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Comparison of Experimental and Computational Aerothermodynamics of a 70-deg Sphere-Cone.

机译：70度球锥的实验和计算气动热力学比较。

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Numerical solutions for hypersonic flows of carbon-dioxide and air around a 70-deg sphere-cone have been computed using an axisymmetric non-equilibrium Navier-Stokes solver. Freestream flow conditions for these computations were equivalent to those obtain ...

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B. R. Hollis J. N. Perkins;
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年度 1996
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
70-deg sphere-cone; Aerobrake configurations; Aerothermodynamics; Air; Blunt-body flows; Carbon dioxide; Comparisons; Cones; Hypersonic flow; Surface heat transfer rates; Turbulent flow;

机译：70度球形锥体; aerobrake配置;气动热力学;空气;钝体流动;二氧化碳;比较;锥体;高超声速流动;表面传热速率;湍流;

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7. Comparison of Experimental and Computational Aerothermodynamics of a 70-deg Sphere-Cone [O] . Brian R. Hollis, John N. Perkins 2008

机译：70度球锥的实验和计算空气热力学的比较

Comparison of Experimental and Computational Aerothermodynamics of a 70-deg Sphere-Cone.

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