Open Access
Issue
JNWPU
Volume 42, Number 2, April 2024
Page(s) 278 - 285
DOI https://doi.org/10.1051/jnwpu/20244220278
Published online 30 May 2024
  1. NEWTON P J, LOCK G D, KRISHNABABU S K, et al. Aero-thermal investigation of tip leakage flow in axial flow turbines: part Ⅲ-tip cooling[J]. Journal of Turbomachinery, 2009, 131(1): 011008 [Article] [CrossRef] [Google Scholar]
  2. YANG H, ACHARYA S, EKKAD S V, et al. Flow and heat transfer predictions for a flattip turbine blade[C]//Turbo Expo: Power for Land, Sea, and Air, 2002: 271–283 [Google Scholar]
  3. AZAD G M, HAN J C, TENG S. Heat transfer and pressure distribution on a gas turbine blade tip[R]. ASME Paper 2000-GT-0194, 2000 [Google Scholar]
  4. DU Kun, SONG Liming, LI Jun. Numerical investigation of turbine blade with grooved tip on the heat transfer performance[J]. Journal of Propulsion Technology, 2014, 35(5): 618–623 [Article] (in Chinese) [Google Scholar]
  5. CHYU M K, MOON H K, METZGER D E. Heat transfer in the tip region of grooved turbine blades[J]. Journal of Turbomachinery, 1989, 111: 131–138 [Article] [CrossRef] [Google Scholar]
  6. NAIK S, GEORGAKIS C, HOFER T, et al. Heat transfer and film cooling of blade tips and endwalls[J]. Journal of Turbomachinery, 2011, 134(4): 041004 [Google Scholar]
  7. JEONG J, KIM W, KWAK J, et al. Heat transfer coefficient and film cooling effectiveness on the partial cavity tip of a gas turbine blade[J]. Journal of Turbomachinery, 2019, 141: 071007 [Article] [CrossRef] [Google Scholar]
  8. KWAK J S, HAN J C. Heat transfer coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade[J]. Journal of Turbomachinery, 2003, 125: 648–657 [Article] [CrossRef] [Google Scholar]
  9. HAN Chang, REN Jing, JIANG Hongde. Multi-parameter influence on film cooling at blade tip[J]. Journal of Engineering Thermophysics, 2012, 33(9): 1501–1504 [Article] (in Chinese) [Google Scholar]
  10. AHN J Y, MHETRAS S, HAN J C. Film cooling effectiveness on a gas turbine blade tip using pressure-sensitive paint[J]. ASME Journal of Heat Transfer, 2005, 127: 521–530 [Article] [CrossRef] [Google Scholar]
  11. HUANG Yan, YAN Xin, HE Kun, et al. Effect of cooling-hole distributions on heat transfer and cooling effectiveness on turbine blade tip[J]. Journal of Xi'an Jiaotong University, 2016, 50(5): 101–107 [Article] (in Chinese) [Google Scholar]
  12. WANG Weijie, LU Shaopeng, MA Haiteng, et al. Cooling and heat transfer characteristics of high-pressure turbine blade with cutback squealer tip[J]. Journaln of Aerospace Power, 2019, 34(10): 2131–2139 [Article] (in Chinese) [Google Scholar]
  13. YANG Beijie, TAN Xiaoming, SHAN Yong, et al. Effects of rib structure on flow and heat transfer characteristics of film cooling rotor blade with squealer tip[J]. Journal of Aerospace Power, 2021, 36(7): 1462–1471 [Article] (in Chinese) [Google Scholar]
  14. YU Jinxing, YE Mingliang, YAN Xin. Investigations on the heat transfer and film cooling effect at squealer tip of a turbine stage under engine conditions[J]. Journal of Xi'an Jiaotong University, 2021, 55(7): 106–116 [Article] (in Chinese) [Google Scholar]
  15. YE Mingliang, YAN Xin, HE Kun. Effect of rib location on heat transfer and cooling effect of a squealer tip in turbine stage[J]. Journal of Xi'an Jiaotong University, 2018, 52(5): 116–124 [Article] (in Chinese) [Google Scholar]
  16. GUO Jiajie, WANG Xinjun, BAO Yuhang. Effects of oval-hole and inclination angle on the flow and heat transfer performance of the turbine blade with squealer tip[J]. Journal of Xi'an Jiaotong University, 2021, 55(1): 153–161 [Article] (in Chinese) [Google Scholar]
  17. Chen Dawei. Film cooling effectiveness of turbine blade surface under the influence of wake[D]. Xi'an: Northwestern Polytechnical University, 2020 (in Chinese) [Google Scholar]
  18. CHEN D W, ZHU H R, LIU C L, et al. Combined effects of unsteady wake and free-stream turbulence on turbine blade film cooling with laid-back fan-shaped holes using psp technique[J]. International Journal of Heat and Mass Transfer, 2019, 133: 382–392 [Article] [CrossRef] [Google Scholar]
  19. MCCLINTOCK F A. Describing uncertainties in single-sample experiments[J]. Mechanical Engineering, 1953, 75(1): 3–8 [Google Scholar]
  20. LI Jia. Experimental and theoretical research on gas turbine film cooling[D]. Beijing: Tsinghua University, 2011 (in Chinese) [Google Scholar]
  21. JOHNSON B E, HU H. Measurement uncertainties analysis in the determination of adiabatic film cooling effectiveness by using pressure sensitive paint(PSP) technique[C]//Fluids Engineering Division Summer Meeting, 2014 [Google Scholar]
  22. NATSUI G, LITTLE Z, KAPAT J S, et al. A detailed uncertainty analysis of adiabatic film cooling effectiveness measurements using pressure-sensitive paint[J]. Journal of Turbomachinery, 2016, 138(8): 081007 [Article] [CrossRef] [Google Scholar]

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