Aerodynamics of UH-60 Helicopter-inlet Integration in Ground Effect

This paper describes a comprehensive numerical investigation into the aerodynamic characteristics of a full-scale UH-60 helicopter–inlet integrated flow field under the ground effect. The impact of both the internal and external flow parameters on the coupled flow field is analyzed, and the aerodyna...

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Bibliographic Details

Published in:	Journal of Applied Fluid Mechanics
Main Authors:	S. Yang, S. Sun, Z. Wu, H. Zhou, Y. Liu
Format:	Article
Language:	English
Published:	Isfahan University of Technology 2025-10-01
Subjects:	ground effect engine inlet aerodynamic characteristics helicopter computational fluid dynamics
Online Access:	https://www.jafmonline.net/article_2765_1d945b0ed28af2c7d2dedb2e6efd3804.pdf