Advanced Thermal Performance of Broken V-Shaped Ribs for Gas Turbine Blade Internal Cooling at High Reynolds Numbers
AIAA SCITECH 2024 Forum
01.01.2024
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
TURBINE BLADE DESIGN AT SMALL REYNOLDS NUMBERS
British Library Conference Proceedings | 2003
|Turbine Blade Internal Cooling System
British Library Conference Proceedings | 1999
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