Turbulent Flow Study Over an Airfoil
Using ANSYS Fluent CFD Solver, I analyzed turbulent flow over a NACA-0012 airfoil by varying the angle of attack while using a constant freestream velocity.
Using ANSYS Fluent CFD Solver, I analyzed turbulent flow over a NACA-0012 airfoil by varying the angle of attack while using a constant freestream velocity.
SolidWorks CAD design of wing ribs and spar internal wing components
Solidworks CAD design of my rocket kit. Currently in the process of obtaining a Level 1 High Powered Rocketry Certification.
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