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Physical criterion study on forward stagnation point heat flux CFD computations at hypersonic speeds
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作者 李邦明 鲍麟 童秉纲 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2010年第7期839-850,共12页
In order to evaluate uncertainties in computational fluid dynamics (CFD) computations of the stagnation point heat flux, a physical criterion is developed. Based on a quasi-one-dimensional hypothesis along the stagn... In order to evaluate uncertainties in computational fluid dynamics (CFD) computations of the stagnation point heat flux, a physical criterion is developed. Based on a quasi-one-dimensional hypothesis along the stagnation line, a new stagnation flow model is applied to obtain the governing equations of the flow near the stagnation point at hypersonic speeds. From the above equations, the compatibility relations are given at the stagnation point and along the stagnation line, which consist of the physical criterion for checking the accuracy in the stagnation point heat flux computations. The verification of the criterion is made with various numerical results. 展开更多
关键词 quasi-one-dimensional hypothesis stagnation point heat flux hypersonic flow physical criterion
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高超声速飞行器前驻点热流数值模拟的物理准则研究 被引量:3
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作者 李邦明 鲍麟 童秉纲 《应用数学和力学》 CSCD 北大核心 2010年第7期801-811,共11页
通过建立高超声速飞行器前驻点处沿驻点线的准一维流简化模型,再将头激波后流场分为无粘区和近壁粘性区,然后从N-S方程组出发,利用流场对称性和量级分析方法,最终推导出驻点邻域简化控制方程组,并证明了其流动具有边界层型特征.在此基础... 通过建立高超声速飞行器前驻点处沿驻点线的准一维流简化模型,再将头激波后流场分为无粘区和近壁粘性区,然后从N-S方程组出发,利用流场对称性和量级分析方法,最终推导出驻点邻域简化控制方程组,并证明了其流动具有边界层型特征.在此基础上,根据该控制方程组,给出了计算结果应满足的壁面驻点以及沿驻点线的相容关系,成为热流CFD计算准确与否应遵循的物理准则.最后通过算例验证了物理准则作为热流CFD计算可靠性判据的正确性. 展开更多
关键词 准一维流 驻点热流 高超声速 物理准则
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