CFD modeling, meshing and analysis was carried out on a blended aircraft wing body. Lift and drag coefficients were estimated for different angle of attacks.
Fluid structure interaction analysis was carried out on an aircraft wing. CFD analysis was performed and aerodynamic loads were mapped onto structural domain to estimate deflection.
A two stage axial turbine was scanned and modelled for CFD analysis using CMM techniques. Performance was compared with test results and validated.
CFD analysis of a three stage axial compressor with variation in tip clearance and axial gap between rotors and stators