Please help! Fluent calculating airplane:DLR-F6
 

Now,I am computing the Cl and Cd of DLR-F6 using Fluent,but the result is not correct.
the ULR is:http://aaac.larc.nasa.gov/tsab/cfdla...nd_Results.htm

Condition: MACH=0.75,alpha=0.201,Cl=0.5,Mesh elements=3370000(provided by Fluent inc.)


but my result:Cl=0.05,reference area=0.339m2,reference length=0.417m,is these two value right?

what's wrong? or,Does anyone have 3D examples about airplane??