VLMpc Manual - the AOE home page

D-52 Applied Computational Aerodynamicsbreak points for this configurationpoint x y z sweep dihedral moveangle angle code1 37.80000 0.00000 0.00000 73.89906 0.00000 12 24.46218 -3.85000 0.00000 73.89906 0.00000 13 22.73000 -4.35000 0.00000 90.00000 0.00000 14 14.69000 -4.35000 0.00000 39.96069 0.00000 15 12.58679 -6.86000 0.00000 39.96069 0.00000 16 9.36076 -10.71000 0.00000 39.96069 0.00000 17 4.17397 -16.90000 0.00000 39.96069 0.00000 18 0.11000 -21.75000 0.00000 90.00000 0.00000 19 -3.24000 -21.75000 0.00000 -40.15676 0.00000 110 -14.96000 -7.86000 0.00000 0.00000 0.00000 111 -14.96000 0.00000 0.00000second planform breakpoints1 -14.96000 0.00000 0.00000 0.00000 0.00000 12 -14.96000 -4.35000 0.00000 0.00000 0.00000 13 -14.96000 -7.86000 0.00000 37.91007 43.00000 14 -22.00000 -16.90000 -8.42994 90.00000 0.00000 15 -24.51000 -16.90000 -8.42994 -38.87364 43.00000 16 -29.50000 -10.71000 -2.65767 41.02898 43.00000 17 -27.02000 -7.86000 0.00000 -53.26718 0.00000 18 -28.36000 -6.86000 0.00000 41.68077 0.00000 19 -25.68000 -3.85000 0.00000 -42.43624 0.00000 110 -29.20000 0.00000 0.00000168 horseshoe vortices used on the left half of the configurationplanform total spanwise1 90 152 78 1316. horseshoe vortices in each chordwise rowaerodynamic dataconfiguration no. 23.static longitudinal aerodynamic coefficients are computedpanel x x y z sno. c/4 3c/41 0.61276 0.21636 -20.91346 0.00000 0.836542 -0.18004 -0.57644 -20.91346 0.00000 0.836543 -0.97284 -1.36924 -20.91346 0.00000 0.836544 -1.76564 -2.16204 -20.91346 0.00000 0.836545 -2.55845 -2.95485 -20.91346 0.00000 0.836546 -3.35125 -3.74765 -20.91346 0.00000 0.836547 1.89745 1.26658 -19.24039 0.00000 0.83654Friday, November 17, 1995