Experimental investigation of turbulent flow in a two-pass channel with different U-shaped bends
Author:
Affiliation:
1. National Key Laboratory of Science and Technology on Aero-Engines Aero-Thermodynamics, Beihang University, Beijing 100191, China
2. Research Institute of Aero-Engine, Beihang University, Beijing 100191, China
Funder
National Science and Technology Major Project
Fundamental Research Funds for the Central Universities
National Natural Science Foundation of China
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0011444
Reference47 articles.
1. Heat transfer and flow characteristics of U-shaped cooling channels with novel wavy ribs under stationary and rotating conditions
2. A numerical investigation of flow and heat transfer in rotating U-shaped square ducts
3. Computation of flow and heat transfer in rotating two-pass rectangular channels (AR=1:1, 1:2, and 1:4) with smooth walls by a Reynolds stress turbulence model
4. Flow and heat transfer in a rotating U-bend with 45° ribs
5. Experimental analysis of turbulent flow structure in a fully developed rib-roughened rectangular channel with PIV
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