Calculate Optimal Design of Rocket Propulsion Systems (Kerbal Space Program).
A comprehensive solution for designing and optimizing student-built liquid rocket engines.
A Python Turbomachinery design library for liquid rocket engine applications.
Computes the contours of a 2D minimum-length supersonic nozzle for non-rotating flows using the method of the characteristics.
liquid rocket engine design, development, and sizing code
Database of propulsion system components for electric and fuel powered UAVs
Bench for measuring parameters of propulsion system (propeller, motor, regulator) of unmanned drones
Modeling performance of GE's F404-GE-402 engine in pyCycle
April 2021 liquid rocket swirl injector designed within OrbitX Philippines.
GitHub repository for the developed Unified Ducted fan Code (UDC) and Ducted Fan Optimisation Framework as part of my MSc thesis
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