NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0012-64 (naca001264-il) Reynolds number: 1,000,000 Max Cl/Cd: 63 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca001264-il-1000000.txt Download as CSV file: xf-naca001264-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0012-64
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1202 0.11676 0.11433 -0.0124 1.0000 0.0145
-19.000 -1.1663 0.10394 0.10134 -0.0194 1.0000 0.0144
-18.750 -1.2069 0.09241 0.08963 -0.0258 1.0000 0.0144
-18.500 -1.2395 0.08249 0.07954 -0.0313 1.0000 0.0144
-18.250 -1.2650 0.07414 0.07102 -0.0360 1.0000 0.0144
-18.000 -1.2831 0.06734 0.06406 -0.0398 1.0000 0.0145
-17.750 -1.2957 0.06179 0.05836 -0.0426 1.0000 0.0145
-17.500 -1.3040 0.05713 0.05356 -0.0447 1.0000 0.0146
-17.250 -1.3131 0.05267 0.04897 -0.0464 1.0000 0.0147
-17.000 -1.3309 0.04759 0.04372 -0.0477 1.0000 0.0150
-16.750 -1.3396 0.04386 0.03989 -0.0482 1.0000 0.0152
-16.500 -1.3413 0.04112 0.03706 -0.0482 1.0000 0.0154
-16.250 -1.3380 0.03901 0.03488 -0.0480 1.0000 0.0157
-16.000 -1.3320 0.03725 0.03305 -0.0476 1.0000 0.0159
-15.750 -1.3252 0.03564 0.03138 -0.0471 1.0000 0.0162
-15.500 -1.3176 0.03417 0.02983 -0.0463 1.0000 0.0165
-15.250 -1.3097 0.03278 0.02835 -0.0454 1.0000 0.0168
-15.000 -1.3010 0.03149 0.02698 -0.0444 1.0000 0.0171
-14.750 -1.2916 0.03031 0.02571 -0.0433 1.0000 0.0175
-14.500 -1.2805 0.02929 0.02459 -0.0421 1.0000 0.0178
-14.250 -1.2675 0.02847 0.02369 -0.0410 1.0000 0.0180
-14.000 -1.2656 0.02676 0.02186 -0.0387 1.0000 0.0184
-13.750 -1.2572 0.02565 0.02071 -0.0369 1.0000 0.0189
-13.500 -1.2438 0.02496 0.01997 -0.0355 1.0000 0.0193
-13.250 -1.2294 0.02436 0.01934 -0.0341 1.0000 0.0197
-13.000 -1.2153 0.02375 0.01868 -0.0325 1.0000 0.0201
-12.750 -1.2010 0.02315 0.01803 -0.0309 1.0000 0.0205
-12.500 -1.1869 0.02258 0.01739 -0.0291 1.0000 0.0210
-12.250 -1.1727 0.02206 0.01680 -0.0272 1.0000 0.0214
-12.000 -1.1587 0.02165 0.01632 -0.0251 1.0000 0.0217
-11.750 -1.1453 0.02140 0.01601 -0.0227 1.0000 0.0219
-11.500 -1.1449 0.02016 0.01469 -0.0182 1.0000 0.0226
-11.250 -1.1349 0.01960 0.01411 -0.0153 1.0000 0.0231
-11.000 -1.1234 0.01922 0.01371 -0.0125 1.0000 0.0236
-10.750 -1.1121 0.01886 0.01333 -0.0095 1.0000 0.0240
-10.500 -1.1008 0.01851 0.01294 -0.0066 1.0000 0.0244
-10.250 -1.0893 0.01815 0.01254 -0.0036 1.0000 0.0249
-10.000 -1.0771 0.01782 0.01216 -0.0008 1.0000 0.0254
-9.750 -1.0638 0.01754 0.01184 0.0018 1.0000 0.0259
-9.500 -1.0334 0.01724 0.01149 0.0008 0.9990 0.0263
-9.250 -1.0071 0.01631 0.01049 0.0005 0.9976 0.0271
-9.000 -0.9795 0.01555 0.00970 -0.0002 0.9962 0.0280
-8.750 -0.9491 0.01511 0.00925 -0.0012 0.9951 0.0288
-8.500 -0.9178 0.01471 0.00884 -0.0023 0.9941 0.0296
-8.250 -0.8881 0.01431 0.00841 -0.0031 0.9927 0.0304
