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Investigation of two-phase flow characteristics of an S-shaped inlet in rain

Shi, Z. Y.; Wu, Z. L.; Tan, H. J.; Yao, Y. F.

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Authors

Z. Y. Shi

Z. L. Wu

H. J. Tan

Yufeng Yao Yufeng.Yao@uwe.ac.uk
Professor in Aerospace Engineering



Abstract

Rain, a common weather hazard for aircraft, is one of major causes of several catastrophic flight accidents. Stealth aircraft commonly employ S-shaped inlets, frequently being subjected to extreme external environmental effects like rain, during mission execution. The present work employs an Eulerian-Lagrangian two-phase flow approach to systematically investigate the effect of rain on the aerodynamic performance of an S-shaped inlet. The Computational Fluid Dynamics (CFD) method is validated by experiments. The results indicate that rainfall intensity, raindrop size distribution, and angle of attack have affected on the aerodynamic performance of the S-shaped inlet. It is found that the stall angle of attack for the inlet aerodynamic performance is 17◦. Smaller-sized raindrops are more likely to form water film on the inner wall surface. Furthermore, the larger the angle of attack, the greater the maximum height of the water film. Larger-sized raindrops are more likely to splash into several secondary droplets, forming ejecta frog near the wall surface. These results are valuable for understanding the influence of rain on the aerodynamic performance of an S-shaped inlet.

Journal Article Type Article
Acceptance Date Jun 17, 2025
Online Publication Date Aug 6, 2025
Publication Date Aug 31, 2025
Deposit Date Aug 19, 2025
Publicly Available Date Aug 20, 2025
Journal Physics of Fluids
Print ISSN 1070-6631
Electronic ISSN 1089-7666
Publisher AIP Publishing
Peer Reviewed Peer Reviewed
Volume 37
Issue 8
Article Number 083324
DOI https://doi.org/10.1063/5.0280200
Public URL https://uwe-repository.worktribe.com/output/14829653

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