Description and constructional details of facility which by exchanging part of test section can be employed as high speed annular cascade wind tunnel and transonic axial flow test compressor; specifications for two installations are given. (In Japanese with English abstract)
High speed annular cascade wind tunnel and transonic axial flow test compressor
Tokyo. Univ -- Inst Space Aeronautical Science -- Bul
1965
19 pages
Article (Journal)
Japanese
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