並列タイトル等The Effect of Slot Configuration and Arrangement on the Characteristics of Jet Flow
タイトル（掲載誌）航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
一般注記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
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43779&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース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