CFD

Upcoming Projects:

transonic CFD Validation on NASA onera wing

Supersonic CFD Validation on NASA canard driven full model missile (it looks something similar to the AIM-9 series of IR air-to-air missile family)

Using Hybrid RANS-LES Methods For More Robust Characterization of External Aerodynamic Flows (having some trouble with this right now, so might take a bit to release).

CFD Analysis of Compressibility effects on wing and comparison to theory and empirical standards (will not go beyond drag divergence point, so probably no more than mach 0.5-0.7)

Effect of sweep on supersonic flow regimes

Effect of mach number on drag of simple shapes such as sphere, cone, and maybe airfoil

Low speed CFD validation on wing featuring comparison to VLM method (OpenVSP / VSPaero)