A Rapid Method for Heat Transfer Coefficient Prediction on the Icing Surfaces of Aircraft Wings Based on a Partitioned Boundary Layer Integral Model

A Rapid Method for Heat Transfer Coefficient Prediction on the Icing Surfaces of Aircraft Wings Based on a Partitioned Boundary Layer Integral Model

Aircraft wing surface icing compromises flight safety, where accurate calculation of heat transfer coefficient on airfoil surfaces serves as a prerequisite for designing thermal anti-icing systems. However, during icing conditions, ice morphology changes wall roughness and transition properties, mak...

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Bibliographic Details
Main Authors: Liu Wang, Dexin Zhang, Zikang Cheng, Jiaxin Feng, Bo Sun, Jianye Chen, Junlong Xie
Format: Article
Language:English
Published: MDPI AG 2025-07-01
Series:Aerospace
Subjects:
convective heat transfer coefficient
CFD
boundary layer integral method
roughness model
Online Access:https://www.mdpi.com/2226-4310/12/7/634
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