737 lift and drag analysis
5 Attachment(s)
Hi all,
I am running a simulation for a 737 wing like the one shown in the picture. For the mesh I used: 210,796 nodes 483,672 elements 15 inflation layers, thirst layer height 9e-2 m, growing at a rate of 1.05. The colored mesh shows the element quality. For the CFD conditions I used: air ideal gas pressure farfield conditons 0 angle of attack Pressure at 11,000 m Velocity is Mach 0.74 216 K (Temperature at 11,000 m) I think that my lift and drag results are too low for a wing of that size. What I get is: net drag = 3586.2391 N net lift = 40687.128 N Can someone explain me what is wrong? Is the mesh not fine enough? or is it the inflation? what should I do to improve the results and what results should I expect? Thank you very much. |
|
All times are GMT -4. The time now is 08:40. |