Computational Results Search Dataset Types Force and Moment Pressure Reynolds Number 19.8 Million 30 Million 5 Million Mach Number 0.7 0.75 0.8 0.83 0.85 0.86 0.87 0.88 0.92 Series Configuration Wing/Body Wing/Body/Nacelle/Pylon Wing/Body/Tail = +2 Wing/Body/Tail = -2 Wing/Body/Tail = 0 Code Used BCFD CFL3D FUN3D OVERFLOW USM3D
