fluid dynamics (CFD) and lifting line theory. Commercially available finite volume CFD code of FLUENT was used to calculate threedimensional, incompressible, steady-state continuity and momentum equations. Reynolds-Averaged Navier-Stokes
Summary
In this study an optimum geometry for a bow thruster propeller is obtained by computational fluid dynamics (CFD) and lifting line theory. Commercially available finite volume CFD code of FLUENT was used to calculate threedimensional, incompressible, steady-state continuity and momentum equations. Reynolds-Averaged Navier-Stokes