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Author:

Jia, Ning (Jia, Ning.) | Jin, Wei (Jin, Wei.) | Wu, Junmei (Wu, Junmei.) | Lei, Jiang (Lei, Jiang.) | Ji, Wentao (Ji, Wentao.)

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Abstract:

Based on NACA airfoil profile and the structure of beveled vortice generator, a novel beveled design of NACA pin-fin and its configuration in the cooling channel of turbine blade were proposed. Numerical simulation was conducted to investigate the flow and heat transfer characteristics of this pin-fin arrays in the cooling channel. The detailed physical field distributions of the flow and heat transfer were discussed and the overall thermal performance was also explored. The result indicated that the bevel cut of the pin-fin can produce lasting and stable longitudinal vortices to strengthen the disturbance of flow field, yielding a good effect on enhancing heat transfer of the cooling channel. © 2021, Editorial Department of Journal of Aerospace Power. All right reserved.

Keyword:

Airfoils Cooling Fins (heat exchange) Heat transfer performance Turbomachine blades Vortex flow

Author Community:

  • [ 1 ] [Jia, Ning]State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 2 ] [Jin, Wei]State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 3 ] [Wu, Junmei]State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 4 ] [Lei, Jiang]State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 5 ] [Ji, Wentao]MOE Key Laboratory of Thermo-Fluid Science and Engineering, School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an; 710049, China

Reprint Author's Address:

  • [Wu, Junmei]State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi'an Jiaotong University, Xi'an; 710049, China;;

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Source :

Journal of Aerospace Power

ISSN: 1000-8055

Year: 2021

Issue: 1

Volume: 36

Page: 61-69

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count: 2

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 11

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