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The Effect of Wall Temperature on Stagnation Region Heat Transfer and Shock Detachment Distance in Hypersonic Incipient Merged Layer Flow

机译：壁面温度对高超声速初始合并层流动中滞留区域传热和冲击距离的影响

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作者
Liu, J. T. C.;
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年度 1965
页码 p.1-43
总页数 43
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Hypersonic flow; Heat transfer; Stagnation temperature; Walls; Reynolds number; Shock waves;

机译：高超声速流动;传热;停滞温度;壁;雷诺数;冲击波;

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1. Effect of wall temperature on separation bubble size in laminar hypersonic shock/boundary layer interaction flows [J] . Amjad A Pasha, Khalid A Juhany Advances in Mechanical Engineering . 2019,第11期

机译：壁温对层压超声冲击/边界层相互作用流动分离气泡尺寸的影响
2. Shock wave boundary layer interactions in hypersonic flows over a double wedge geometry by using conjugate heat transfer [J] . Ravi K. Peetala, Vinayak Kulkarni, Niranjan Sahoo Heat transfer . 2021,第1期

机译：通过使用共轭热传递，在双楔几何上过度流动的冲击波边界层相互作用
3. Calculations of heat transfer in stagnation flow regions by using second-moment closure models in conjunction with the new general wall treatment [J] . B. Basara Progress in computational fluid dynamics . 2010,第4期

机译：通过使用第二矩闭合模型和新的常规壁面处理来计算滞流区域内的传热
4. NUMERICAL PREDICTION OF STAGNATION-POINT SHOCK-DETACHMENT DISTANCE FOR HYPERSONIC LOW-DENSITY FLOW OVER BLUNT NOSE SHAPES [C] . . 2004

机译：超声速低密度流过鼻形孔的定点震荡距离的数值预测
5. The influence of equivalence ratio and wall temperature on the ignition of hydrogen(2)/air mixtures in hypersonic flow boundary layers. [D] . Sussman, Darien. 1998

机译：当量比和壁温对高超声速流动边界层中氢（2）/空气混合物着火的影响。
6. MHD Stagnation-Point Flow and Heat Transfer with Effects of Viscous Dissipation Joule Heating and Partial Velocity Slip [O] . Mohd Hafizi Mat Yasin, Anuar Ishak, Ioan Pop -1

机译：粘滞耗散焦耳热和部分速度滑移对MHD驻点流动和传热的影响
7. Effect of wall temperature on separation bubble size in laminar hypersonic shock/boundary layer interaction flows [O] . Amjad A Pasha, Khalid A Juhany 2019

机译：壁温对层压超声冲击/边界层相互作用流动分离气泡尺寸的影响
8. Nongray Radiative Transfer Effects on the Radiating Stagnation Region Shock Layer and Stagnation Point Heat Transfer [R] . Anderson, J. D. 1967

机译：非辐射传递对辐射停滞区震动层和停滞点传热的影响

The Effect of Wall Temperature on Stagnation Region Heat Transfer and Shock Detachment Distance in Hypersonic Incipient Merged Layer Flow

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