Labs

I worked with low speed and high speed wind tunnels at Arizona state university designing and conducting tests on Airfoils of various types. Some of them involved obtaining lift and drag characteristics for various profile.

Calculating Lift and Drag for Various Wings

Calculating Lift and Drag for Various Wings

Drag Polars and Effects of Winglets

Investigation of a Shock Wave using a Shock Tube

Investigation of Compressible Flow through a Nozzle

Drag Divergence Mach Number

Numerical Solution for Prandtl Glauert Equation