Listed below is the input data (.dat) file demo.dat used for this case.
Demo of airfoil/flap Chimera grid Mach 0.6 First run / Inlet conditions Freestream static 0.6 14.7 520. 0. 0. / Boundary conditions Downstream pressure 14.7 zone 1 / Viscous terms Turbulence sst / Numerics Cycles 500 End
Two runs were made for a total of 1000 cycles (5000 iterations) On an SGI Octane R10000 system, in serial mode, each run required just over 3200 seconds of CPU time. Genplot files for the maximum and L2 residuals were generated using resplt, as described under "Monitor Convergence" in the "Tutorial" section of the Wind-US User's Guide.
The residuals are shown below.
Last updated 9 Feb 2000