Direct simulations of trailing-edge noise generation from two-dimensional airfoils at low Reynolds numbers

2012 ◽  
Vol 331 (3) ◽  
pp. 556-574 ◽  
Author(s):  
Tomoaki Ikeda ◽  
Takashi Atobe ◽  
Shohei Takagi
Keyword(s):  
Reynolds Numbers ◽  
Noise Generation ◽  
Two Dimensional ◽  
Trailing Edge ◽  
Low Reynolds Numbers ◽  
Trailing Edge Noise ◽  
Low Reynolds

Aerodynamic Effects of Trailing Edge Serrations at Low Reynolds Numbers

2022 ◽  
Author(s):  
Israel Bron Simplicio ◽  
Giovanni F. Nino ◽  
Robert Breidenthal
Keyword(s):  
Reynolds Numbers ◽  
Trailing Edge ◽  
Low Reynolds Numbers ◽  
Low Reynolds ◽  
Trailing Edge Serrations

Vortex-induced rotations of a rigid square cylinder at low Reynolds numbers

2017 ◽  
Vol 813 ◽  
pp. 482-507 ◽  
Author(s):  
Sungmin Ryu ◽  
Gianluca Iaccarino
Keyword(s):  
Cross Flow ◽  
Reynolds Numbers ◽  
Dynamic Responses ◽  
Two Dimensional ◽  
Square Cylinder ◽  
Low Reynolds Numbers ◽  
Pressure Distributions ◽  
Low Reynolds ◽  
Drag And Lift ◽  
Vortex Patterns

A numerical investigation of vortex-induced rotations (VIRs) of a rigid square cylinder, which is free to rotate in the azimuthal direction in a two-dimensional uniform cross-flow, is presented. Two-dimensional simulations are performed in a range of Reynolds numbers between 45 and 150 with a fixed mass and moment of inertia of the cylinder. The parametric investigation reveals six different dynamic responses of the square cylinder (expanding on those reported by Zaki et al. (J. Fluids Struct., vol. 8, 1994, pp. 555–582)) and their coupled vortex patterns at low Reynolds numbers. In each characteristic regime, moment generating mechanisms are elucidated with investigations of instantaneous flow fields and surface pressure distributions at chosen time instants in a period of rotation response. Our simulation results also elucidate that VIRs significantly influence the statistics of drag and lift force coefficients: (i) the onset of a rapid increases of the two coefficients at $Re=80$ and (ii) their step increases in the autorotation regime.

Two Dimensional RANS Analysis of NACA0012 Airfoil at Low Reynolds numbers

2019 ◽  
Vol 2019.57 (0) ◽  
pp. 515
Author(s):  
Yuki INOUE ◽  
Yasunori NAGATA ◽  
Toshinori KOUCHI ◽  
Shinichiro YANASE
Keyword(s):  
Reynolds Numbers ◽  
Two Dimensional ◽  
Low Reynolds Numbers ◽  
Naca0012 Airfoil ◽  
Low Reynolds ◽  
Rans Analysis
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