Control of Trailing Edge Separation with the Use of Circular Endwall Slot in a Highly Loaded Turbine Blade Cascade
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-5990-7_57
Reference8 articles.
1. Hergt A, Meyer R, Engel K (2012) Effects of vortex generator application on the performance of a compressor cascade. J Turbomach 135(2)
2. Tao Z, Guo Z, Song L, Li J (2020) Uncertainty quantification of aero-thermal performance of a blade endwall considering slot geometry deviation and mainstream fluctuation
3. Schreiner BDJ, Wilson M, Li YS, Sangan CM (2020) Effect of purge on the secondary flow-field of a gas turbine blade-row. J Turbomach 142(10)
4. Zhang S, MacManus DG, Luo J (2016) Parametric study of turbine NGV blade lean and vortex design. Chinese J Aeronaut 29(1):104–116
5. Xue X, Wang S, Luo L, Zhou X (2020) The compound bowing design in a highly loaded linear cascade with large turning angle. Proc Inst Mech Eng Part G J Aerosp Eng 234(16):2323–2336
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