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Combustion, Explosion and Shock Waves

, Volume 27, Issue 6, pp 669–674 | Cite as

Experimental investigation of H2 combustion and supersonic cooling in an annular channel

  • R. V. Albegov
  • V. A. Vinogradov
  • G. G. Zhadan
  • S. A. Kobyzhskii
Article
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Abstract

Results are presented for an experimental investigation of H2 combustion and cooling in a channel which simulates the intake and combustion chamber of a supersonic ram jet. Stable operation conditions were obtained for operating the intake and combustion chamber with various fuel distributions through the feed zones. The cooling rate and the combustion efficiency were determined at the chamber wall at varying flows in the channel.

Keywords

Combustion Dynamical System Mechanical Engineer Cool Rate Experimental Investigation 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Plenum Publishing Corporation 1992

Authors and Affiliations

  • R. V. Albegov
  • V. A. Vinogradov
  • G. G. Zhadan
  • S. A. Kobyzhskii

There are no affiliations available

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