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Shock Waves pp 871-876 | Cite as

Direct initiation of detonation with ignition tube

  • H. Chen
  • X. Y. Zhang
  • H. R. Yu
Conference paper

Abstract

Experiments of direct initiation of hydrogen-oxygen by means of a hot turbulent jet were made. Results indicate that the length of ignition tube is the dominant factor in determining the ignition capability of hot turbulent jet, and that the ignition capability of turbulence jet increases with the length of ignition tube. Because this ignition capability can meet the demands of a gas-detonation-driver shock tunnel and it doesn’t require additional facilities, the hot turbulent jet initiation method can be applied to large hydrogen-oxygen detonation-driver shock tunnels. Influences of obstacles on the ignition capability were also studied. It was found that the presence of obstacles weakens the ignition capability of a hot turbulent jet.

Keywords

Combustion Chamber Detonation Wave Shock Tube Inside Diameter Gaseous Detonation 
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

© Tsinghua University Press and Springer-Verlag Berlin Heidelberg 2005

Authors and Affiliations

  • H. Chen
    • 1
  • X. Y. Zhang
    • 1
  • H. R. Yu
    • 1
  1. 1.Key Laboratory of High Temperature Gas Dynamics, Institute of MechanicsChinese Academy of SciencesBeijingChina

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