-8.000 -0.8592 0.01391 0.00798 -0.0037 0.9906 0.0310
-7.750 -0.8285 0.01360 0.00764 -0.0046 0.9888 0.0316
-7.500 -0.7988 0.01305 0.00704 -0.0054 0.9871 0.0325
-7.250 -0.7685 0.01249 0.00646 -0.0063 0.9857 0.0337
-7.000 -0.7362 0.01210 0.00606 -0.0076 0.9846 0.0348
-6.750 -0.7031 0.01176 0.00572 -0.0090 0.9837 0.0360
-6.500 -0.6692 0.01146 0.00541 -0.0106 0.9830 0.0372
-6.250 -0.6406 0.01120 0.00512 -0.0109 0.9801 0.0380
-6.000 -0.6117 0.01079 0.00470 -0.0114 0.9773 0.0402
-5.750 -0.5811 0.01047 0.00440 -0.0122 0.9750 0.0426
-5.500 -0.5495 0.01020 0.00413 -0.0131 0.9730 0.0451
-5.250 -0.5190 0.00986 0.00384 -0.0139 0.9709 0.0516
-5.000 -0.4938 0.00956 0.00362 -0.0134 0.9665 0.0630
-4.750 -0.4680 0.00927 0.00339 -0.0131 0.9619 0.0784
-4.500 -0.4411 0.00897 0.00317 -0.0130 0.9581 0.0937
-4.250 -0.4155 0.00870 0.00298 -0.0126 0.9539 0.1122
-4.000 -0.3918 0.00841 0.00280 -0.0118 0.9480 0.1383
-3.750 -0.3672 0.00809 0.00261 -0.0112 0.9431 0.1719
-3.500 -0.3429 0.00777 0.00245 -0.0105 0.9378 0.2099
-3.250 -0.3198 0.00740 0.00227 -0.0096 0.9315 0.2591
-3.000 -0.2972 0.00692 0.00206 -0.0087 0.9260 0.3320
-2.750 -0.2763 0.00640 0.00188 -0.0074 0.9192 0.4209
-2.500 -0.2546 0.00593 0.00172 -0.0062 0.9128 0.5053
-2.250 -0.2326 0.00553 0.00160 -0.0050 0.9064 0.5838
-2.000 -0.2091 0.00527 0.00152 -0.0041 0.8994 0.6383
-1.750 -0.1846 0.00507 0.00146 -0.0033 0.8933 0.6855
-1.500 -0.1593 0.00494 0.00143 -0.0026 0.8861 0.7176
-1.250 -0.1329 0.00485 0.00139 -0.0022 0.8794 0.7403
-1.000 -0.1059 0.00480 0.00137 -0.0019 0.8721 0.7571
-0.750 -0.0793 0.00474 0.00134 -0.0015 0.8632 0.7767
-0.500 -0.0530 0.00470 0.00133 -0.0010 0.8516 0.7947
-0.250 -0.0265 0.00467 0.00131 -0.0005 0.8383 0.8094
0.000 0.0000 0.00467 0.00130 0.0000 0.8238 0.8239
0.250 0.0265 0.00467 0.00131 0.0005 0.8093 0.8382
0.500 0.0530 0.00470 0.00133 0.0010 0.7947 0.8515
0.750 0.0794 0.00474 0.00134 0.0015 0.7767 0.8632
1.000 0.1060 0.00480 0.00137 0.0019 0.7570 0.8721
1.250 0.1329 0.00485 0.00139 0.0022 0.7403 0.8794
1.500 0.1593 0.00494 0.00143 0.0026 0.7176 0.8861
1.750 0.1846 0.00507 0.00146 0.0033 0.6854 0.8933
2.000 0.2091 0.00527 0.00152 0.0041 0.6382 0.8994
2.250 0.2327 0.00553 0.00160 0.0050 0.5843 0.9064
2.500 0.2546 0.00594 0.00172 0.0062 0.5048 0.9127
2.750 0.2763 0.00640 0.00189 0.0074 0.4204 0.9192
3.000 0.2972 0.00692 0.00206 0.0087 0.3322 0.9260
3.250 0.3199 0.00740 0.00227 0.0096 0.2591 0.9315
3.500 0.3429 0.00777 0.00245 0.0105 0.2097 0.9378
3.750 0.3672 0.00809 0.00261 0.0111 0.1719 0.9431
4.000 0.3919 0.00841 0.00280 0.0117 0.1383 0.9480
4.250 0.4155 0.00870 0.00298 0.0126 0.1123 0.9539
4.500 0.4412 0.00897 0.00317 0.0130 0.0937 0.9581
4.750 0.4680 0.00927 0.00339 0.0131 0.0784 0.9619
5.000 0.4939 0.00956 0.00362 0.0134 0.0630 0.9665
5.250 0.5190 0.00986 0.00384 0.0139 0.0516 0.9709
