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Review

Table 1

Overview of the recent CFD models with static geometry since 2010. Abbreviations: VF = vocal fold, M5/M6 = Scherer’s M5/M6 parametric vocal fold model [13], custom = customized, MRI = Magnetic Resonance Imaging, FvF = False Vocal Folds, full/hemi = full larynx/hemilarynx, VT = vocal tract, ic = incompressible, c = compressible, Ps/Ps(t) = constant/unsteady subglottal pressure at inlet, Pout/Pout (t) = constant/unsteady pressure at oulet, Q/Q(t) = constant/unsteady volume flow rate, FDM = Finite Difference Method, FVM = Finite Volume Method, FEM = Finite Element Method, LES = Large-Eddy-Simulation, WALE = Wall-adaptive Local Eddy (LES) subgrid scale model, RANS = Reynolds Averaged Navier Stokes equations, k – ε = RANS model, na = not available (not provided in the paper). *Only the first author is mentioned.

Study* Year ID Geometry VF & Model FvF Load Num. scheme/fluid model scheme/turb. model
Mihaescu 2010 [31] 3D M5 similar & hemi Q = 27.5 L/min FVM/ic (Smargorinsky-Lilly)
Scherer 2010 [14] 3D M6 & full Ps = 0.29–2.45 kPa (6 constant levels) FVM/ic, laminar
Schwarze 2011 [116] 3D custom & full Experimental U(t) FVM/ic, LES (no model)
Chisari 2011 [32] 2D half cylinders & full x Re = 1000 FDM/ic, laminar
Li 2012 [15] 2D M5 & hemi U = 30.198 m/s FVM/ic, laminar
Farahani 2013 [33] 2D half cylinders & full x Re = 900 FDM/ic, laminar
de Luzan 2015 [11] 3D M5 similar & hemi x Ps = 687 Pa FVM/c & ic
Re = 3600 LES (WALE)
Li 2018 [16] 2D M5 & hemi Ps = ? FVM/ic laminar
Schickhofer 2019 [9] 3D MRI & full + VT x Q(t) model FVM/c LES (WALE)
Schickhofer 2020 [10] 3D MRI & full + VT x Ps = 558.4 Pa FVM/c LES (WALE)
Li 2020 [17] 2D M5 & hemi Ps = ? FVM/ic
laminar
X. Zhang 2020 [18] 3D M5 & full Ps = 500 Pa FVM/ic
RANS (k − ε)
Li 2021 [19] 2D M5 & hemi Ps = ? FVM/ic laminar
de Luzan 2021 [20] 3D M5 & full x Experimental Ps (t) FVM/ic
LES (WALE)

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