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Author:

He, Juan (He, Juan.) | Deng, Qinghua (Deng, Qinghua.) | Feng, Zhenping (Feng, Zhenping.) (Scholars:丰镇平)

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Abstract:

Film cooling is an effective technique to isolate the heat flux from high-temperature mainstream, but the counter-rotating vortex pair (CRVP) generated by the interaction between film jet and mainstream leads to serious jet-off and poor film coverage. To enhance film cooling performance, a v-shaped protru-sion/dimple vortex generator is arranged at the upstream location of film hole for suppressing the CRVP. The flow and heat transfer characteristics of film cooling with four kinds of vortex generators, v-shaped protrusion vortex generator (VSPVG), v-shaped dimple vortex generator (VSDVG), anti-v-shaped protru-sion vortex generator (AVSPVG) and anti-v-shaped dimple vortex generator (AVSDVG), are investigated in detail over the blowing ratio ranging from 0.5 to 1.5 by solving three dimensional Reynolds-Averaged Navier-Stokes (RANS) equations with Realizable k-epsilon turbulence model. Results indicate that both the v-shaped vortex generators can generate additional anti-counter-rotating vortex pairs (ACRVP) to weaken the CRVP, while both the anti-v-shaped vortex generators will enlarge the CRVP. The arrangement of VSPVG or VSDVG is proved to enhance film cooling performance significantly, especially the VSPVG, which improves the adiabatic film cooling effectiveness by 82.3%, 187.9%, 157.7%, 162.2% and 145.2% re-spectively corresponding to the BR = 0.5, 0.75, 1, 1.25 and 1.5 compared with Baseline case. Considering the total pressure loss, it is found that the enhancement of film cooling effectiveness comes at the cost of slightly increased total pressure loss. In further study, the effect of VSPVG height on film cooling per-formance is also discussed. It is observed that the adiabatic film cooling effectiveness increases with an increase of the height, and the total pressure loss also inescapably increases, but it is worth celebrat-ing that compared with Baseline case, the higher film cooling effectiveness and lower total pressure loss coefficient is obtained when the height is lower than 0.15 D . (c) 2021 Elsevier Ltd. All rights reserved.

Keyword:

Counter-rotating vortex pair Film cooling Total pressure loss Vortex generator

Author Community:

  • [ 1 ] [He, Juan]Xi An Jiao Tong Univ, Inst Turbomachinery, Shaanxi Engn Lab Turbomachinery & Power Equipment, Xian 710049, Peoples R China
  • [ 2 ] [Deng, Qinghua]Xi An Jiao Tong Univ, Inst Turbomachinery, Shaanxi Engn Lab Turbomachinery & Power Equipment, Xian 710049, Peoples R China
  • [ 3 ] [Feng, Zhenping]Xi An Jiao Tong Univ, Inst Turbomachinery, Shaanxi Engn Lab Turbomachinery & Power Equipment, Xian 710049, Peoples R China
  • [ 4 ] [Deng, Qinghua]Beihang Univ, Collaborat Innovat Ctr Adv Aeroengine, Beijing 100191, Peoples R China

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Source :

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER

ISSN: 0017-9310

Year: 2021

Volume: 180

5 . 5 8 4

JCR@2020

ESI Discipline: ENGINEERING;

ESI HC Threshold:30

CAS Journal Grade:2

Cited Count:

WoS CC Cited Count: 3

SCOPUS Cited Count: 21

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 3

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