Pressure far field B.C
 

Hi, I am trying to carry out CFD of delta wing. Wind tunnel data for B.C is available which is " test section = 8x8 ft test section, super sonic wind tunnel, Stagnation pressure = 26" Hg for all mach nos from 1.3 to 2.8. Re = 2e+6/ft at Mach = 1.3 to Re = 4e+6/ft at 2.8". Can any body provide me Pressure far field B.C for FLUENT 6.1. Thanks.