Effect of Large Stagger Angle Endwall on Secondary Losses in a High-Lift Turbine
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-97-3998-1_115
Reference11 articles.
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3. Wood, L.E., Jones, R.R., Pountney, O.J., et al.: A geometry generation framework for contoured endwalls. In: Proceedings of ASME Turbo Expo 2019: Turbine Technical Conference and Exposition. GT2019, p. 90446 (2019)
4. Wei, Z., Qiao, W., Liu, J., et al.: Reduction of endwall secondary flow losses with leading-edge fillet in a highly loaded low-pressure turbine. Proc. IMechE Part A J. Power Energy 230(2), 184–195 (2016)
5. Zess, G.A., Thole, K.A.: Computational design and experimental evaluation of using a leading edge fillet on a gas turbine vane. J. Turbomach. 124, 167–175 (2002)
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