Numerical investigation of truncated-root rib on heat transfer performance of internal cooling turbine blades-Reference-Cited by-同舟云学术

Numerical investigation of truncated-root rib on heat transfer performance of internal cooling turbine blades

Published:2021-07 Issue:7 Volume:33 Page:076104
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Dinh C. T.¹^ORCID,Nguyen T. M.²,Vu T. D.³,Park S. G.³,Nguyen Q. H.⁴

Affiliation:

1. Department of Aerospace Engineering, Hanoi University of Science and Technology, No. 1, Dai Co Viet Road, Hai Ba Trung District, Hanoi 100000, Vietnam

2. Department of Fluid Power and Automation Engineering, Hanoi University of Science and Technology, No. 1, Dai Co Viet Road, Hai Ba Trung District, Hanoi 100000, Vietnam

3. Department of Mechanical Engineering and Automotive Engineering, Seoul National University of Science and Technology, No. 232 Gongreung-ro, Nowon-gu, Seoul 01811, South Korea

4. Viettel Aerospace Institute, Viettel Building–Hoa Lac Hi-Tech Park, Hanoi 100000, Vietnam

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0054149

Reference51 articles.

1. Establishment of a long-short-term-memory model to predict film cooling effectiveness under superposition conditions

2. Simulation of air/mist cooling in a conjugate, 3-D gas turbine vane with internal passage and external film cooling

3. Film cooling performance and flow characteristics of internal cooling channels with continuous/truncated ribs

4. Vortex dynamics based analysis of internal crossflow effect on film cooling performance

5. Experimental study and numerical analysis of heat transfer enhancement and turbulent flow over shallowly dimpled channel surfaces

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