Zobrazeno 1 - 2
of 2
pro vyhledávání: '"Hypersonic Shock Tunnel - Heat Transfer"'
Autor:
C. E. Wittliff
Publikováno v:
18th Thermophysics Conference.
Heat transfer measurements have been made on a 0.0175-scale NASA Space Shuttle orbiter model having a simulated SILTS (Shuttle Infrared Leeside Temperature Sensor) pod on top of the vertical tail. Heat transfer distributions were measured both on the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ba0bb95da79b71b2cb6e961d5ff80f11
https://doi.org/10.2514/6.1983-1535
https://doi.org/10.2514/6.1983-1535
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
