Effect of airstream mach number on H2/N2 plasma igniter

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

Effect of airstream mach number on H₂/N₂ plasma igniter

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

Research output: Contribution to conference › Paper › peer-review

Abstract

Experimental study of the plasma igniter was conducted in non-heated high-speed airstream. The effects of the Mach number and the stagnation pressure of the airstream as well as the hydrogen fraction in the H²/N² feedstock of the torch 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 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.

Original language	English
Publication status	Published - 2001
Externally published	Yes
Event	39th Aerospace Sciences Meeting and Exhibit 2001 - Reno, NV, United States Duration: 2001 Jan 8 → 2001 Jan 11

Other

Other	39th Aerospace Sciences Meeting and Exhibit 2001
Country/Territory	United States
City	Reno, NV
Period	01/1/8 → 01/1/11

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering

Cite this

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title = "Effect of airstream mach number on H2/N2 plasma igniter",

abstract = "Experimental study of the plasma igniter was conducted in non-heated high-speed airstream. The effects of the Mach number and the stagnation pressure of the airstream as well as the hydrogen fraction in the H2/N2 feedstock of the torch 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 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.",

author = "Goro Masuya and Kenichi Takita and Katsuyoshi Takahashi and Fumio Takatori and Hiroyuki Ohzeki",

year = "2001",

language = "English",

note = "39th Aerospace Sciences Meeting and Exhibit 2001 ; Conference date: 08-01-2001 Through 11-01-2001",

}

TY - CONF

T1 - Effect of airstream mach number on H2/N2 plasma igniter

AU - Masuya, Goro

AU - Takita, Kenichi

AU - Takahashi, Katsuyoshi

AU - Takatori, Fumio

AU - Ohzeki, Hiroyuki

PY - 2001

Y1 - 2001

N2 - Experimental study of the plasma igniter was conducted in non-heated high-speed airstream. The effects of the Mach number and the stagnation pressure of the airstream as well as the hydrogen fraction in the H2/N2 feedstock of the torch 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 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.

AB - Experimental study of the plasma igniter was conducted in non-heated high-speed airstream. The effects of the Mach number and the stagnation pressure of the airstream as well as the hydrogen fraction in the H2/N2 feedstock of the torch 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 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.

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M3 - Paper

AN - SCOPUS:84897830132

T2 - 39th Aerospace Sciences Meeting and Exhibit 2001

Y2 - 8 January 2001 through 11 January 2001

ER -

Effect of airstream mach number on H₂/N₂ plasma igniter

Abstract

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ASJC Scopus subject areas

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