DESIGN PROBLEMS OF A DETONATION INITIATOR FOR STARTING COMBUSTION CHAMBERS OF AIRCRAFT DETONATION ENGINES

Authors

  • Kamil Mansurovich Ahmetgaleev VUNC VVS "VVA"
  • Taras Vasilevich Grasko
  • Sergey Mihaylovich Barancev
  • Irina Stanislavovna Moiseeva

Keywords:

ignition device, detonation, initiator, detonation combustion, shock waves, fuel-air mixture, cellular structure

Abstract

The article is devoted to the study of the specifics of designing an ignition device for combustion chambers using detonation as the combustion mode of the fuel-air mixture. An analysis of various sources was carried out, according to the results of which instructions were derived to provide the most optimal characteristics of this device.

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Published

2021-12-04

Issue

Vol. 25 No. 1 (91) (2021): Vestnik UGATU

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY