Experimental Investigation of Rotor Tip Film Cooling at an Axial Turbine with Swirling Inflow Using Pressure Sensitive Paint
- Sprache
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Englisch
- Identifier
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1236694635
Beteiligte Personen und Organisationen
- DOI
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10.26083/tuprints-00019089
- URN
- Rechteinformation
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Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
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26.01.2023, 13:57 MEZ
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