Why doesn't the simple airfoil example wing tip position plot start at zero? #145
Replies: 1 comment
|
Dear wmschy, The solvers included in the The simple airfoil case is a cantiliver beam subjected to aerodynamic forces. The idea behind it is finding the equilibrium position for that cantilever beam (with If you think of this case as an airplane wing: Running I hope this helps. |

Dear wmschy,
The solvers included in the
flowvariable run sequentially and use the solution from the previous solver. For example,StaticCoupleduses the model thatBeamLoaderandAerogridLoaderhave created.The simple airfoil case is a cantiliver beam subjected to aerodynamic forces. The idea behind it is finding the equilibrium position for that cantilever beam (with
StaticCoupled) and then change the angle of attack (with respect to the equilibrium position) withDynamicCoupled.If you think of this case as an airplane wing:
StaticCoupledwould give you the cruise deformation (which is not zero as you noted) andDynamicCoupledwould simulate a sudden change in the angle of attack.Ru…