<--- Back to Details
First PageDocument Content
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

Add to Reading List

Source URL: www.itam.nsc.ru

Download Document from Source Website

File Size: 567,38 KB

Share Document on Facebook

Similar Documents