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Measurements of OH and H2O for reacting flow in a supersonic combusting ramjet combustor

  • Published:1995-11 Issue:6 Volume:11 Page:1154-1161
  • ISSN:0748-4658
  • Container-title:Journal of Propulsion and Power
  • language:en
  • Short-container-title:Journal of Propulsion and Power

Author:

Parker Terence E.1,Allen Mark G.1,Foutter Richard R.1,Sonnenfroh David M.1,Rawlins W. Terry1

Affiliation:

1. Physical Sciences, Inc., Andover, Massachusetts 01810

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Cited by 15 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. Review of combustion stabilization for hypersonic airbreathing propulsion;Progress in Aerospace Sciences;2020-11

2. Flow Dynamics and Mixing of a Sonic Jet into Supersonic Crossflow;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

3. Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows;Physics of Fluids;2006-02

4. OH PLIF Imaging of Supersonic Combustion Using Cavity Injection;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16

5. Characterization of Expansion Tube Flows for Hypervelocity Combustion Studies;Journal of Propulsion and Power;2002-07
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