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Hot gas piloted energy for supersonic combustion of kerosene with dual-cavity

  • Published:2001-01-08 Issue: Volume: Page:
  • ISSN:
  • Container-title:39th Aerospace Sciences Meeting and Exhibit
  • language:
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Author:

Situ M.1,Wang C.1,Lu H.1,Yu G.2,Zhang X.2

Affiliation:

1. CASC, Beijing, China

2. CAS, Inst. of Mechanics, Beijing, China

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Segal C, Owens M G, Tehranian S and Vinogradov V." Flameholding configurations for kerosene combustion in a mach 1.8 airflow," AIAA 97-2888.

2. Mathur,T., Lin,K.C., Kennedy, Gruber,M., Donbar,!., Jackson,T., and Billig,F.S."Liquid JP7 combustion in a scramjet combustor," AIAA 2000-3581.

3. Baurle,R.A., and Gruber,M.R."A study of recessed cavity flowfields for supersonic combustion applications," AIAA 98-0938.

4. Burnes, R., Parr, T.P., Wilson, K.J., Yu,K."Investigation of Supersonic Mixing Control Using Cavities:effect of fuel injection location,"AIAA 2000-3618.

5. K.Yu, KJ.Wilson, R.A.Smith, K.C. Schadow, "Experimental Investigation on Dual-Purpose Cavity in Supersonic Reacting Flows," AIAA 98-0723.

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1. Introduction;Unsteady Supersonic Combustion;2020

2. Numerical and experimental study on flame structure characteristics in a supersonic combustor with dual-cavity;Acta Astronautica;2015-12

3. Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity;Acta Astronautica;2015-03

4. Research on Hot Gas Jet Ignition Process of Scramjet Combustor Fueled with Kerosene;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

5. Integrated Liquid-Fuel-Injector/Plasma-Igniter for Scramjets;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15
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