Direct Numerical Simulation of Flow and Heat Transfer in a Compressor Blade Passage Across a Range of Reynolds Numbers

Direct Numerical Simulation of Flow and Heat Transfer in a Compressor Blade Passage Across a Range of Reynolds Numbers

This study employs Direct Numerical Simulation (DNS) to investigate the flow and heat transfer characteristics in a compressor blade passage at five Reynolds numbers (<inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics>&l...

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Bibliographic Details
Main Authors: Yang Liu, Chenchen Zhao, Lei Zhou, Duo Wang, Hongyi Xu
Format: Article
Language:English
Published: MDPI AG 2025-06-01
Series:Aerospace
Subjects:
compressor blade passage
boundary layer
turbulent heat transfer
vortex structure
direct numerical simulation
Reynolds number effect
Online Access:https://www.mdpi.com/2226-4310/12/6/563
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