Effects of airstream Mach number on H2/N2 plasma igniter

Goro Masuya, Kenichi Takita, Katsuyoshi Takahashi, Fumio Takatori, Hiroyuki Ohzeki

研究成果: Article査読

28 被引用数 (Scopus)

抄録

Experimental study of the plasma igniter was conducted in nonheated high-speed air stream. The effects of the Mach number, from 0.9 to 2.4, and the stagnation pressure of the airstream, from 64 to 100 kPa, as well as the hydrogen fraction in the H2/N2 feedstock of the torch, from 0 to 50%, were investigated. In the higher Mach number airstream, more input power to the torch was required to ignite hydrogen fuel. The stagnation pressure of the airstream had complicated effects relating to chemistry and aerodynamics. Improvement of ignition performance due to the increased hydrogen fraction in the feedstock was well correlated with the sum of the electric input energy and the heat of combustion of the hydrogen fed as the feedstock of the torch.

本文言語English
ページ(範囲)679-685
ページ数7
ジャーナルJournal of Propulsion and Power
18
3
DOI
出版ステータスPublished - 2002

ASJC Scopus subject areas

  • 航空宇宙工学
  • 燃料技術
  • 機械工学
  • 宇宙惑星科学

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