Some useful links about ANSYS-Fluent [Always update]

Tutorials

List of the tutorials in this resource:
1.    What's Under the CFD Blackbox?
2.    Big Ideas: Fluid Dynamics
3.    Computational Fluid Dynamics
4.    Laminar Pipe Flow
5.    Turbulent Pipe Flow
6.    Flat Plate Boundary Layer
7.    Supersonic Flow Over a Wedge
8.    Compressible Flow in a Nozzle
9.    Turbulent Forced Convection
10.   Laminar Convection: Nusselt Problem
11.   Steady Flow Past a Cylinder
12.   Unsteady Flow Past a Cylinder
13.   Flow over an Airfoil
14.   3D Transonic Flow over a Wing
15.   Bifurcating Artery
16.   3D Bifurcating Artery
17.   Wind Turbine Blade FSI (Part 1) (Advanced)
18.   Vertical Axis Wind Turbine (Part 1) (Advanced)
19.   Vertical Axis Wind Turbine (Part 2) (Advanced)
20.   Over-expanded Nozzle (Advanced)
21.   3D Convection through an Electronics Box
22.   Sudden Expansion in Laminar Pipe Flow
23.   Turbulent Pipe Flow (LES)
24.   Turbulent Jet (k-epsilon model)
25.   User Defined Functions
26.   Partially Premixed Combustion
27.   Particles in a Periodic Double Shear Layer
28.   Nasal Airway Model

Lectures of Prof. Kent L. Lawrence from University of Texas Arlington 
            List of the tutorials in this resource:
1.     Truss Examples
2.     Plane Stress Examples
3.     Axisymmetric Problems
4.     Three Dimensional Models
5.     Heat Conduction & Axisymmetric Thermal Stress
6.     Beam Examples
7.     Plate Models
8.     Natural Frequency & Normal Mode Calculation
9.     Miscellaneous Topics

Comments

Post a Comment

Popular posts from this blog

Parallel run with Fluent on a HPC cluster

Fluent Fluent is used for computational fluid dynamics (CFD). Fluent Journal Script A Fluent journal script (e.g. " journalfile.jou ") might look like this: file/read-case-data aircraft.cas it 1000 wd "aircraft.dat" Submitting a Batch Fluent Job to Slurm With the correct journal file set up, the final step is to submit this to the Slurm queuing system. #!/bin/sh #SBATCH -n 1 # 1 core #SBATCH -t 1-03:00:00 # 1 day and 3 hours #SBATCH -p compute # parition name #SBATCH -J fluent_batch # sensible name for the job # load the relevant module files. NB: if unsure about # what you need, please contact ops source /etc/profile.d/modules.sh module load apps fluent # run slurm in batch on the allocated node(s) # the '-t4' specifies 4 cores (academic licensing) fluent 2d -g -t4 -i journalfile.jou > outputfile.out The fluent options in the above Slurm script are: 2d the fluent version used -g no graphical environment -i journ
Read more

yPlus utility in OpenFOAM

Image
This post is about how to calculate yPlus in OpenFOAM. For RANS Note that yPlusRAS calculates y* and not y+ 1.      With wall function;   ·         type ‘yPlusRAS’ for incompressible flow ·         type ‘yPlusRAS’ –compressible for compressible flow 2.      Without wall function; ·         type wallShearStress if it is incompressible. If not, add " -compressible " flag ·         calculate manually: sqrt(wallShearStress/rho) * y/nu y = the distance to first cell from the wall nu = kinematic viscosity Be careful: You should use the cell center (height of the cell devided by two) for y For LES type ‘ yPlusLES’ Note: Y-star = rho*Cmu^0.25*sqrt(k)*y/mu y-plus = rho*sqrt(tau_w/rho_w)*y/mu Y-star is related to the turbulent kinetic energy and y-plus to the wall shear stress. Where   is the friction velocity at the nearest wall,   is the distance to the nearest wall and   is the local kinematic viscosity of the fluid.  is often refered to
Read more

wallShearStress in OpenFOAM

Image
The wall shear stress,  , is given by: Where   is the dynamic viscosity,   is the flow velocity parallel to the wall and   is the distance to the wall. The SI unit of wall shear stress is pascal ( ), which is identical to  . The skin friction coefficient,  , is defined by: Where   is the local  wall shear stress ,   is the fluid density and   is the free-stream velocity (usually taken ouside of the boundary layer or at the inlet). Incompressible Flow Laminar In OpenFOAM, wallShearStress usually is in "kinematic pressure", namely in "m2/s2". It doesn't take into account the density of the fluid. So, you should multiply by rho to reach tau. tau = (wallShearStress) * rho or with wallGradU utility   tau = (wallGradU) * mu You can use the Calculator filter in ParaView to multiply the "wallShearStress" field by the density value. Turbulence Compressible Flow You must run "wallShearSress -compressible&qu
Read more