Towards reliable transpiration cooling for rocket combustion chambers through novel methods of uncertainty quantification
In Richtung zuverlässiger Transpirationskühlung für Raketenbrennkammern durch neuartige Methoden der Unsicherheitsquantifizierung
2024
1 Online-Ressource
Theses
Electronic Resource
English
New Experimental Results on Transpiration Cooling for H2/O2 Rocket Combustion Chambers
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