5.500 0.5496 0.01020 0.00413 0.0131 0.0450 0.9730
5.750 0.5811 0.01047 0.00440 0.0122 0.0425 0.9750
6.000 0.6117 0.01079 0.00470 0.0114 0.0401 0.9773
6.250 0.6406 0.01120 0.00512 0.0109 0.0380 0.9802
6.500 0.6693 0.01146 0.00541 0.0106 0.0372 0.9830
6.750 0.7032 0.01176 0.00572 0.0090 0.0360 0.9838
7.000 0.7363 0.01209 0.00606 0.0076 0.0348 0.9846
7.250 0.7686 0.01249 0.00646 0.0063 0.0337 0.9857
7.500 0.7989 0.01305 0.00704 0.0054 0.0325 0.9871
7.750 0.8286 0.01360 0.00764 0.0046 0.0316 0.9888
8.000 0.8593 0.01392 0.00798 0.0036 0.0310 0.9907
8.250 0.8882 0.01431 0.00841 0.0031 0.0304 0.9927
8.500 0.9179 0.01471 0.00884 0.0023 0.0296 0.9942
8.750 0.9492 0.01510 0.00924 0.0011 0.0288 0.9951
9.000 0.9796 0.01555 0.00970 0.0001 0.0280 0.9962
9.250 1.0073 0.01631 0.01049 -0.0005 0.0271 0.9976
9.500 1.0336 0.01723 0.01148 -0.0009 0.0263 0.9990
9.750 1.0637 0.01753 0.01183 -0.0018 0.0259 1.0000
10.000 1.0769 0.01782 0.01216 0.0009 0.0254 1.0000
10.250 1.0891 0.01815 0.01254 0.0037 0.0249 1.0000
10.500 1.1007 0.01851 0.01293 0.0066 0.0244 1.0000
10.750 1.1120 0.01886 0.01332 0.0096 0.0240 1.0000
11.000 1.1233 0.01922 0.01371 0.0125 0.0236 1.0000
11.250 1.1349 0.01960 0.01411 0.0153 0.0231 1.0000
11.500 1.1450 0.02016 0.01469 0.0182 0.0226 1.0000
11.750 1.1457 0.02139 0.01601 0.0226 0.0219 1.0000
12.000 1.1592 0.02165 0.01632 0.0250 0.0217 1.0000
12.250 1.1733 0.02206 0.01679 0.0270 0.0214 1.0000
12.500 1.1876 0.02257 0.01738 0.0289 0.0209 1.0000
12.750 1.2018 0.02315 0.01802 0.0307 0.0205 1.0000
13.000 1.2161 0.02374 0.01868 0.0324 0.0201 1.0000
13.250 1.2304 0.02435 0.01933 0.0339 0.0197 1.0000
13.500 1.2449 0.02494 0.01996 0.0353 0.0193 1.0000
13.750 1.2583 0.02564 0.02069 0.0367 0.0189 1.0000
14.000 1.2665 0.02676 0.02186 0.0386 0.0184 1.0000
14.250 1.2688 0.02846 0.02367 0.0408 0.0180 1.0000
14.500 1.2821 0.02925 0.02455 0.0419 0.0177 1.0000
14.750 1.2930 0.03030 0.02569 0.0430 0.0174 1.0000
15.000 1.3026 0.03146 0.02695 0.0442 0.0171 1.0000
15.250 1.3113 0.03275 0.02832 0.0452 0.0168 1.0000
15.500 1.3197 0.03411 0.02977 0.0460 0.0165 1.0000
15.750 1.3272 0.03559 0.03132 0.0468 0.0162 1.0000
16.000 1.3342 0.03718 0.03298 0.0473 0.0159 1.0000
16.250 1.3402 0.03895 0.03481 0.0477 0.0157 1.0000
16.500 1.3431 0.04110 0.03704 0.0479 0.0154 1.0000
16.750 1.3415 0.04384 0.03986 0.0479 0.0152 1.0000
17.000 1.3323 0.04763 0.04377 0.0474 0.0149 1.0000
17.250 1.3135 0.05287 0.04917 0.0460 0.0147 1.0000
17.500 1.3072 0.05697 0.05340 0.0444 0.0146 1.0000
17.750 1.2991 0.06160 0.05817 0.0423 0.0145 1.0000
18.000 1.2862 0.06720 0.06393 0.0394 0.0144 1.0000
18.250 1.2682 0.07399 0.07087 0.0357 0.0144 1.0000
18.500 1.2437 0.08221 0.07925 0.0311 0.0143 1.0000
18.750 1.2104 0.09223 0.08945 0.0254 0.0144 1.0000
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