Plan, set up, and run CFD analyses for aerodynamic designs using Star CCM+ to solve challenges and determine appropriateness and application to Missiles and UAVs. Geometry cleanup and quality grid generation for CFD analysis.After post-processing the results, give recommendations to the design team based on the generated results. Prepare reports on the aerodynamic data generated, such as flight performance validation and aircraft configurations. Study of dynamic stability of Air vehicles using low fidelity tools like OpenVSP, Xflr5 and AVL. Design and development of NACA submerged Intake for missile configurations using Solidworks and FloEFD.

Integrated CFD Simulation of Fixed Wing Unmanned Air Vehicles(UAVs)