1. Project : Investigation of CFD-CAA Coupling Schemes in MDO Framework
Client : Airbus (European Aeronautic Defense and Space)
2-D Grid for flow past a cylinder
Vortex shedding in the wake region
Grid cross­section of Airbus wing @ 0.06S from root

2. Flow streamlines at the wing tip
Frequency spectrum for dipole noise sources at a point on the control surface 900 from + x axis

3. Directivity plot of dipole SPL (dB) at r = 25 Croot , z = 0 for f = 128 Hz : dipole (y­axis)
Project : Package for Optimization of Wankel Engine and Research
Package for Optimization of Wankel Engine and Research (GUI)