LETALIS: Liquid Propellant Rocket Engine thermal analysis and cooling system design.
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Updated
Sep 16, 2023 - Python
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LETALIS: Liquid Propellant Rocket Engine thermal analysis and cooling system design.
This CFD analysis investigates and compares the thermal performance of a panel cooled by **air flow at 2 m/s** (previous study) and **water flow at 1 m/s** (this current study). The focus is on evaluating the improvement in cooling when the same heat load is applied to the system but different cooling mediums are used.
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