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Date: 2014-12-04 04:51:54Aerospace Fluid dynamics Spacecraft propulsion Wind tunnel Hypersonic speed Sting Aerodynamics Aerospace engineering Space technology | ICMARREALIZATION OF "DOUBLING" METHODS IN AERODYNAMIC EXPERIMENT FOR A MODEL WITH DUCT A.V. Lokotko Khristianovich Institute of Theoretical and Applied Mechanics SB RASAdd to Reading ListSource URL: www.itam.nsc.ruDownload Document from Source WebsiteFile Size: 567,38 KBShare Document on Facebook |