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Numerical study of the performance of swept, curved compression surface scramjet inlets

  • Published:1994-11 Issue:6 Volume:10 Page:841-847
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Korte John J.1,Singh D. J.2,Kumar Ajay3,Auslender Aaron H.4

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

2. Analytical Services and Materials Inc., Hampton, Virginia 23666

3. NASA Langley Research Center, Hampton, Virginia 23681

4. Lockheed Engineering and Sciences Company, Inc., Hampton, Virginia 23666

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Study on aerodynamic performance of outlet pipe of ram air system;Fourth International Conference on Mechanical, Electronics, and Electrical and Automation Control (METMS 2024);2024-06-05

2. Recent advances and prospects in hypersonic inlet design and intelligent optimization;Aerospace Science and Technology;2024-03

3. Study on the separation in the shock wave/boundary layer interaction induced by a curved fin;Physics of Fluids;2023-07-01

4. Study on the aerodynamic performance of inlet pipe different bending radius of ram air system;Journal of Physics: Conference Series;2023-05-01

5. Starting Characteristics of Prandtl–Meyer Scramjet Intakes with Overboard Spillage;Journal of Propulsion and Power;2018-01
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