Numerical simulation of turbine 'hot spot' alleviation using film cooling
- 1 May 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 9 (3) , 329-336
- https://doi.org/10.2514/3.23626
Abstract
No abstract availableKeywords
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