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Ashwin

Milan | Italy

ABOUT ME

Hi, I'm Ashwinraj. I'm an Aeronautical Engineering Master's student at Politecnico di Milano. I specialize in high-speed aerodynamics and computational fluid dynamics (CFD).

Previously, I served as the Team Leader and Head of Aerodynamics for the thrustMIT rocketry team, managing 40 members to achieve a successful 10,331-foot launch at the Spaceport America Cup. I also love the intersection of aerospace and code.

I won the FOSSHACK 3.0 hackathon by building a 6-DOF trajectory simulator in Python, and I'm currently diving deep into open-source solvers like OpenFOAM on my custom Linux machine. I'm actively looking for an internship where I can tackle complex, real-world aerospace problems.

PROJECTS
CONTACT
RESUME
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thrustMIT 10,000 Feet - Sounding Rocket

I was the 2022-2023 Team Leader & Head of Aerodynamics of thrustMIT, Manipal Rocketry team and led a 40-member multidisciplinary rocketry team to design, build, and launch a sounding rocket for the Spaceport America Cup 2023. Directed all...

ANSYS FluentTeam LeadershipProject ManagementTrajectory SimulationTransonic/Supersonic AerodynamicsComputational Fluid Dynamics (CFD)
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Computational Aerodynamics - Method Implementation and Aircraft Analysis

The primary goal of this project was to move beyond commercial "black-box" solvers by writing custom MATLAB code to implement foundational aerodynamic theories. The project involved developing, validating, and applying 2D and 3D computational...

XFOIL XFLR5 MATLAB Hess-Smith Method Weissinger Method Computational Aerodynamics Aircraft Performance Analysis
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Helios - 6DOF Rocket Trajectory Simulator

First-place winning hackathon project (Awarded ₹1,00,000 / ~$1,100). Developed a high-precision, 6-degree-of-freedom flight dynamics simulator in Python designed to accurately predict sounding rocket trajectories, apogees, and performance under...

PythonAerodynamicsFlight Dynamics6-DOF SimulationMathematical Modeling
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CFD Performance Analysis of a Rocket-Based Combined Cycle (RBCC) Engine

Culminating Bachelor's Thesis evaluating the aerodynamic and propulsive efficiencies of a novel Rocket-Based Combined Cycle (RBCC) engine for supersonic cruise missile applications. Designed a 3D model in Fusion 360 and conducted rigorous CFD...

MATLABAnsys FluentAerodynamicsPropulsion SystemsAutodesk Fusion 360Supersonic Flow AnalysisComputational Fluid Dynamics (CFD)