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...

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Bibliographic Details
Main Authors: Leontiev Alexander, Popovich Sergey, Strongin Mark, Vinogradov Yurii
Format: Article
Language:English
Published: EDP Sciences 2017-01-01
Series:EPJ Web of Conferences
Online Access:https://doi.org/10.1051/epjconf/201715900030

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