Design and Investigation of Hypersonic Scramjet Inlet for Mach number of 10 and its performance at various flight regimes

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Design and Investigation of Hypersonic Scramjet Inlet for Mach number of 10 and its performance at various flight regimes

机译：马赫数为10的高超音速超燃冲压进气口的设计与研究及其在各种飞行状态下的性能

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《Advances in Natural and Applied Sciences》 |2016年第7期|共7页
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1. Analysis and Design of a Scramjet Engine Inlet Operating from Mach 5 to Mach 10 [J] . Luu Hong Quan, Nguyen Phu Hung, Le Doan Quang, International Journal of Mechanical Engineering and Applications . 2016,第1期

机译：从5马赫到10马赫的Scramjet发动机进气道的分析和设计
2. Shock-Wave Modes of Flow at the Inlet to the Diffuser of a Hypersonic Scramjet Engine: The Effect of Flight Altitude and Velocity [J] . G. A. Tarnavskii High temperature: English translation of teplofizika vysokikh temperatur . 2005,第1期

机译：高超音速超燃发动机扩散器入口处的冲击波流动模式：飞行高度和速度的影响
3. Suppression of Combustor-Inlet Interaction in a Scramjet Engine under Mach 4 Flight Conditions [J] . Kan Kobayashi, Takeshi Kanda, Sadatake Tomioka, Transactions of the Japan society for aeronautical and space sciences . 2007,第166期

机译：在4马赫飞行条件下超燃冲压发动机中燃烧器-进气道相互作用的抑制
4. Combined Numerical and Experimental Investigation of a 2-D Scramjet Inlet at Mach Numbers from 10 to 25 [C] . D.Messitt, H.Nagamatsu, L.Mrabo AIAA Sixth International Aerospace Planes and Hypersonics Technologies Conference 3-7 April 1995 / Chattanooga, TN . -1

机译：马氏数为10到25的二维Scramjet进气道的组合数值和实验研究
5. Investigation of side wall effects on an inward scramjet inlet at Mach number 8.6. [D] . Rolim, Tiago Cavalcanti. 2013

机译：研究马赫数为8.6时向内超燃冲压进气口的侧壁效应。
6. Luminescent Measurement Systems for the Investigation of a Scramjet Inlet-Isolator [O] . Azam Che Idris, Mohd Rashdan Saad, Hossein Zare-Behtash, 2014

机译：用于研究超燃冲压发动机进气口隔离器的发光测量系统
7. Reynolds Number and Cowl Position Effects for a Generic Sidewall Compression Scramjet Inlet at Mach 10: A Computational and Experimental Investigation [O] . Holland Scott D. 1992

机译：通用侧壁压缩超燃冲压发动机进气口在10马赫时的雷诺数和风帽位置影响：计算和实验研究

Design and Investigation of Hypersonic Scramjet Inlet for Mach number of 10 and its performance at various flight regimes

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