Return to search

Transpiration Cooling Analysis Including Binary Diffusion Using 2-D Navier-Stokes Equations At Hypersonic Mach Numbers

No description available.
Identiferoai:union.ndltd.org:IISc/oai:etd.ncsi.iisc.ernet.in:2005/1767
Date06 1900
CreatorsRavi, B R
ContributorsReddy, K P J, Reddy, N M
Source SetsIndia Institute of Science
Languageen_US
Detected LanguageEnglish
TypeThesis
RelationG14701

Page generated in 0.0015 seconds