Quantifying the surface heat transfer on transpiration cooled porous materials in laminar and turbulent hypersonic boundary layers

The design of a transpiration cooled system requires detailed local heat transfer information on and in the vicinity of the porous injector; however, limited spatially resolved experimental studies exist, particularly in hypersonic flows. In this work experiments were conducted on a flat plate model...

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מידע ביבליוגרפי
Main Authors: Naved, I, Hermann, T, Hambidge, C, Ifti, HS, McGilvray, M, Tirichenko, IS, Vandeperre, L
פורמט: Conference item
שפה:English
יצא לאור: ESA Conference Bureau / ATPI Corporate Events 2022

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