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We use Xfoil to find our drag and lift coefficients on a NACA 4415 airfoil. We also determine the critical angle of attack for maximum aerodynamic performance of this airfoil, using different Reynolds numbers. We then export our data to Excel for plotting.

We use Ansys Fluent to analyze flow around a stationary and rotating cylinder. We use different flow velocities to monitor change in our lift and drag coefficients.

We simulate laminar fluid flow over a flat plate, in which we analyze skin fiction, wall shear stress and velocity profiles.

We create the geometry for a 2d wind tunnel, in which we analyze the pressure and velocity profiles during simulation. We then place an airfoil inside the tunnel and re-analyze our pressure and velocity profiles. Data is exported to excel.

We plot pressure coefficients on a graph using different angles of attack. We then export our data to Excel.

We use Ansys Mechanical to analyze how a square, fixed, beam vibrates.

Using Ansys Mechanical, we can see how a rectangular beam vibrates.

We use multiple Reynolds numbers to analyze how streamlines and drag forces change.

Pressure and Velocity profiles of a flow around a cylinder. Multiple Reynolds numbers are used to show the change in profiles as the Reynolds number increases.

A short video showing a robotic arm I created, in action.

We look at velocity and pressure profiles of air flow over a flat plate.

We use Ansys software to simulate pressure driven Poiseuille flow and wall driven Couette flow. This software allows us to see when the flow is fully developed in the straight pipe. It also allows us to analyze pressure and velocity profiles of the flow throughout the length of the straight pipe.