Measurement of Velocity and Temperature Profiles at the Exit Plane of a Tubular Gas Turbine Combustor

Material type: 文書・図像類

Author: 田丸, 卓ほか

Publisher: 航空宇宙技術研究所

Publication date: 1989-08

Material Format: Digital

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Note (General)：: Detailed velocity and temperature profile data at the exit plane of a high pressure gas turbine tubular combustor were obtained at atmospheric conditi...

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Material Type: 文書・図像類
Title: Measurement of Velocity and Temperature Profiles at the Exit Plane of a Tubular Gas Turbine Combustor
Author/Editor: 田丸, 卓
下平, 一雄
TAMARU, Takashi
SHIMODAIRA, Kazuo
Author Heading: 田丸, 卓
下平, 一雄
TAMARU, Takashi
SHIMODAIRA, Kazuo
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1989-08
Publication Date (W3CDTF): 1989-08
Alternative Title: ガスタービン筒形燃焼器出口断面での風速および温度分布の測定
Periodical title: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
No. or year of volume/issue: 609
Volume: 609
Pages: 16-
ISSN (Periodical Title): ISSN : 0452-2982
Text Language Code: eng
Target Audience: 一般
Note (General): 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.
資料番号: NALTM0609000
レポート番号: NAL TM-609
Access Restrictions: 限定公開
Periodical Title (NCID): AN00314334
https://ci.nii.ac.jp/ncid/AN00314334
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