school

Formula Sae 2024-2025 Season

For my final year of being on UBC FSAE, I take a step back from design-oriented projects and focus on more research based projects for the season.These projects are all work-in-progress, so I will update this page as the project develops. Check back for updates!

Cornering simulation development

Context

Our team currently doesn't have the capability to simulate the vehicle's aerodynamic behavior during cornering in Star CCM+. Design judges in past competitions have asked us to demonstrate this, but we didn’t have an answer. This is a fundamental issue since the car is cornering more often than not!Not only could we lose points in the design category during competitions, but it also means our design choices lack justification when it comes to cornering performance.



Approach

To tackle this, I’ll be developing our full car simulation template in Star CCM+ to support cornering simulations. The main challenge here is researching, developing, and testing a new template that includes cornering capabilities.This will involve automating steering angles, setting up complex domain boundary conditions, adjusting meshing controls, and plenty of trial and error!


Using Linux computational cluster

Our design team has access to UBC's Sockeye Supercomputer, which is a huge help in this research process. Sockeye allows us to reduce computational time by around 10 times!

project goal

My goal is to allow users to simulate the full car with any aerodynamic package configuration and generate a map of varying Cd and Cl values at different yaw angles during cornering.Once we have this cornering data, I’ll integrate it into our internally developed MATLAB lap time simulation for a more accurate lap time prediction. This will enable us to thoroughly evaluate and justify our design choices by comparing performance across various designs with different cornering maps.


Surface oil flow visibility development

The second project I am working on this year is the development of Surface Oil Flow Visibility procedures for our team.


Context

Validation is essential to complement CFD, but since we lack access to large wind tunnels for full scale testing, we have to get creative!One approach is to use Surface Oil Flow Visibility (SOFV), a custom mix of bright pigment and oil. There isn’t an off-the-shelf product available, so teams often develop their own. The previous year tried, but failed. In the image below, you can see one of our mixtures, which dried too quickly.Getting the right mixture involves a lot of testing and trial and error!


approach

To develop this, I plan to use UBC's Parkinson Wind Tunnel to replicate our running speeds during test days. I'll create an arbitrary aerodynamic shape with a carbon fiber surface finish that mimics our competition vehicle. This will be tested in the wind tunnel with various SOFV mixtures to determine the most suitable one.As a complementary validation exercise, I'll simulate the same wind tunnel in CFD and compare the flow patterns revealed by the SOFV mixture with those from Star CCM+.We have acquired kerosene and titanium dioxide which will be used to conduct our SOFV tests.

Star CCM+

Below are some miscallaneous images that show me going through the process of developing the mesh. I go through steps of prism layer refinement, wake refinement, and domain surface controls.The final mesh wasn't 100% satisfactory, but was good enough to use as a starting point. I set up y+ surface monitors so that once the simulation was complete, I can go back and check whether or not the target y+ of 1 is met on all surfaces, and use that to reiterate.Note: I later ran the simulation and had some results which were not satisfactory, I am working on improving these simulations and will provide some nice photos when ready!


Wind Tunnel

UBC's wind tunnel allows us to run at speeds of 20m/s, which is the same speed at which all our simulations are conducted at.The speed is callibrated through a Betz Micromanometer which is used to find the pressure differential between the test section, and upstream section.

Wind tunnel Callibration

The load cells must be callibrated prior to use. We use a standard set of weights to measure the voltage, and find the slope of the relationship between weight and voltage. This is then entered into DASYLab to calculate lift and drag values.

Manufacturing

Included below are some of the photos I took over the course of October-November detailing the manufacturing process. As you can see, the manufacturing process is concluded. That means I am currently working on testing and will update once those results are ready! Stay tuned.

project goal

Once developed, we can use SOFV during test days to observe real-world airflow behavior and, hopefully, enhance the accuracy of our CFD simulations.


Questions?

If you would like to discuss the technical details of these projects before I find time to update this page, please reach out to me!

Thanks for reading!