Back to Results
First PageMeta Content
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

Document Date: 2014-12-04 04:51:54


Open Document

File Size: 567,38 KB

Share Result on Facebook
UPDATE