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Effects of injector geometry on scramjet combustor performance

  • Published:1993-01 Issue:1 Volume:9 Page:146-152
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Chinzei Nobuo1,Komuro Tomoyuki1,Kudou Kenji1,Murakami Atsuo1,Tani Kouichiro1,Masuya Goro1,Wakamatsu Yoshio1

Affiliation:

1. National Aerospace Laboratory, Miyagi 981-15, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Cited by 32 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. Using numerical simulation to investigate the effect of injection configurations over the scramjet performance;Materials Today: Proceedings;2021

2. Fabrication of Sodium/Inconel 718 Heat Pipes for Combustor Cooling;Microgravity Science and Technology;2019-06-06

3. Highly cited literature of high-speed compressible flow research;Aerospace Science and Technology;2013-04

4. Numerical Simulation of Dual-Mode Scramjet Combustor with Significant Upstream Interaction;International Journal of Manufacturing, Materials, and Mechanical Engineering;2012-07

5. A three-dimensional computational study of the effect of the inlet conditions on supersonic mixing and combustion;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-03-08
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