Effect of Splitter Angles on Characteristics of Mixing Layer Flow: A Numerical Study

This study investigates the effect of splitter angles on the aerodynamic flow of two free streams under incompressible conditions. The angle of the splitter is changed from 0 to 40° to simulate different wake structures on the slant. The convective Mach number was selected at 0.185. The velocities a...

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Bibliographic Details
Main Authors: Trung Dung Nguyen, Dinh Anh Le, Van Minh Do, Anh Tuan Nguyen, The Hung Tran
Format: Article
Language:English
Published: Shahid Chamran University of Ahvaz 2025-01-01
Series:Journal of Applied and Computational Mechanics
Subjects:
Online Access:https://jacm.scu.ac.ir/article_19112_10d14b560e1947fbd4460087082c42fe.pdf
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