Transpiration cooling for double-walled jet engine turbine blades

Increasing thermal loads on turbine blades has led to the need for more advanced cooling sys- tems. Transpiration cooling techniques are of renewed interest, partly because of more ad- vanced manufacturing methods, and are characterised by small film-cooling hole sizes, with a high coverage density,...

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Hlavní autor: Courtis, M
Další autoři: Ireland, P
Médium: Diplomová práce
Jazyk:English
Vydáno: 2023
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