19.04.2011 08:37
BOUNDARY: hf2_lb_in 1
Boundary Type = INLET
Interface Boundary = Off
Location = hf2_1
BOUNDARY CONDITIONS:
FLOW REGIME:
Option = Subsonic
END
HEAT TRANSFER:
Option = Static Temperature
Static Temperature = areaAve(T)@REGION:hf2_1
END
MASS AND MOMENTUM:
Normal Speed = v LB HF2
Option = Normal Speed
END
TURBULENCE:
Option = Medium Intensity and Eddy Viscosity Ratio
END
END
END