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Investigation at supersonic speeds of a translating-spike inlet employing a steep-lip cowl

机译：使用陡唇罩进行平移钉入口的超音速研究

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作者
Gorton, Gerald C;
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年度 1954
页码 1-32
总页数 32
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Investigation of aerodynamic heating in V-shaped cowl-lip of the inward turning inlet [J] . Meng Zewei, Fan Xiaoqiang, Xiong Bing, Proceedings of the Institution of Mechanical Engineers . 2019,第8期

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3. Buzz evolution process investigation of a two-ramp inlet with translating cowl [J] . Shi Wen, Chang Juntao, Wang Youyin, Aerospace science and technology . 2019,第JANa期

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4. Matematical Modeling of Supersonic Turbulent Flows in Inlets with Rotating Cowl [C] . Bedarev I.A., Fedorova N.N., Goldfeld M.A., International Conference on Computational Fluid Dynamics . 2006

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5. Rocket Based Combined Cycle Exchange Inlet Performance Estimation at Supersonic Speeds . [D] . Murzionak, Aliaksandr. 2013

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6. Effect of Inlet and Outlet Flow Conditions on Natural Gas Parameters in Supersonic Separation Process [O] . Yan Yang, Chuang Wen, Shuli Wang, 2010

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7. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot [O] . Trefny C. J., Welge H. R., Powell A. G. 1985

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Investigation at supersonic speeds of a translating-spike inlet employing a steep-lip cowl

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