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pro vyhledávání: '"Hypersonic Shock Tunnel - Heat Transfer"'
Autor:
Nagashetty, K
In the flying field of space transportation domain, the increased efforts involving design and development of hypersonic flight for space missions is on toe to provide the optimum aerothermodynamic design data to satisfy mission requirements. Aerothe
Externí odkaz:
http://hdl.handle.net/2005/3195
http://etd.ncsi.iisc.ernet.in/abstracts/4067/G26579-Abs.pdf
http://etd.ncsi.iisc.ernet.in/abstracts/4067/G26579-Abs.pdf
