Evaluation of Total Heat Transfer in Hypersonic Flow Environments.

机译：高超声速流动环境中总传热的评估。

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Equations for the total heat transfer to bodies in constant hypersonic flow environments and a ballistic trajectory environment have been derived. Using these equations and graphical results presented, total heat transfer can be easily evaluated for selected sphere-cone and flat-face cone geometries. (Author)

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baker, r. l. kramer, r. f.;
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年度 1978
页码 1-46
总页数 46
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; Equations; Geometric forms; Conical bodies; Laminar flow; Turbulent flow; Computations;

机译：高超声速流动;传热;方程;几何形状;锥形体;层流;湍流;计算;

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1. A low-computational-cost inverse heat transfer technique for convective heat transfer measurements in hypersonic flows [J] . Avallone F., Greco C. S., Schrijer F. F. J., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2015,第4期

机译：一种低计算成本的逆传热技术，用于高超声速流中的对流传热测量
2. Parametric study on the heat transfer of a blunt body with counterflowing jets in hypersonic flows [J] . Jinghui Guo, Guiping Lin, Xueqin Bu, International Journal of Heat and Mass Transfer . 2018,第juna期

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3. 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

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4. Predictions of Heat Transfer in Hypersonic Viscous Flows by an Improved Third-Order WENO Scheme [C] . Chen Li, Qin Li, Hanxin Zhang Asia-Pacific international symposium on aerospace technology . 2019

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5. Quantitative global heat-transfer measurements using temperature-sensitive paint on a blunt body in hypersonic flows [D] . Kurits, Inna 2008

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6. Analysis of Heat Transfers inside Counterflow Plate Heat Exchanger Augmented by an Auxiliary Fluid Flow [O] . A.-R. A. Khaled -1

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7. Heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity He, N2, air, and CO2 flows [O] . Wilder, S. E., Miller, C. G., Micol, J. R., 1983

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8. Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer Data for Flows Ahead of Ramps, Part of an Investigation of Hypersonic Flow Separation and Control Characteristics [R] . Kaufman, L. G. 1964

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Evaluation of Total Heat Transfer in Hypersonic Flow Environments.

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