Adiabatic wall temperature and heat transfer coefficient influenced by separated supersonic flow
Investigations of supersonic air flow around plane surface behind a rib perpendicular to the flow direction are performed. Research was carried out for free stream Mach number 2.25 and turbulent flow regime - Rex>2·107. Rib height was varied in range from 2 to 8 mm while boundary layer thickness...
Main Authors: | Leontiev Alexander, Popovich Sergey, Strongin Mark, Vinogradov Yurii |
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Format: | Article |
Language: | English |
Published: |
EDP Sciences
2017-01-01
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Series: | EPJ Web of Conferences |
Online Access: | https://doi.org/10.1051/epjconf/201715900030 |
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