A Comparative Study of Airfoil Stall Characteristics Based on Detached Eddy Simulation Incorporated with Weighted Essentially Non-Oscillatory Scheme and Weighted Compact Nonlinear Scheme

A Comparative Study of Airfoil Stall Characteristics Based on Detached Eddy Simulation Incorporated with Weighted Essentially Non-Oscillatory Scheme and Weighted Compact Nonlinear Scheme

In this paper, the detached eddy simulation (DES) method is used to calculate the aerodynamic characteristics of NACA0015 airfoil by combining the Riemann approximate solution HLLC (Harten–Lax–van Leer Contact) with the high-order weighted essentially non-oscillatory (WENO) scheme and the weighted c...

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Bibliographic Details
Main Authors: Yan Qi, Bowen Zhong, Song Zou
Format: Article
Language:English
Published: MDPI AG 2024-11-01
Series:Aerospace
Subjects:
detached eddy simulation
WENO scheme
WCNS
numerical dissipation
Online Access:https://www.mdpi.com/2226-4310/11/11/917
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