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Experimental study on the effect of combustor configuration on the performance of dual-mode combustor

  • Published:2015-04 Issue: Volume:42 Page:169-175
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Wang Z.P.,Li F.,Gu H.B.,Yu X.L.,Zhang X.Y.

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference25 articles.

1. Hypersonic combustion and mixing studies using simultaneous OH-PLIF and schlieren imaging;Ben-Yakar,1998

2. Analysis of penetration and mixing of gas jets in supersonic cross flow;Billig,1992

3. Gas sampling/analysis of the high enthalpy supersonic flow;Chen,2005

4. Experimental study on combustion mode transition in a scramjet with parallel injection;Chun,2006

5. Laser-based measurements of OH, temperature, and water vapor concentration in a hydrocarbon-fueled scramjet;Gruber,2008

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