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hypersonic相关的网络例句

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A method using CFD technology is used for accurate prediction of aerodynamic force and heat of air-breathing hypersonic vehicles.

对吸气式高超声速飞行器而言,物面热流和摩阻的准确预测对飞行器设计及安全十分关键。

Hypersonic vehicle ; afterbody/nozzle ; integrated design ; genetic algorithms

高超声速飞行器;后体/尾喷管;一体化设计;遗传算法

Aiming at the strong coupling characteristic during the multi-disciplinary optimization process of hypersonic aerocraft, in order to reduce computing time and increase the feasibility of optimization process, this paper adopted the approximate method to build the responding model between disciplines, In this paper, under the condition of ensuring the engine stable and high efficient , the designing work also consider the whole aerocraft performance sufficiently from the effect of forebody and afterbody.

针对高超音速飞行器多学科设计优化过程中的强耦合特性,为了减少计算时间,提高优化过程的可行性,采用近似的方法来建立学科之间的响应模型,以此来减少每次迭代时所用的大量计算时间。

Through ground test and hypersonic flow research, he made great progress in air-breathing hypersonic technology.

通过地面试验和高超声速非平衡流的研究,取得了再入突防气动物理的重要进展。

In the longer term, air-breathing hypersonic craft could cut the cost of reaching space.

从长远来看,吸入式超高音速飞行器能削减太空之旅的成本。

Air-breathing hypersonic vehicle 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。

In order to grasp the hypersonic vehicle models complex dynamic characteristics,a new hypersonic vehicle model method was proposed.

为了掌握高超音速飞机复杂的动态特性,提出了一种研究高超音速飞机模型的新方法。

In order to improve penetrativity of hypersonic missile and enable air-launched hypersonic cruise missile to penetrate with skip trajectory, a new approach of generating positive angle of attack during reentry phase of trajectory was proposed. Some key parameters of realizing skip trajectory were found out, and the effects of these parameters on ballistic performance were discussed.

为提高高超声速导弹的突防能力,使常规布局空中发射的高超声速巡航弹能采用跳跃式弹道突防,采用了在导弹再入段附加相应的正攻角产生气动升力的方法,找出了实现弹道起跳的关键参数,讨论了这些参数对弹道性能的影响。

Results indicate:(1) The newly developed simulation technology can form fairly average and easily controllable back pressure downstream the inlet, so it can he used to investigate the back pressure characteristics of hypersonic inlets.(2) By regulating the valve of injection pipe, the simulation technology can realize the switch of hypersonic inlet started state and unstarted state in about 8 milliseconds, so it is suitable to investigate the starting/unstarting/resarting problem of hypersonic inlets.

结果表明:(1)所提出的凹腔喷流技术可在进气道下游形成较为均匀的、可控的背压环境,因此可用于进气道的反压特性研究;(2)适当调节凹腔的喷流总压,并在实验中实时控制阀门的开度,凹腔喷流技术能够在较短的风洞实验时间内(约8s)实现进气道起动、不起动、再起动流态之间的切换,因此可用于进气道的不起动/再起动特性研究。

Firstly, studies for hypersonic inlets are reviewed, including issues related to interaction between boundary and shock wave in hypersonic inlet, unstarting/restarting phenomena, isolator, boundary bleeding for hypersonic inlet, internal/external compression ratio for inlet, inlets with sidewall compression, etc..

首先是高超声速进气道的研究进展,包括高超声速进气道中激波与附面层干扰、起动和再起动、隔离段、进气道附面层抽吸、进气道通道内外压缩比、侧压式进气道、Busemann进气道等。

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