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Cfd module, hull viscous resistance
Posted 2010年11月16日 GMT-5 10:29 Fluid & Heat, Computational Fluid Dynamics (CFD) Version 4.0a 9 Replies
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Hi all,
i'm trying to solve the viscous resistance of a simplyfied hull geometry: i have modelled the boundary layer with the proper instruments an i've also checked the maximum wall lift off in viscous units as described in the Comsol cfd user manual. my problem is that the solution doesn't converge. Can you suggest me a solution to this problem or some guide lines to solve it?
Geometry and boundary conditions
The hull lenght is about of 10 m, the beam is of 3 m, the maximum draft is of 0.57 m . i've done such model using an ellipsoid with those charachteristics (a=5m,b=1.5m,c=0.57m) and i put it in a rectangular channel (L=40m, B=5m,C=2m) with the stern at a distance of 10m from the inlet. the model is only half because of the symmetry of the hull, the waterline plane is also a boundary of my rectangular domain and i chose for it a symmetry condition. At the inlet i have a normal velocity of 3.5 m/s; at the outlet i have pressure, no viscous stress, on the hull i have wall functions (k-eps turb. model with 0.05 turbolence intensity and 0.1m as turb lenght scale), on the other walls i have allowed the slip condition.
As a result of my calculations the height of the first cell in the boundary near the hull, should be of about 1e-5 m to satisfy the condition on the wall lift off in viscous units parameter.
Thank you very much for the attentions, Edoardo
i'm trying to solve the viscous resistance of a simplyfied hull geometry: i have modelled the boundary layer with the proper instruments an i've also checked the maximum wall lift off in viscous units as described in the Comsol cfd user manual. my problem is that the solution doesn't converge. Can you suggest me a solution to this problem or some guide lines to solve it?
Geometry and boundary conditions
The hull lenght is about of 10 m, the beam is of 3 m, the maximum draft is of 0.57 m . i've done such model using an ellipsoid with those charachteristics (a=5m,b=1.5m,c=0.57m) and i put it in a rectangular channel (L=40m, B=5m,C=2m) with the stern at a distance of 10m from the inlet. the model is only half because of the symmetry of the hull, the waterline plane is also a boundary of my rectangular domain and i chose for it a symmetry condition. At the inlet i have a normal velocity of 3.5 m/s; at the outlet i have pressure, no viscous stress, on the hull i have wall functions (k-eps turb. model with 0.05 turbolence intensity and 0.1m as turb lenght scale), on the other walls i have allowed the slip condition.
As a result of my calculations the height of the first cell in the boundary near the hull, should be of about 1e-5 m to satisfy the condition on the wall lift off in viscous units parameter.
Thank you very much for the attentions, Edoardo
9 Replies Last Post 2010年12月18日 GMT-5 17:10