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Correlation between aerodynamic forces and vortex dynamics of a NACA0012 wing section in compressible dynamic stall via IDDES | Synapse
March 3, 2026
Correlation between aerodynamic forces and vortex dynamics of a NACA0012 wing section in compressible dynamic stall via IDDES
DM
Dechuan Ma
GL
Gaohua Li
Shanghai Jiao Tong University
JL
Jiahao Liu
Shanghai Maritime University
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Puntos clave
Dynamic stall significantly alters aerodynamic forces acting on the NACA0012 wing section, elevating lift and drag fluctuations.
Using implicit detached-eddy simulation (IDDES) reveals intricate vortex dynamics affecting airflow behavior near the wing.
Numerical simulations demonstrate how compressible flow affects lift during dynamic stall, with implications for aircraft design.
Understanding these interactions may enable improved performance predictions for aircraft under various flight conditions.
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Ma et al. (Thu,) studied this question.
synapsesocial.com/papers/69a767cdbadf0bb9e87e2642
https://doi.org/https://doi.org/10.1016/j.ast.2026.111843