All Courses
All Courses
Courses by Software
Courses by Semester
Courses by Domain
Tool-focused Courses
Machine learning
POPULAR COURSES
Success Stories
In this challenge we are supposed to simulate the mixing of air, in a mixing tee of different lengths, air entering the system has different temperatures and momentum ratios. We are to observe the changes in temperature at the outlet, how it is affected by these parameters. Also, we need to notice the changes when we use…
Aditya Iyer
updated on 25 Feb 2021
In this challenge we are supposed to simulate the mixing of air, in a mixing tee of different lengths, air entering the system has different temperatures and momentum ratios. We are to observe the changes in temperature at the outlet, how it is affected by these parameters.
Also, we need to notice the changes when we use different turbulent models, in this case, k-epsilon and k-omega SST.
Here below are the pictures of the mesh, mesh metrics, residuals, and simulation results for different cases.
SHORT TEE:
LONG TEE:
The pictures above show the mesh which had been used for simulation, it's evident that the mesh is an unstructured mesh with tetrahedral elements, the size of the mesh used here for both cases is 2mm, for faster mesh generation and convergence in results. The other mesh settings were left at default, only changes in mesh quality were made. Corresponding name selections were also made namely the inlet, outlet, and walls.
The mesh metric for both cases is uploaded here:
SHORT TEE:
LONG TEE:
As we can evidently see the mesh quality is well above 5% for both cases hence the mesh can be used for simulation.
The cases for simulations with elements and nodes are provided in the table.
INLET VELOCITY | ELEMENTS | NODES | TEMPERATURE | |
LONG TEE | 6 M/S AND 12 M/S | 139627 | 28201 |
At hot inlet: 36 At cold inlet:19 |
SHORT TEE | 6 M/S AND 12 M/S | 105857 | 21330 |
At hot inlet: 36 At cold inlet:19 |
Post the meshing we proceed towards setting up the different aspects of the simulation in fluent, the following setup was followed:
1. Pressure solver ( Speeds are low, compressibility effects can be neglected)
2. Turbulence models: k- epsilon & k-omega SST.
3. Energy equation turned on to get the temperature.
4. Materials in simulation specified as air, with standard properties.
5. The inlets are velocity inlets, with outlets as pressure outlets with gauge pressure zero.
6. Residuals are set to 1e-3 to 1e-4.
7. Create report definitions with a temperature average distribution at the outlet ( Surface weighted average).
8. Hybrid initialization with 250 iterations to be run.
The residuals for the different cases are shown below:
LONG TEE MOMENTUM RATIO 2
LONG TEE MOMENTUM RATIO 4
SHORT TEE MOMENTUM RATIO 2
SHORT TEE MOMENTUM RATIO 4
The different simulation cases with the number of iterations for convergence is shown below:
MOMENTUM RATIO | ITERATION FOR CONVERGENCE | |
LONG TEE | 2 | 175 |
LONG TEE | 4 | 135 |
SHORT TEE | 2 | 160 |
SHORT TEE | 4 | 160 |
The condition for convergence observed here is that the plot shows the same trend.
The plots obtained, i.e the average temperature distribution at the outlet for the simulated cases are:
LONG TEE MOMENTUM 2:
LONG TEE MOMENTUM 4:
SHORT TEE MOMENTUM 2:
SHORT TEE MOMENTUM 4:
The average temperature and deviations can be inferred as:
AVERAGE TEMPERATURE DISTRIBUTION | STANDARD DEVIATIONS | |
LONG TEE (M-2) |
30.388 |
1.181 |
SHORT TEE (M-2) | 30.52 | 1.773 |
LONG TEE (M-4) | 27.49 | 0.646 |
SHORT TEE (M-4) | 27.586 | 1.5229 |
The temperature contours for the different cases are shown as below:
LONG TEE (M-2)
LONG TEE (M-4)
SHORT TEE (M-2)
SHORT TEE (M-4)
CONCLUSIONS:
1. It is very evident from the plots, data, and contours that lower average temperatures are achieved when the momentum ratio is higher, i.e higher velocity of the cold inlet will result in lower average temperatures.
2. Momentum ratios do not play a vital role in the uniformity of the outlet temperature distribution.
3. The length of the tee does not affect the average temperature at the outlet, but yes we do observe that the standard deviation in temperature for a shorter tee is higher, irrespective of the momentum ratio, i.e temperature distribution at the outlet is not uniform, for the shorter tee.
4. Regarding the turbulence models k-epsilon is preferred due to two reasons:
a. It is evident from contours that the mixing occurs away from the walls, hence k-epsilon gives better results reason being k-omega SST gives better results for interactions at the walls or close to them.
b. On performing simulations with k-omega & epsilon it was noticed that epsilon has lower standard deviation in temperature, hence preferred.
Leave a comment
Thanks for choosing to leave a comment. Please keep in mind that all the comments are moderated as per our comment policy, and your email will not be published for privacy reasons. Please leave a personal & meaningful conversation.
Other comments...
Week 3 - Adiabatic Flame Temperature calculation
AIM: To use Python and the Cantera library to understand the factors affecting the adiabatic flame temperature. OBJECTIVE: To write a Python script to see the variance of equivalence ratio and adiabatic flame temperature. Using the Cantera library to do the same and observe the differences. Varying the heat…
01 Jul 2023 04:43 PM IST
Week 9 - FVM Literature Review
Aim:- To discuss different types of Interpolation schemes and Flux Limiters used infinite volume method.Interpolation Schemes in Finite Volume Method:-1. Upwind Interpolation Scheme(UDS)2. Central Differencing Schemes(CDS)3. Quadratic Upwind Differencing Scheme(QUICK)4. Hybrid Interpolation Scheme(HIS)5. Total Variation…
26 Sep 2021 03:30 PM IST
Week 8 - Simulation of a backward facing step in OpenFOAM
Aim:-The aim of this project is to create the geometry for incompressible cavity flowproblem in OpenFOAM and also to simulate the flow through a backward facing step fordifferent grading factor using icoFOAM solver.OpenFOAM code:-● BlockMeshDict File:-In the following code we have created the required geometryfor grading…
26 Sep 2021 03:15 PM IST
Week 7 - Simulation of a 1D Super-sonic nozzle flow simulation using Macormack Method
Aim:- Simulation of a 1D Super-sonic nozzle flow using Macormack Method forconservative form as well as for non-conservative form.Discretization:-The process of converting the PDE equation into algebric equation isbasically discretization.Now, here in this step, we will use the Mccormack method to solve it.Boundary conditions:-…
26 Sep 2021 03:05 PM IST
Related Courses
0 Hours of Content
Skill-Lync offers industry relevant advanced engineering courses for engineering students by partnering with industry experts.
© 2025 Skill-Lync Inc. All Rights Reserved.