Pressure contour computed with FlightStream for ONERA M6 wing case

Shuchi2026

Hi, I tried to load the surface mesh from CFD which is in PLOT3D format. And I ran the case M=0.84, AoA = 3.06 deg with the transonic field panel method. I just ran the case without boundary-layer coupling. The pressure contour does show the Lambda-type shockwave. The surface grid is attached. Not sure whether you can repeat this case and compare the results.

m6surf.p3d

shahfiqshahjahan

Hi Shuchi2026, thank you for your enquiry. I'm afraid I don't quite understand the question here. Could you email me directly with your enquiries? My email address is shahfiq.shahjahan@siemens.com. Thank you!