Case studies

Few of our case studies completed for research scholars

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.
CFD analysis of fin and tube heat exchanger (radiator) and evaluation of heat transfer rate for various cooling fan configurations.
Design improvement of centrifugal vapour compressor was carried out using CFD simulations and design principles.
CFD analysis of fin and tube heat exchanger (radiator) and evaluation of heat transfer rate for various cooling fan configurations.
CFD modelling, analysis and validation of NASA 74-A three stage axial flow compressor.
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.
Aerodynamic design, CFD analysis and performance evaluation of a five stage axial compressor.
CFD analysis and simulation of a propeller blade with downstream swirl recovery vanes.
CFD analysis and performance evaluation of axial turbine stage with cooling purge flow from hub region into main stream flow.
CFD analysis of fin and tube heat exchanger (radiator) and evaluation of heat transfer rate for various design configurations.
CFD analysis of a three stage axial compressor with variation in tip clearance and axial gap between rotors and stators
CFD analysis of shell and tube heat exchanger and evaluation of heat transfer rate.
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.