DPW-IV Common Research Model (CRM) CASE-1 CP Data Form (version 3) ------------------------------------------------------ Date: [Due 26 MAY 2009] PARTICIPANT INFORMATION ----------------------- Name: Email: Phone: Address: Address: Address: Address: Address: Address: SOLVER INFORMATION -------------------- Method Name: Basic Algorithm: Turbulence Model: Miscellaneous: --------------------------------------------------- CASE 1.1: SINGLE-POINT GRID CONVERGENCE STUDY - WING CP AND CF DISTRIBUTIONS --------------------------------------------------- WING/BODY/TAIL (iH = 0 degrees) - COARSE GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 WING/BODY/TAIL (iH = 0 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 WING/BODY/TAIL (iH = 0 degrees) - FINE GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 WING/BODY/TAIL (iH = 0 degrees) - EXTRAFINE GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 -------------------------------------------------------------- CASE 1.1: SINGLE-POINT GRID CONVERGENCE STUDY - HORIZONTAL TAIL CP AND CF DISTRIBUTIONS -------------------------------------------------------------- WING/BODY/TAIL (iH = 0 degrees) - COARSE GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.650, 75.600, 256.242) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.582, 126.000, 263.200) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2358.134, 210.000, 274.796) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2429.687, 294.000, 286.393) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2501.239, 378.000, 297.989) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2519.128, 399.000, 300.888) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2533.438, 415.800, 303.207) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.760, 74.554, 256.101), X_TE=(2450.611) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2250.906, 84.118, 257.421), X_TE=(2455.280) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2259.052, 93.681, 258.741), X_TE=(2459.948) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 WING/BODY/TAIL (iH = 0 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.650, 75.600, 256.242) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.582, 126.000, 263.200) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2358.134, 210.000, 274.796) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2429.687, 294.000, 286.393) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2501.239, 378.000, 297.989) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2519.128, 399.000, 300.888) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2533.438, 415.800, 303.207) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.760, 74.554, 256.101), X_TE=(2450.611) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2250.906, 84.118, 257.421), X_TE=(2455.280) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2259.052, 93.681, 258.741), X_TE=(2459.948) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 WING/BODY/TAIL (iH = 0 degrees) - FINE GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.650, 75.600, 256.242) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.582, 126.000, 263.200) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2358.134, 210.000, 274.796) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2429.687, 294.000, 286.393) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2501.239, 378.000, 297.989) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2519.128, 399.000, 300.888) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2533.438, 415.800, 303.207) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.760, 74.554, 256.101), X_TE=(2450.611) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2250.906, 84.118, 257.421), X_TE=(2455.280) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2259.052, 93.681, 258.741), X_TE=(2459.948) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 WING/BODY/TAIL (iH = 0 degrees) - EXTRAFINE GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 ?.??? 0.50?? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.650, 75.600, 256.242) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.582, 126.000, 263.200) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2358.134, 210.000, 274.796) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2429.687, 294.000, 286.393) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2501.239, 378.000, 297.989) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2519.128, 399.000, 300.888) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2533.438, 415.800, 303.207) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.760, 74.554, 256.101), X_TE=(2450.611) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2250.906, 84.118, 257.421), X_TE=(2455.280) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2259.052, 93.681, 258.741), X_TE=(2459.948) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 ----------------------------------------------------- CASE 1.2: DOWNWASH STUDY DRAG POLARS - WING CP AND CF DISTRIBUTIONS - ALPHA = 2.500 ----------------------------------------------------- WING/BODY/NO TAIL - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 WING/BODY/TAIL (iH =-2 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 WING/BODY/TAIL (iH = 0 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 WING/BODY/TAIL (iH =+2 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? WING SECTION 1 Y/BO2 = 0.1050 (Y = 121.459 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = ( 993.728, 121.459, 176.053) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 466.466 WING SECTION 2 Y/BO2 = 0.1150 (Y = 133.026 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1002.168, 133.026, 176.306) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 459.571 WING SECTION 3 Y/BO2 = 0.1250 (Y = 144.594 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1010.656, 144.594, 176.539) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 452.687 WING SECTION 4 Y/BO2 = 0.1306 (Y = 151.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1015.435, 151.074, 176.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 448.836 WING SECTION 5 Y/BO2 = 0.2009 (Y = 232.444 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1076.873, 232.444, 177.509) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 400.743 WING SECTION 6 Y/BO2 = 0.2828 (Y = 327.074 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1148.974, 327.074, 178.606) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 344.991 WING SECTION 7 Y/BO2 = 0.3430 (Y = 396.765 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1202.038, 396.765, 180.222) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 304.101 WING SECTION 8 Y/BO2 = 0.3700 (Y = 427.998 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1225.822, 427.998, 181.162) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 285.806 WING SECTION 9 Y/BO2 = 0.3971 (Y = 459.370 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1249.711, 459.370, 182.250) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 278.111 WING SECTION 10 Y/BO2 = 0.5024 (Y = 581.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1342.440, 581.148, 188.658) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 248.312 WING SECTION 11 Y/BO2 = 0.6028 (Y = 697.333 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1430.914, 697.333, 198.060) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 219.904 WING SECTION 12 Y/BO2 = 0.7268 (Y = 840.704 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1540.091, 840.704, 213.659) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 184.844 WING SECTION 13 Y/BO2 = 0.8456 (Y = 978.148 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1644.738, 978.148, 233.317) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 151.235 WING SECTION 14 Y/BO2 = 0.9500 (Y = 1098.926 in) EXPERIMENTAL (X_LE,Y_LE,Z_LE) = (1736.708,1098.926, 253.727) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 121.735 WING SECTION 15 Y/BO2 = 0.9700 (Y = 1122.048 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1754.313,1122.048, 257.777) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 116.095 WING SECTION 16 Y/BO2 = 0.9900 (Y = 1145.183 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (1771.927,1145.183, 261.823) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 110.452 ---------------------------------------------------------------- CASE 1.2: DOWNWASH STUDY DRAG POLARS - HORIZONTAL TAIL CP AND CF DISTRIBUTIONS - ALPHA = 2.500 ---------------------------------------------------------------- WING/BODY/TAIL (iH =-2 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.681, 75.600, 252.007) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.343, 126.000, 260.458) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2357.448, 210.000, 274.545) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2428.552, 294.000, 288.631) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2499.656, 378.000, 302.717) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2517.432, 399.000, 306.239) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2531.653, 415.800, 309.056) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.791, 74.549, 251.837), X_TE=(2450.435) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.644 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.644 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2250.893, 84.120, 253.442), X_TE=(2455.064) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.171 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.171 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2258.995, 93.692, 255.046), X_TE=(2459.693) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.698 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.698 WING/BODY/TAIL (iH = 0 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.650, 75.600, 256.242) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.582, 126.000, 263.200) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2358.134, 210.000, 274.796) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2429.687, 294.000, 286.393) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2501.239, 378.000, 297.989) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2519.128, 399.000, 300.888) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2533.438, 415.800, 303.207) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.760, 74.554, 256.101), X_TE=(2450.611) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.851 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2250.906, 84.118, 257.421), X_TE=(2455.280) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.374 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2259.052, 93.681, 258.741), X_TE=(2459.948) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.896 WING/BODY/TAIL (iH =+2 degrees) - MEDIUM GRID GRID_SIZE MACH ALPHA CL_TOT ????????. 0.85 2.500 0.???? HORIZONTAL TAIL SECTION 1 Y/bo2 = 0.1800 (Y = 75.600 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2243.768, 75.600, 260.477) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 224.363 HORIZONTAL TAIL SECTION 2 Y/bo2 = 0.3000 (Y = 126.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2286.916, 126.000, 265.932) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.525 HORIZONTAL TAIL SECTION 3 Y/bo2 = 0.5000 (Y = 210.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2358.829, 210.000, 275.024) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 171.467 HORIZONTAL TAIL SECTION 4 Y/bo2 = 0.7000 (Y = 294.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2430.743, 294.000, 284.116) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 138.421 HORIZONTAL TAIL SECTION 5 Y/bo2 = 0.9000 (Y = 378.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2502.657, 378.000, 293.208) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 105.398 HORIZONTAL TAIL SECTION 6 Y/bo2 = 0.9500 (Y = 399.000 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2520.635, 399.000, 295.481) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 97.148 HORIZONTAL TAIL SECTION 7 Y/bo2 = 0.9900 (Y = 415.800 in) CFD-ONLY (X_LE,Y_LE,Z_LE) = (2535.018, 415.800, 297.300) X/C Y/C Z/C CP CF CFX CFY CFZ CHORD ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 ???.???? 0.0000 ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 90.551 HORIZONTAL TAIL SOB CUT 8 0.1736X + 0.9848Y + 0.0Z = 462.873 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2242.858, 74.537, 260.361), X_TE=(2450.690) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.832 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 207.832 HORIZONTAL TAIL SOB CUT 9 0.1736X + 0.9848Y + 0.0Z = 473.706 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2251.040, 84.094, 261.396), X_TE=(2455.393) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.354 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 204.354 HORIZONTAL TAIL SOB CUT 10 0.1736X + 0.9848Y + 0.0Z = 484.539 CFD-ONLY (X_LE,Y_LE,Z_LE) = (2259.222, 93.652, 262.430), X_TE=(2460.097) X/CUTLEN(X) Y/CUTLEN(X) Z/CUTLEN(X) CP CF CFX CFY CFZ CUTLEN(X) ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.875 ???.???? ???.???? ???.???? ???.???? ???.?????? ???.?????? ???.?????? ???.?????? 200.875 NOTES: ------ * Information lines are 80 characters long. * Information blocks allow free-form miscellaneous information. * GRID_SIZE (F10.0) Number of grid nodes or cells * MACH (F10.2) Mach Number. * ALPHA (F10.3) Angle of Attack in Degrees. * CL_TOT (F10.4) Total Lift Coefficient. * Include as many X/C, CP pairs as necessary for each cut location * X/C (F12.4) [(X coordinate) - (X_LE)] non-dimensionalized by local chord (CHORD) * Y/C (F12.4) [(Y coordinate) - (Y_LE)] non-dimensionalized by local chord (CHORD) * Z/C (F12.4) [(Z coordinate) - (Z_LE)] non-dimensionalized by local chord (CHORD) * X/CUTLEN(X) (F12.4) [(X coordinate) - (X_LE)] non-dimensionalized by CUTLEN(X) * Y/CUTLEN(X) (F12.4) [(Y coordinate) - (Y_LE)] non-dimensionalized by CUTLEN(X) * Z/CUTLEN(X) (F12.4) [(Z coordinate) - (Z_LE)] non-dimensionalized by CUTLEN(X) * X_LE (F10.3) X coordinate at leading edge of cut * Y_LE (F10.3) Y coordinate at leading edge of cut * Z_LE (F10.3) Z coordinate at leading edge of cut * X_TE (F10.3) X coordinate at trailing edge of cut * CHORD (F10.3) Local chord - distance from cut leading edge to trailing edge * CUTLEN(X) (F10.3) Difference between (X_TE) - (X_LE) * CP (F12.4) Coefficient of pressure * CF (F14.6) Skin-friction Coefficient at wall = tauw/(freestream dynamic pressure) * CFX, CFY, CFZ (F14.6) Components of skin-friction Coefficient at wall * BO2 Wing Semispan (1156.75 in) * bo2 Tail Semispan ( 420.00 in)