Effect of tip clearance and axial gap variation in a three stage axial compressor
CFD analysis of a three stage axial compressor with variation in tip clearance and axial gap between rotors and stators
turbomachinery
CFD and FEA simulation of a cross flow turbine
Fluid strucutre interaction analysis of a hydro turbine is performed in this case. Initially CFD analysis was completed and hydrodynamic loads are transferred to the structure to evaluate deformation and mode shape.