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STUDY ON TRANSONIC CASCADE PERFORMANCE BY USE OF NEWLY BUILT FACILITY
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作者 S.Kaji H.Takata +3 位作者 m.hiramoto Y.Machida H.Fujita H.Ito 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1991年第2期104-112,共9页
Progress in computational fluid dynamics in the field of turbomachine cascades has increased recently the importance of the study by cascade wind tunnels to verify various newly introduced concepts. A transonic cascad... Progress in computational fluid dynamics in the field of turbomachine cascades has increased recently the importance of the study by cascade wind tunnels to verify various newly introduced concepts. A transonic cascade wind tunnel test facility has been built for this purpose in the Department of Aeronautics, University of Tokyo. The system and operation of this facility will be explained in detail. The tunnel is of blowdown type, and can be run repeatedly at a short interval. Experimental cascade performances obtained by this facility as well as numerical results for cascades designed along new concepts are discussed. 展开更多
关键词 STUDY ON TRANSONIC CASCADE PERFORMANCE BY USE OF NEWLY BUILT FACILITY Figure
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