The university has been working on hypersonic technology for nearly 16 years.
该大学研究极超音速技术已经近16年了。
We know how to insert the aircraft into atmospheric hypersonic flight.
我们知道如何让飞机进入大气层并以高超音速飞行。
The system will be capable of destroying hypersonic and ballistic targets.
该系统将能够摧毁超音速和弹道目标。
HTV-2, an unmanned hypersonic aircraft designed to travel at Mach 20, failed during a test flight last month.
HTV - 2，一架巡航速度设计为20马赫的无人超音速飞机，于上月试飞失败。
Might the idea of near-hypersonic passenger aircraft, which has lain dormant for a few years, be coming back?
已被搁置多年的超音速民航客机概念是否会再次复苏？
Trajectory optimization is a key technology of hypersonic glide vehicle.
轨迹优化是高超声速滑翔式飞行器关键技术之一。
The next grat leap forward in aviation is expected to be hypersonic travel.
可以预料，航空学的下一个重大飞跃将是高超声速飞行。
A hypersonic cruise vehicle MDO model based on parametric method is established.
建立了基于参数方法的高超声速巡航飞行器MDO模型。
The thermal environment of the wedge leading edge is rigorous in hypersonic flow.
高超声速气流条件下，尖楔前缘的热环境非常恶劣。
In this thesis, the aerodynamic heating methods of hypersonic projectile are presented.
本论文进行了高超声速弹丸的气动热研究。
All these features make hypersonic flight control design a great challenge to researchers.
这些特点使得高超声速飞行器的飞行控制设计极具挑战性。
So research of power hypersonic vibration system and its control technique is paid more and more attention.
因此，功率超声振动系统及其控制的研究越来越受重视。
The analysis and computation of chemical nonequilibrium hypersonic wakes are important tasks of aerodynamics.
高超声速化学非平衡尾流的分析与计算是空气动力学中的一个重要课题。
The design and computation of the hypersonic nozzle have scientific and practical value to solve these problems.
而高超声速风洞喷管的设计和计算则对解决这一类问题具有重要的科学意义和实用价值。
Metallic thermal protection system (MTPS) provides a feasible solution for thermal protection of hypersonic vehicles.
金属热防护系统是高超飞行器热防护系统的理想候选方案。
In this paper, plasma wake flow of hypersonic reentry vehicle and radar scattering characteristics have been studied.
对再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。
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。
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。
Scramjet is the perfect propulsive device to hypersonic vehicle, and is a hot issue in current hypersonic technology area.
超燃冲压发动机是高超声速飞行器理想的动力装置，是当前高超声速技术领域的研究热点。
Trajectory optimization is one of the key factors in scheme planning of the new type of hypersonic gliding reentry vehicles.
轨迹优化是新型高超声速滑翔式再入飞行器方案设计的关键技术之一。
Air-breathing hypersonic vehicle(AHV) has been the next generation single stage to orbit vehicle and hypersonic cruise vehicle.
吸气式高超声速飞行器是下一代单级入轨和高超声速巡航研究的重点飞行器。
The new principles and methods of distributed parameter control may have an impact on the operation and design of hypersonic jets.
分布参数控制体系的新原理、方法、实现手段将对高超声速发动机系统的运行和设计产生重要影响。
The design concept and principle of injector valve system of hypersonic wind tunnel controlled by the computer are introduced in this paper.
本文介绍了高超声速风洞引射器阀门系统采用计算机控制的设计思想和原理框图。
The developing tools for hypersonic vehicle, i. e. ground test, computation and flight lest all have limitations for simulating hypersonic flight.
高超声速飞行器的设计工具，即地面试验、计算和飞行试验，在模拟高超声速飞行方面都有其局限性。
The developing tools for hypersonic vehicle, i. e. ground test, computation and flight lest all have limitations for simulating hypersonic flight.
高超声速飞行器的设计工具，即地面试验、计算和飞行试验，在模拟高超声速飞行方面都有其局限性。
应用推荐