In 2013, the Hyperloop concept was introduced as a revolutionary fifth mode of transportation in the paper, "Hyperloop Alpha." The concept involves a magnetically levitated pod propelled by electromagnetic forces, designed to transport passengers and cargo at speeds of up to 760 mph through a near-vacuum tube. The aerodynamics subteam intends to design a faring to maximize the aerodynamic efficiency and accessibility of open-air components. Using Ansys Fluent and SolidWorks Fluid Simulations, we have optimized both the side and top profiles of the pod. The profiles on the right were optimized using nozzle refining techniques and wind tunnel testing.
After the reinstatement of the aerodynamic structures subteam after 3 years of absence, the current team was starved of the valuable resource of experience. We had to start from scratch, drafting out our own set of design goals, system timeline, and subteam structure. The timeline on the right showcases the design, testing, and manufacturing of our HX 10 pod throughout the year.
Following the CFD analysis, a scaled model of the fairing was fabricated with XPS foam using CNC machining for wind tunnel testing. These tests provided real-world validation of the simulated results since a perfect CFD analysis doesn't take into account shifting. Overall, we calculated a small drag coefficient of 0.22, which validated our fluid simulation results.
Prototype fairing undergoing wind tunnel testing at 45 mph airflow.
Internal vectorized velocity flow for the full pod.
X-direction velocity pathlines of our 2.5 meter model at 60 mph.
The final fairing design incorporated a 2.5-meter aerodynamic shell constructed from carbon fiber composites on a male mold. The optimized layup process ensured both strength and lightweight properties, with a refined aerodynamic profile that maximized the pod efficiency and minimized the drag coefficient. The cutout for the I-beam also serves as a strategic cooling solution, bringing in cold air through the gaps between the I-beam and the fairing
For the male plug, we used Fusion 360 manufacturing software to generate G-code for a foam CNC machine. Then, 32 layers were cut out for our desired fairing shape. The specific carbon fiber used is 12k 2x2 twill high-density CF.
The final step was the integration of the fairing onto the pod. In combination with the statics subteam, mounting arms were attached to the back sides of the CF faring to the pivot point on the pod, allowing it to swing up and down like an aircraft canopy
Thank you for reading through one of my proudest engineering projects. Overall, HX was a large team of 35 people, and thanks to our sponsors and individual contributions, we were able to construct a 40K pod to bring to Canada. We participated in the Canadian Hyperloop Global Challenge 2025 alongside Canadian, European, and American Hyperloop pods.
Thank you for chekcing out my experience on HyperXite at UCI.
Want to see my walker project below? Where I tackle the daunting issue of moving a rover without rolling wheels to generate traction. The walker's 4-legs enable smooth movement due to the concept of two grounded legs at a time.
Personal: shaikaman2004@gmail.com
School: abshaik@uci.edu
@2024 by Aman Shaik
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