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不同流态对高超声速飞行器热流的影响
Authors
李维东
王发民
雷麦芳
Publication date
1 January 2012
Publisher
Abstract
近空间高超声速巡航飞行,面临高升阻比复杂布局和长时间中低热流的气动热环境。飞行器周围流场中激波边界层干扰等复杂的流动现象,以及层流、转捩区和完全发展湍流等不同流态对气动热特性的影响,是一个很重要的工程科学问题。本文探讨了不同流态对气动加热的影响规律,建立了不同流态热流计算模型和数值求解方法。通过典型布局气动热实验结果的对比,说明模型是合理的
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Institute Of Mechanics,Chinese Academy of Sciences
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Last time updated on 12/02/2018