Wind Tunnel Measurement around NACA 2415
The purpose of this project is to do the post analysis of the experimental data of wind tunnel experiment of NACA 2415 airfoil and calculate the coefficient of drag, lift and moment using the numerical method and comparing the result with external resources.
Potential Flow
The purpose of this project is to find out the stagnation points and maximum thickness of a Rankine full body formed by a source and sink of equal strengths.
Vortex Sheet and Vortex Panel
The purpose of this project is to prove the pressure difference across the vortex sheet proportional to the local vortex strength and the pressure coefficient distribution around circular cylinder using source panel method
Computational Model of Closed Loop Wind Tunnel
In this project, a detailed Computational Fluid Dynamics (CFD) investigation of a closed looped wind tunnel was carried to characterize the fluid flow pattern and pressure drop in a wind tunnel, especially highlighting the effect of turning vanes profile to flow uniformity of air in test section and the resulting pressure drop across the 90 degree turning vanes.
