국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Measurement of Velocity and Temperature Profiles at the Exit Plane of a Tubular Gas Turbine Combustor
저자	Takashi TAMARU, Kazuo SHIMODAIRA
Keyword
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00609.pdf?id=NALTM0000609
보고서번호	NAL TM-609
발행년도	1989.8
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	Detailed velocity and temperature profile data at the exit plane of a high pressure gas turbine tubular combustor were obtained at atmospheric conditions. Such data are very requisite for designing a high performance turbine, but there is no data presently available that takes into account the combustor characteristics. Measurements were made under atmospheric conditions but were adjusted to have the same Mach number at the exit plane as under design conditions, which were a pressure of 55 atm and a temperature of 1600K. The resultant temperature profiles were compared with those data obtained in the high pressure combustion test.