Experimental Investigation of the Effect of Nozzle Shape and Test Section Perforation on the Stationary and Non-stationary Characteristics of Flow Field in the Large Transonic TsAGI T-128 Wind Tunnel
Proceedings, Aerospace aerodynamics research conference ; 2004 ; London
2004-01-01
Paper 5
Shelved in Conference Index.; Held on CD-ROM
Conference paper
English
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Some Peculiarities of Balance Tests in the Transonic TsAGI T-128 Wind Tunnel
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