Numerical conjugate flow and heat transfer investigation of a transonic convection-cooled turbine guide vane with stress-adapted thicknesses of different thermal barrier coatings
38th Aerospace Sciences Meeting and Exhibit ; 2000 ; Reno , NV , U.S.A.
2000-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2000
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|Conjugate Heat Transfer Analysis of a Cooled Turbine Vane Using the V2F Turbulence Model
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