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Author:

Gao, Tieyu (Gao, Tieyu.) | Zhu, Jiangnan (Zhu, Jiangnan.) | Li, Jun (Li, Jun.) | Xia, Qingfeng (Xia, Qingfeng.)

Indexed by:

SCIE Scopus

Abstract:

Strong secondary flow generated by ribbed channel and U-shaped bend is the key for forced convection performance and energy dissipation in U-shaped cooling passage. This investigation studies the coupling of nine different rib orientation and the 180-degree bend on overall friction loss and forced convection in the U-shaped passage by ANSYS CFX commercial CFD package when Re=30000. The comprehensive evolution of secondary flow is visualized by vortex core method and colored by turbulence kinetic energy. The qualitative results show that the Nu ratio and overall pressure loss in the downstream passage (Passage 2) is highly affected by the upstream geometry. The N-type rib orientation in Passage 1 delivers more disturbance energy into Passage 2 where P-type rib orientation can reduce the momentum loss of the upstream secondary flows and pressure loss. Based on the understanding of interaction of secondary flow near the bend, modified bend geometry is proposed with 9% thermal performance gain over the existent optimized rib orientation. This investigation suggests vortex core method is a promising visualization tool for the flow control and optimization in U-shaped cooling channel with angled ribs.

Keyword:

Blade cooling rib orientation secondary flow two-pass channel U-shaped bend vortex core

Author Community:

  • [ 1 ] [Gao, Tieyu; Li, Jun] Xi An Jiao Tong Univ, Sch Energy & Power Engn, Inst Turbomachinery, Xian, Shaanxi, Peoples R China
  • [ 2 ] [Zhu, Jiangnan] Aeroengine Acad China, Basic & Appl Res Ctr, Beijing, Peoples R China
  • [ 3 ] [Xia, Qingfeng] Univ Oxford, Dept Engn Sci, Onsey Thermofluids Lab, Oxford, England
  • [ 4 ] [Gao, Tieyu]Xi An Jiao Tong Univ, Sch Energy & Power Engn, Inst Turbomachinery, Xian, Shaanxi, Peoples R China
  • [ 5 ] [Li, Jun]Xi An Jiao Tong Univ, Sch Energy & Power Engn, Inst Turbomachinery, Xian, Shaanxi, Peoples R China
  • [ 6 ] [Zhu, Jiangnan]Aeroengine Acad China, Basic & Appl Res Ctr, Beijing, Peoples R China
  • [ 7 ] [Xia, Qingfeng]Univ Oxford, Dept Engn Sci, Onsey Thermofluids Lab, Oxford, England

Reprint Author's Address:

  • Univ Oxford, Dept Engn Sci, Onsey Thermofluids Lab, Oxford, England.

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Source :

ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS

ISSN: 1994-2060

Year: 2018

Issue: 1

Volume: 12

Page: 117-136

2 . 1 6 3

JCR@2018

8 . 3 9 1

JCR@2020

ESI Discipline: ENGINEERING;

ESI HC Threshold:108

JCR Journal Grade:3

CAS Journal Grade:3

Cited Count:

WoS CC Cited Count: 7

SCOPUS Cited Count: 11

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 3

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