Inlet ramp for supersonic or hypersonic aircraft

• 1. 梭镖型垂直发射可返回高超音速导弹飞机 [P] . 中国专利： CN112594089A . 2021-04-02
• 2. 飞碟型垂直起降高超音速喷气隐形飞机 [P] . 中国专利： CN106005402B . 2018.09.04
• 3. Two-dimensional supersonic and hypersonic air inlet, with three movable ramps, for the combustion air of an aircraft engine. [P] . 法国专利： FR2710607B1 . 1995-12-01

  机译： 具有三个可移动坡道的二维超音速和高超音速进气口，用于飞机发动机的燃烧空气。

• 4. Two-dimensional supersonic and hypersonic air intake with three movable ramps for the combustion air of an aircraft engine [P] . 德国专利： DE69406622T2 . 1998-05-20

  机译： 具有三个可移动坡道的二维超音速和高超音速进气口，用于飞机发动机的燃烧空气

• 5. Bidimensional supersonic and hypersonic air intake with three mobile ramps for the combustion air of an aircraft engine [P] . 欧洲知识产权局专利： EP0646525B1 . 1997-11-05

  机译： 具有三个移动坡道的二维超音速和高超音速进气口，用于飞机发动机的燃烧空气

• 1. Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack [J] . 刘建新, 罗纪生 应用数学和力学：英文版 . 2010,第005期
• 2. Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack [J] . Jian-xin LIU, Ji-sheng LUO 应用数学和力学（英文版） . 2010,第005期
• 3. Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions [J] . W.H.Fan, F.Q.Zhong, S.G.Ma, 力学学报：英文版 . 2019,第005期
• 4. Experimental Investigation of a Fixed-geometry Two-dimensional Mixed-compression Supersonic Inlet with Sweep-forward High-light and Bleed Slot in an Inverted "X"-type Layout [J] . Wan Dawei, Guo Rongwei 中国航空学报（英文版） . 2007,第004期
• 5. Large-eddy Simulation of Shock-wave/Boundary-layer Interactions in Hypersonic Inlet Compression Ramps [C] . L. Krishnan, N. D. Sandham, J. Steelant International Symposium on Air Breathing Engines . 2007
• 6. Inlets of Supersonic Airplanes with Deflection Ramps [D] . Manjunath, Kallanna James. 2020
• 7. Supersonic and Hypersonic Flight [O] . 1960
• 8. Numerical Analysis of Supersonic Film Cooling in Supersonic Flow in Hypersonic Inlet with Isolator [O] . Silong Zhang, Jiang Qin, Wen Bao, 2014
• 9. Performance of supersonic ramp-type side inlet with combinations of fuselage and inlet throat boundary-layer removal [R] . Campbell, Robert C 1956

• 1. Application of Nano Technique in Measuring Supersonic/Hypersonic Flow [J] . Chen Zhi ,YI Shihe ,Zhu Yangzhu . 材料科学建模与数值模拟（英文） . 2013,第1期
• 2. 高超音速二维进气道设计和起动性能研究 [C] . 宋文艳 ,刘伟雄 ,贺伟 . 第十一届全国激波与激波管学术会议 . 2004
• 3. DSMC方法在过渡区超音速、高超音速流动中的应用研究 [A] . 汤继斌 . 2005