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

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...

Полное описание

Библиографические подробности
Главные авторы:	Naved, I, Hermann, T, Hambidge, C, Ifti, HS, McGilvray, M, Tirichenko, IS, Vandeperre, L
Формат:	Conference item
Язык:	English
Опубликовано:	ESA Conference Bureau / ATPI Corporate Events 2022

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