Effect of non-axisymmetric endwall contouring and swirling inlet flow on film cooling performance of turbine endwall
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Published:2024-09
Issue:
Volume:229
Page:125702
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ISSN:0017-9310
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Container-title:International Journal of Heat and Mass Transfer
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language:en
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Short-container-title:International Journal of Heat and Mass Transfer
Author:
Du KunORCID,
Zhang Rongxia,
Jia YihaoORCID,
Liu Cunliang,
Sunden BengtORCID
Reference28 articles.
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2. L.E. Wood, R.R. Jones, O.J. Pountney, A geometry generation framework for contoured endwalls, ASME Paper No. GT2019-90446,2019.
3. M.G. Rose, Non-axisymmetric end wall profiling in the HP NGVs of an axial flow gas turbine, ASME 94-GT-249,1994.
4. Nonaxisymmetric turbine endwall design: Part I−three-dimensional linear design system;Harvey;Turbomach,2000
5. Experimentally verified numerical optimization of a three-dimensional parameterized turbine vane with non-axisymmetric end walls;Nagel;Turbomach,2005
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