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高焓高超声速风洞
释义
高焓高超声速风洞
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理学
实验流体力学
释
high enthalpy hypersonicwind tunnel
高焓高超声速风洞
实验马赫数超过10或12的风洞。主要用于研究导弹、人造卫星或其他飞行器的超高马赫数飞行。在这类风洞中不仅要模拟高马赫数、高雷诺数等,而且要模拟真实飞行的高温(高焓)以及与气动加热有关的现象。
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adjustment method
adjustment of astro-geodetic network
adjustment of boiler combustion
adjustment of correlated observation
adjustment of economic structure
adjustment of marine gravity survey network
adjustment of mind
adjustment of observations
adjustment of pipe suspension and support
adjustment of posture
adjustment of respiration
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adjustment parameter
Adjustment, reform, rectification and improvement of the national economy
adjustment residual
adjustments and reconstructions of Chinese sociology
adjustment time
adjustment value
adjutant role in Canjun opera
adjuvant
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