The project focused on numerically analyzing hydrogen fuel injection into a Mach 2 air stream within a scramjet combustor, distinguishing combustion effects from non-combustion scenarios. Key results included static wall pressure, temperature, Mach number, and velocity distribution. 

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The primary objective of this project is to investigate aerodynamic drag reduction in aerospace vehicles through the utilization of aerospikes and to assess their feasibility. If aerospikes prove effective in drag reduction, it could revolutionize aircraft design. The incorporation of aerospike on blunt noses not only reduces fuel consumption but also significantly reduces the pressure drag

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In this project, I used ANSYS Fluent to simulate sloshing in an accelerating container. I looked at important details like slosh angles and water heights. I added a Python script to ANSYS to make the acceleration change in three directions. I also explored different ways to move the simulation results from ANSYS Fluent to a Python file. This project helped me improve my skills in computational fluid dynamics.