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    Title :

    Towards reliable transpiration cooling for rocket combustion chambers through novel methods of uncertainty quantification


    Additional title:

    In Richtung zuverlässiger Transpirationskühlung für Raketenbrennkammern durch neuartige Methoden der Unsicherheitsquantifizierung


    Contributors:


    Publication date :

    2024


    Size :

    1 Online-Ressource


    Remarks:



    Type of media :

    Theses


    Type of material :

    Electronic Resource


    Language :

    English




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