TAGGED: airfoil, turbulence-model, y-plus
-
-
October 31, 2021 at 8:29 pmjanetjSubscriber
Hello everyone,
I am working on two element airfoil with a trailing edge flap at 25 degree. I have done quad structured meshing. I have some questions regarding that.
My Y-plus value is 7 when I am using Spalart Allmaras model with Reynolds number of 200,000. (Density 1.225 kg/m3, Chord Length 1m, Viscosity 1.7894e-5, Velocity 2.92 m/s). Looking at the mesh and model, is my Y-plus value of 7 okay for S-A turbulence model? What should be the the minimum or maximum Y-plus value?
Secondly, when I use K-epsilon (2 equation) model with Realizable K-Epsilon Model and Scalable Wall Function, my Y-plus reaches nearly 16. I am getting lower Cd and higher Cl using this model as compare to Spalart Allmaras. I know that Scalable Wall Function increases the Y-plus above 15. My question is, is it okay to use Realizable K-Epsilon Model with Scalable Wall Function for Airfoil?
November 1, 2021 at 5:49 pmKalyan GoparajuAnsys EmployeeHello,
In Ansys Fluent, the Spalart-Allmaras model has a y+ insensitive wall treatment. On intermediate grids, 1I would recommend using the Realizable K-epsilon model with Enhanced Wall Treatment. This is a y+ insensitive wall treatment and will automatically adjust based on the local y+.
Thanks,
Kalyan
November 3, 2021 at 9:59 pmjanetjSubscriberDear Kalyan I am still not getting a lower Cd after using the Realizable K-epsilon model with Enhanced Wall Treatment.What could possibly be wrong? My airfoil is a high-lift one (Selig1223) and with the flap, the idea is the get an increased Cl with nominal increase in Cd. But I am getting a Cl of 1.8, whereas Cd is 0.12 and the Cl/Cd is 14.66 at 0 degree alpha which is quite low.
November 4, 2021 at 12:26 pmRobForum ModeratorCan you check the forces are correct? Cd and Cl are coefficients so if the forces are as expected check you're using the correct reference areas etc
November 4, 2021 at 2:32 pmKalyan GoparajuAnsys EmployeeHello,
A couple of things
do you have any validation for the numbers that you are getting? experimental or theoretical?
are both Cl and Cd wrong or is it only the Cd? Drag is notorious for being strongly dependent on the mesh. is your mesh fine enough to capture all the relevant physics? Boundary layers, separation (if any), gap between the elements etc.
As my colleague suggested, please also check if you are using the correct reference quantities.
Thanks Kalyan
Viewing 4 reply threads- The topic ‘Y plus value for Airfoil and Turbulence model’ is closed to new replies.
Ansys Innovation SpaceTrending discussions- How do I get my hands on Ansys Rocky DEM
- Non-Intersected faces found for matching interface periodic-walls
- Unburnt Hydrocarbons contour in ANSYS FORTE for sector mesh
- Fluent fails with Intel MPI protocol on 2 nodes
- Help: About the expression of turbulent viscosity in Realizable k-e model
- Cyclone (Stairmand) simulation using RSM
- Mass Conservation Issue in Methane Pyrolysis Shock Tube Simulation
- Script Error
- convergence issue for transonic flow
- Facing trouble regarding setting up boundary conditions for SOEC Modeling
Top Contributors-
1487
-
599
-
591
-
591
-
366
Top Rated Tags© 2025 Copyright ANSYS, Inc. All rights reserved.
Ansys does not support the usage of unauthorized Ansys software. Please visit www.ansys.com to obtain an official distribution.
-