DESCRIPTION
Drag = 0.5 * Cd * Rho * V**2
| with | Cd = P1Drag / ( Re**P2Drag) |
| Rho = (MGas*Press/RUniv) / (T+Tref+T0)
Re = Radius * V / NuGas |
|
| where | Re is the Reynolds number |
| Rho is the density of the gas (air) | |
| MGas is the mole mass of the gas (air) | |
| Press is the pressure | |
| RUniv is the molar gas constant | |
| Tref is a temperature reference | |
| T0 is a temperature offset | |
| Radius is the local radius of the fiber | |
| NuGas is the kinematik viscosity of the gas (air) |
-1Upper level menu The current parameters are accepted 0Enable drag Switches the model on 0'Disable drag Switches the model off 1Modify P1Drag = 1.0000000E+00 2Modify P2Drag = 0.0000000E+00 3Modify MGas = 1.0000000E+00 4Modify Press = 1.0000000E+00 5Modify RUniv = 1.0000000E+00 6Modify Tref = 0.0000000E+00 7 Modify T0 = 0.0000000E+00 8Modify NuGas = 1.0000000E+00 Remark : NuGas cannot be set when the sub-task is non-isothermal and the user has access to the 'Flux fiber spinning' thermal boundary condition. In such a case, NuGas is calculated as a function of temperature.