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This paper documents a numerical model, developed for the McGill Rocket Team based on classical chemical thermodynamics coupled with the Trebble-Bishnoi equation of state, to solve for the oxidizer tank conditions (pressure, temperature, mole flowrate and liquid/vapour equilibrium) during the operation of a hybrid rocket. This model is modular and can be coupled to fluid mechanics and combustion chamber models for a more detailed analysis of a hybrid rocket engine.

This is a simple template that i used for my projects at the university. The most of it is in italian so you have to change languages set if you want to use it.

Simple template for approving software components.

Lizhen Zhu's Resume Created with the Friggeri CV template

Final Project of the course named Scientific Researching Method. Our project was about emotional recognition

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A discussion essay template for my assignment.

CV for french version Created with the Friggeri CV template

Sandeep Kumar's CV Created with the Friggeri CV template