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cpxs.out
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cpxs.out
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0 CL = 0.008688
CM = -0.041285
CP* = -0.043010
TSFOIL2 Mach = 0.975 CL = 0.009
i X/C Cp-up M-up Cp-low M-low
0 -1.0750 0.21298 0.8403 0.21298 0.8403
0 -0.9500 0.21851 0.8365 0.21851 0.8365
0 -0.8250 0.22639 0.8311 0.22639 0.8311
0 -0.7000 0.23947 0.8220 0.23947 0.8220
0 -0.5750 0.25921 0.8081 0.25921 0.8081
0 -0.4500 0.28691 0.7882 0.28691 0.7882
0 -0.3500 0.32333 0.7612 0.32333 0.7612
0 -0.2500 0.37225 0.7234 0.37225 0.7234
0 -0.1750 0.43304 0.6734 0.43304 0.6734
0 -0.1250 0.50490 0.6091 0.50490 0.6091
0 -0.0750 0.59625 0.5159 0.59625 0.5159
0 -0.0525 0.69055 0.3973 0.69055 0.3973
0 -0.0350 0.77976 0.2355 0.77976 0.2355
0 -0.0225 0.86961 0.0000 0.86961 0.0000
0 -0.0150 0.95210 0.0000 0.95210 0.0000
0 -0.0075 1.03276 0.0000 1.03276 0.0000
0 -0.0025 1.11202 0.0000 1.11202 0.0000
0 0.0025 1.23367 0.0000 1.24729 0.0000
0 0.0075 0.99182 0.0000 1.00482 0.0000
0 0.0125 0.75885 0.2819 0.76897 0.2605
0 0.0175 0.58796 0.5250 0.59231 0.5203
0 0.0225 0.47083 0.6404 0.46739 0.6435
0 0.0275 0.38392 0.7141 0.37228 0.7234
0 0.0325 0.31697 0.7660 0.29745 0.7805
0 0.0375 0.26134 0.8066 0.23395 0.8259
0 0.0450 0.20532 0.8455 0.17037 0.8689
0 0.0550 0.15330 0.8801 0.11379 0.9055
0 0.0650 0.11163 0.9069 0.07129 0.9321
0 0.0750 0.07799 0.9279 0.03875 0.9519
0 0.0850 0.04766 0.9465 0.01063 0.9687
0 0.0975 0.01494 0.9662 -0.01909 0.9862
0 0.1150 -0.02601 0.9902 -0.06234 1.0110
0 0.1406 -0.08015 1.0211 -0.11283 1.0393
0 0.1719 -0.13231 1.0500 -0.15820 1.0641
0 0.2031 -0.17205 1.0715 -0.19972 1.0862
0 0.2344 -0.20732 1.0902 -0.23859 1.1066
0 0.2656 -0.23940 1.1070 -0.28107 1.1284
0 0.2969 -0.26957 1.1225 -0.33316 1.1546
0 0.3281 -0.29925 1.1376 -0.39581 1.1853
0 0.3594 -0.32833 1.1522 -0.46344 1.2176
0 0.3906 -0.35679 1.1663 -0.52920 1.2483
0 0.4219 -0.38573 1.1804 -0.58820 1.2751
0 0.4531 -0.41682 1.1955 -0.63767 1.2972
0 0.4844 -0.45078 1.2117 -0.67627 1.3141
0 0.5156 -0.48707 1.2287 -0.70397 1.3262
0 0.5469 -0.52435 1.2460 -0.72225 1.3341
0 0.5781 -0.55997 1.2623 -0.73317 1.3388
0 0.6094 -0.59140 1.2765 -0.73810 1.3409
0 0.6406 -0.61863 1.2887 -0.73759 1.3407
0 0.6719 -0.64298 1.2995 -0.73145 1.3380
0 0.7031 -0.66569 1.3095 -0.71925 1.3328
0 0.7344 -0.68712 1.3189 -0.70040 1.3246
0 0.7656 -0.70725 1.3276 -0.67527 1.3137
0 0.7969 -0.72609 1.3357 -0.64428 1.3001
0 0.8281 -0.74342 1.3432 -0.60548 1.2829
0 0.8594 -0.75925 1.3499 -0.55875 1.2618
0 0.8850 -0.77229 1.3554 -0.51233 1.2405
0 0.9000 -0.78198 1.3595 -0.47218 1.2218
0 0.9150 -0.79064 1.3632 -0.43152 1.2025
0 0.9300 -0.79980 1.3670 -0.38328 1.1792
0 0.9450 -0.80956 1.3711 -0.32380 1.1499
0 0.9600 -0.82048 1.3757 -0.22489 1.0995
0 0.9750 -0.83364 1.3812 0.04751 0.9466
0 0.9900 -0.79059 1.3632 0.28674 0.7883
0 1.0000 -0.65032 1.3028 -0.02102 0.9873
0 1.0100 -0.42953 1.2015 -0.42953 1.2015
0 1.0250 -0.38331 1.1793 -0.38331 1.1793
0 1.0500 -0.36081 1.1683 -0.36081 1.1683
0 1.0900 -0.35576 1.1658 -0.35576 1.1658
0 1.1500 -0.35154 1.1637 -0.35154 1.1637
0 1.2250 -0.34113 1.1586 -0.34113 1.1586
0 1.3000 -0.32506 1.1506 -0.32506 1.1506
0 1.4000 -0.30752 1.1418 -0.30752 1.1418
0 1.5000 -0.14140 1.0550 -0.14140 1.0550
0 1.6250 0.13322 0.8931 0.13322 0.8931
0 1.7500 0.25559 0.8107 0.25559 0.8107
0 1.8750 0.26614 0.8032 0.26614 0.8032