曲面壁上の噴流に対する噴出孔の形状,配列の効果について

Material type: 文書・図像類

Author: 西村, 英明ほか

Publisher: 航空宇宙技術研究所

Publication date: 1971-01

Material Format: Digital

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Note (General)：: To improve the performance of a gas turbine,it is required to raise the turbine inlet temperature;and at the same time the blade should be cooled to m...

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Material Type: 文書・図像類
Title: 曲面壁上の噴流に対する噴出孔の形状,配列の効果について
Author/Editor: 西村, 英明
臼井, 弘
井上, 重雄
三村, 富嗣雄
NISHIMURA, Hideaki
USUI, Hiroshi
INOUE, Shigeo
MIMURA, Fujio
Author Heading: 西村, 英明
臼井, 弘
井上, 重雄
三村, 富嗣雄
NISHIMURA, Hideaki
USUI, Hiroshi
INOUE, Shigeo
MIMURA, Fujio
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1971-01
Publication Date (W3CDTF): 1971-01
Alternative Title: The Effect of Slot Configuration and Arrangement on the Characteristics of Jet Flow
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: 195
Volume: 195
Pages: 13-
ISSN (Periodical Title): ISSN : 0452-2982
Text Language Code: jpn
Target Audience: 一般
Note (General): To improve the performance of a gas turbine,it is required to raise the turbine inlet temperature;and at the same time the blade should be cooled to maintain material properties.Many methods are investigated to cool the turbine blade,for example,internal convection cooling,film cooling,film cooling and transpiration cooling.On the other hand,in order to obtain highly-loaded blades of the compressor,slotted blades are being investigated.Such situations as mentioned above are the same with respect to the aerodynamic behavior.It is,therefore,of interest to know the characteristics of jet flow on an aerofoil surface from the slots.In view of this fundamental situation,the influence of slot configuration and arrangement on the characteristics of jet flow was experimentally investigated,when the jet issued from the slot.
資料番号: NALTM0195000
レポート番号: NAL TM-195
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