Items where Division is "16 Department of Mechanical Engineering > Institute of Gas Turbines and Aerospace Propulsion (GLR) > Rolls-Royce University Technology Center Combustor Turbine Interaction (UTC)" and Year is [pin missing: value2]
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- TU Darmstadt (3)
- 16 Department of Mechanical Engineering (3)
- Institute of Gas Turbines and Aerospace Propulsion (GLR) (3)
- Rolls-Royce University Technology Center Combustor Turbine Interaction (UTC) (3)
- Institute of Gas Turbines and Aerospace Propulsion (GLR) (3)
- 16 Department of Mechanical Engineering (3)
Number of items at this level (without sub-levels): 3.
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Schneider, Marius (2019):
Robust aero-thermal design of high pressure turbines at uncertain exit conditions of low-emission combustion systems.
Darmstadt, [Book]
W
Werschnik, Holger (2017):
Aerodynamic impact of swirling Combustor Inflow on endwall heat transfer and the robustness of the film cooling design in an axial turbine.
Darmstadt, Shaker, ISBN 978-3-8440-5591-7,
[Book]
Wilhelm, Manuel (2020):
Aerothermal Impact of Low Emission Combustion on the Turbine Blade Tip.
In: Forschungsberichte aus dem Institut für Gasturbinen, Luft- und Raumfahrtantriebe, 15, Darmstadt, Shaker, ISBN ISBN 978-3-8440-7482-6,
DOI: 10.25534/tuprints-00011911,
[Book]
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