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Performance of supersonic ramp-type side inlet with combinations of fuselage and inlet throat boundary-layer removal

机译：超音速斜面式侧入口的性能与机身和入口喉部边界层移除的组合

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作者
Campbell, Robert C;
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年度 1956
页码 1-21
总页数 21
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Design of top mounted supersonic inlets for a cylindrical fuselage [J] . Saheby Eiman B., Huang Gouping, Hays Anthony Proceedings of the Institution of Mechanical Engineers . 2019,第8期

机译：圆柱形机身顶部安装的超音速进气口的设计
2. Design of top mounted supersonic inlets for a cylindrical fuselage [J] . Saheby Eiman B., Huang Gouping, Hays Anthony Proceedings of the Institution of Mechanical Engineers . 2019,第8期

机译：用于圆柱形机身的顶部安装超音速入口的设计
3. Experimental characteristics of a supersonic three-dimensional air inlet with adjustable throat [J] . Gounko Y.P., Mazhul I.I. Thermophysics and Aeromechanics . 2013,第1期

机译：嗓音可调的超音速三维进气口的实验特性
4. Control of shock/boundary-layer interactions in a supersonic inlet isolator using geometric modification [C] . Raihan Ali Khan, Shadman Tahmid, A. B. M. Toufique Hasan International Conference on Mechanical Engineering . 2018

机译：使用几何修改控制超音速入口隔离器中的冲击/边界层交互
5. The Supersonic Performance of High Bypass Ratio Turbofan Engines with Fixed Conical Spike Inlets [D] . Cleary, Spencer. 2018

机译：高旁路比率涡发发动机与固定锥形尖峰入口的超音速性能
6. Effect of Inlet and Outlet Flow Conditions on Natural Gas Parameters in Supersonic Separation Process [O] . Yan Yang, Chuang Wen, Shuli Wang, 2010

机译：超声分离过程中进，出口流动条件对天然气参数的影响
7. On Supersonic-Inlet Boundary-Layer Bleed Flow [O] . Smith Gregory E., Harloff Gary J. 1995

机译：关于超音速入口边界层流失

Performance of supersonic ramp-type side inlet with combinations of fuselage and inlet throat boundary-layer removal

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