Improved Turbine Vane Endwall Film Cooling by Using Sand-Dune-Inspired Design

ZHOU Wenwu, SHAO Hongyi, QENAWY Mohamed, PENG Di, HU Hui, LIU Yingzheng

Journal of Thermal Science ›› 2022, Vol. 31 ›› Issue (3) : 958-973.

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Journal of Thermal Science ›› 2022, Vol. 31 ›› Issue (3) : 958-973. DOI: 10.1007/s11630-022-1638-1  CSTR: 32141.14.JTS-022-1638-1
Aerothermodynamics

Improved Turbine Vane Endwall Film Cooling by Using Sand-Dune-Inspired Design

  • ZHOU Wenwu1,2, SHAO Hongyi1,2, QENAWY Mohamed1,2, PENG Di1,2, HU Hui3, LIU Yingzheng1,2*
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Abstract

As continuous of the previous sand-dune-inspired design, the Barchan-Dune-Shaped Injection Compound (BDSIC)’s film cooling performance at the endwall region was further investigated both experimentally and numerically. While the public 777-shaped hole was served as a baseline, the BDSIC’s endwall effectiveness was assessed at various blowing ratios. Experiments were performed in a single-passage transonic wind tunnel using pressure-sensitive paint (PSP) technique. Carbon dioxide was used as coolant with density ratio of DR=1.53. The purge slot’s blowing ratio was fixed at M=0.3, but the coolant holes were adjusted within M= 0.5–2.0. The measured experimental results indicate that the film distribution at the endwall is strongly affected by the passage flow structures. The BDSIC holes demonstrate much higher film effectiveness than the 777-shaped holes for all blowing ratios, ~30% enhancement for regionally averaged effectiveness at M=1.0 and ~26% at M=2.0. As shown by the numerical results, the existence of BDSIC reduced the coolant penetration effect at a higher blowing ratio. Coolant was deflected and its momentum increased in the streamwise direction, therefore providing more robust film coverage over the endwall region. The anti-counter-rotating vortex pair induced by the BDSIC further stabilized the coolant film and increased the coolant spreading downstream.

Key words

endwall film cooling / pressure-sensitive paint / Barchan dune / 777-shaped hole / counter-rotating vortex

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ZHOU Wenwu, SHAO Hongyi, QENAWY Mohamed, PENG Di, HU Hui, LIU Yingzheng. Improved Turbine Vane Endwall Film Cooling by Using Sand-Dune-Inspired Design[J]. Journal of Thermal Science, 2022, 31(3): 958-973 https://doi.org/10.1007/s11630-022-1638-1

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Funding

The authors appreciate for the funding supports from the NSFC (92052107, 51806138).

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Science Press, Institute of Engineering Thermophysics, CAS and Springer-Verlag GmbH Germany, part of Springer Nature 2022
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