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高超声速

网络hypersonic; hypersonic velocity; hypersonic speed

高超声速

高超声速

高超声速

hypersonic

　　高超声速（Hypersonic）飞行器是指飞行速度大于5马赫（Mach）的飞行器，作为一种近空间飞行器，其研究与发展对军事战 …

hypersonic velocity

核能专业词汇英语翻译(F-L) ... hyperon bubble chamber 超子气泡室 hypersonic velocity 高超声速 hypertonic solution 高渗溶液 ...

hypersonic speed

机械专业英语词汇 -... ... hypersonic similarity 特超声速相似 hypersonic speed 高超声速 hypersonic speed 高超音速 ...

hypersonic eed

机械工程学专业词汇英语翻译... ... hypersonic similarity 特超声速相似 hypersonic eed 高超声速 hypersonic velocity 高超声速 ...

Hypersonie

高超声速(Hypersonie)一般指的是流动或飞行的速度超过5倍声速,即马赫数超过5。白60年代以来,以火箭为动力的高超声速技术 …

HyTech

...行器”(Hyper - X)计划,美国空军提出了 高超声速 (HyTech)计划。2001年,美国提出了新世纪的高超声速战略,将高超声速巡航 …

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Variable bend tail concept may be one of the possible approaches for satisfying the maneuvering requirement of hypersonic reentry vehicle .

可变弯尾飞行器的气动方案是高超声速机动的潜在可行方案。

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This method can be applied to pre-research and multi-objective optimization design of hypersonic QWV.

该方法可应用于高超声速类乘波体飞行器的概念研究和多目标优化设计。

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This paper presents the separation shock motion features induced by a hemicylindrically blunted fin in a hypersonic turbulent flow .

给出半圆柱前缘舵诱导的高超声速湍流分离激波运动特性。

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Strict performances of aerodynamics and requirements of thermal protection are put forward for the hypersonic aircrafts .

高超声速飞行对飞行器的气动性能以及防热提出了更高的要求。

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The steady hypersonic flow of air over a sphere is studied numerically using CFD-FASTRAN softwares .

利用 CFD 软件数值模拟高超声速空气绕流球体的层流流场。

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A sliding mode observer is designed to estimate the angle of attack and flight path angle for a hypersonic vehicle .

对一个高超声速飞行器设计了滑动模态观测器来估计攻角和航迹倾角。

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Hypersonic vehicle has a huge foreground in heading off the high speed and highly maneuvering target .

高超声速战术导弹以其固有的特点在高速目标拦截上应用前景巨大。

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The SERN of a hypersonic vehicle was designed for improving the lift and propulsion force .

为了提升高超声速飞行器单壁膨胀喷管的升力和推力，对其进行了优化设计。

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This brief communication introduces an experiment of hypersonic flow using high enthalpy expansion tube .

该研究简报介绍了用膨胀波管产生高超声速气流的实验结果。

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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。

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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。

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The data collected will be used by the Department of Defense to model and develop future hypersonic boost-glide capabilities.

所收集的数据将被国防部用于建模研发未来高超声速助推滑翔武器。

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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。

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