35th Wind Energy Symposium 2017
DOI: 10.2514/6.2017-2000
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A Computationally-Efficient Panel Code for Unsteady Airfoil Modelling Including Dynamic Stall

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“…Panel methods further improve the blade representation of the lifting surface model by taking airfoil thickness into account when modeling its geometry [166] using singularity elements. These singularity elements can be constant-strength doublets or sources [58]. The strength of the doublets, like the ones used in Figure 5.4, are typically represented as µ, although this strength is equivalent to the circulation over the panel [86], Γ = µ.…”
Section: Blade Aerodynamic Modelsmentioning
confidence: 99%
“…Panel methods further improve the blade representation of the lifting surface model by taking airfoil thickness into account when modeling its geometry [166] using singularity elements. These singularity elements can be constant-strength doublets or sources [58]. The strength of the doublets, like the ones used in Figure 5.4, are typically represented as µ, although this strength is equivalent to the circulation over the panel [86], Γ = µ.…”
Section: Blade Aerodynamic Modelsmentioning
confidence: 99%