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The Numerical Solution of Mach-Zehnder Interferogram Analysis of Supersonic Airflow about Cylindrical and Symmetrical Projectiles

机译：圆柱形和对称弹丸超音速气流mach-Zehnder干涉图分析的数值解

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作者
Ding, P.; Pan, S.;
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年度 1982
页码 p.1-19
总页数 19
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Supersonic flow; Projectiles; Numerical analysis; Interferograms; Shock waves; Air flow; China;

机译：超音速流;弹丸;数值分析;干涉图;冲击波;气流;中国;

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3. Numerical combustion analysis for a two-staged combustion strut in supersonic airflow [J] . S. Ogami, T. Niioka 燃焼研究 . 2003,第132期

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5. A Numerical Comparison of Symmetric and Asymmetric Supersonic Wind Tunnels. [D] . Clark, Kylen D. 2015

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6. Non-Uniform Curvature Model and Numerical Simulation for Anti-Symmetric Cylindrical Bistable Polymer Composite Shells [O] . Zheng Zhang, Xiaochen Yu, Helong Wu, 2020

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7. Experimental Investigations of the Supersonic Flow past a Circular Cylinder by the Mach-Zehnder Interferometer [O] . Shigeo UCHIDA, Michiru YASUHARA 1957

机译：通过Mach-Zehnder干涉仪通过圆柱体的超音速流动的实验研究
8. The Numerical Solution of Mach-Zehnder Interferogram Analysis of Supersonic Airflow about Cylindrical and Symmetrical Projectiles. [R] . Ding, P., Pan, S. 1982

机译：圆柱形和对称弹丸超音速气流mach-Zehnder干涉图分析的数值解。

The Numerical Solution of Mach-Zehnder Interferogram Analysis of Supersonic Airflow about Cylindrical and Symmetrical Projectiles

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