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ETH Zurich
Aerothermal Effects of High-Pressure Turbine Rim Seals and Blade Tip Geometries in the Presence of Cooling Flows
Degree
thesis:*- Grantor dc:publisher
- ETH Zurich
- Year dc:date
- 2019
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Schädler, Rainer
- Contributors dc:contributor
-
- Abhari, Reza S.
- di Mare, Francesca
- Kalfas, Anestis I.
Subjects
dc:subject × 3- Turbomachinery; Experimental Flow Physics; fast response aerodynamic probes; High-pressure turbine; rim seal; Blade Tip; Rim Seal Purge Flow; Cavity heat transfer; Computational fluid dynamics (CFD); Non-synchronous Pressure Perturbations and Cavity Modes
- info:eu-repo/classification/ddc/620
- Engineering & allied operations
Rights
dc:rights- Statement dc:rights
-
- info:eu-repo/semantics/openAccess
- In Copyright - Non-Commercial Use Permitted
- Language dc:language
- en
Identifiers
dc:identifier.*- Identifier
- https://doi.org/10.3929/ethz-b-000395420
- OAI identifier oai:identifier
- oai:www.research-collection.ethz.ch:20.500.11850/395420