“high enthalpy hypersonicwind tunnel”的概念、定义、翻译、参考文献-科学参考

单词	high enthalpy hypersonicwind tunnel
释义	high enthalpy hypersonicwind tunnel Encyclopedia 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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