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Document type:
Dissertation / Thesis
Title:
On Aerothermal Effects of Film Cooling on Turbine Blades with Flow Separation
Advisor:
Niehuis, Reinhard
Referee:
Pfitzner, Michael; Hennecke, Dietmar
Submission date:
11.03.2010
Date oral examination:
25.06.2010
Place of publication:
München
Publisher:
Dr. Hut
Year:
2010
Pages (Book):
174
Language:
Englisch
Keywords:
Effects of Film Cooling on Turbine Blades
Abstract:
The high pressure turbine of jet engines or stationary gas turbines is set under high thermal stress and efficient cooling techniques have to be used in order to prevent the metallic parts from serious damage.
ISBN:
978-3-86853-600-3
Department:
Fakultät für Luft- und Raumfahrttechnik
Institute:
LRT 12 - Institut für Strahlantriebe
Chair:
Niehuis, Reinhard
Open Access yes or no?:
Nein / No
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