Research Reviews on Flameholders and Combustion of an Afterburner and a Ramjet Engine

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概要

• 論文の詳細を見る

• A super/hypersonic aircraft is expected to be realized in the 21st century. Ramjet engines with subsonic flow combustion may be used for its propulsion up to the flight speed range of Mach 6, in combination with other accelerating propulsive systems. Much research has been conducted on combustion problems related to this engine, but new and additional technologies are still needed to cope with the problems encountered in the advanced ramjet engine. By reviewing past work on flameholding techniques, the author will introduce recent research results in an attempt to resolve the problems involved in realizing super/hypersonic vehicle engines.

• 一般社団法人日本機械学会の論文
• 1996-02-15

著者

• Tamaru T

  National Aerospace Lab. Tokyo Jpn

• Tamaru Takashi

  Aeroengine Division National Aerospace Laboratory

関連論文

• Evaluation of Thermocouple and Thermal Radiation Instrumentation for Measuring Gas turbine Combustor Liner Wall Temperature
• Research Reviews on Flameholders and Combustion of an Afterburner and a Ramjet Engine

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