Towards reliable transpiration cooling for rocket combustion chambers through novel methods of uncertainty quantification
- Alternative title
-
In Richtung zuverlässiger Transpirationskühlung für Raketenbrennkammern durch neuartige Methoden der Unsicherheitsquantifizierung
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
RWTH Aachen University, Dissertation, 2024
- Keyword
-
Filmkühlung
Brennkammer
Raketentriebwerk
Unsicherheit
Heißgasturbine
Transpirationskühlung
- Event
-
Veröffentlichung
- (where)
-
Aachen
- (who)
-
Universitätsbibliothek der RWTH Aachen
- (when)
-
2024
- Creator
- Contributor
- DOI
-
10.18154/RWTH-2024-03577
- URN
-
urn:nbn:de:101:1-2405150137111.702795130272
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:41 PM CET
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Steins, Ella Luisa
- Herty, Michael
- Behr, Marek
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2024
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Effective boundary conditions for transpiration cooling applications
Probabilistic constrained Bayesian inversion for transpiration cooling
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A Coupled Two-Domain Approach for Transpiration Cooling
An Effective Model for the Simulation of Transpiration Cooling
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A contribution to transpiration cooling for aerospace applications using CMC walls
Investigation on Heat Transfer in Small Hydrocarbon Rocket Combustion Chambers