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Aerospace / Fluid dynamics / Spacecraft propulsion / Wind tunnel / Hypersonic speed / Sting / Aerodynamics / Aerospace engineering / Space technology
Date: 2014-12-04 04:51:54
Aerospace
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 RAS

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