wind tunnel 乘波外形高超声速风洞测力试验研究
- Hypersonic wind tunnels operating at very low densities were developed starting in about 1960. 低密度超音速风洞大约开始发展于1960年。
- Departures form the ideal practice followed by the Wright have been particularly noticeable in the development of supersonic and hypersonic vehicles. 特别值得注意的是在发展超音速和高超音速飞行器的过程中，偏离了莱特理想的工作方式。
- With such a large heat sink value, FRA can meet the requirement of hypersonic flying machine. 在 80 0℃时 ,两者都具有较高的热沉值 ,分别达到 5 6 9MJ kg和 6 6 0MJ kg ,该热沉值能够满足超高音速飞行器的热管理要求。
- The experimental results of low temperature ablator (beeswax and camphor) tests in the hypersonic wind Tunnel are presented in this paper. 本文给出了低温烧蚀材料的高超声速风洞烧蚀实验研究的结果。
- Cross-section design of a controllable hypersonic inlet. The research is being done at the Nanjing University of Aeronautics and Astronautics. 南京航空航天大学正在进行一个可控高超音速进气道断面设计研究。
- The analysis and computation of chemical non-equilibrium hypersonic wakes are important tasks of reentry aerodynamics. 高超音速化学非平衡尾迹流场的分析及计算是再入空气动力学的一个重要课题。
- SiO2/(Si3N4+BN) composite,a high performance hypersonic missile radome material,has been developed recently. SiO2/(Si3N4+BN)复合材料是近几年发展起来的综合性能优良的适用于高马赫数的导弹天线罩材料。
