NACA 23015 (naca23015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 23015 (naca23015-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.95 at α=10° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca23015-il-1000000.txt Download as CSV file: xf-naca23015-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 23015
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2974 0.08215 0.07855 -0.0362 0.9999 0.0175
-19.500 -1.3199 0.07517 0.07144 -0.0396 0.9999 0.0176
-19.250 -1.3391 0.06890 0.06504 -0.0426 0.9999 0.0178
-19.000 -1.3542 0.06338 0.05941 -0.0450 0.9999 0.0180
-18.750 -1.3652 0.05860 0.05453 -0.0469 0.9999 0.0182
-18.500 -1.3730 0.05443 0.05027 -0.0484 0.9999 0.0184
-18.250 -1.3781 0.05074 0.04649 -0.0495 0.9999 0.0186
-18.000 -1.3804 0.04750 0.04316 -0.0502 0.9999 0.0188
-17.750 -1.3807 0.04460 0.04018 -0.0507 0.9999 0.0191
-17.500 -1.3795 0.04198 0.03747 -0.0509 0.9999 0.0194
-17.250 -1.3768 0.03959 0.03499 -0.0509 0.9999 0.0197
-17.000 -1.3727 0.03745 0.03276 -0.0506 0.9999 0.0200
-16.750 -1.3669 0.03557 0.03078 -0.0502 0.9999 0.0203
-16.500 -1.3659 0.03334 0.02847 -0.0495 0.9999 0.0207
-16.250 -1.3627 0.03142 0.02649 -0.0485 0.9999 0.0211
-16.000 -1.3557 0.02993 0.02496 -0.0475 0.9999 0.0216
-15.750 -1.3467 0.02867 0.02365 -0.0463 0.9999 0.0220
-15.500 -1.3364 0.02756 0.02248 -0.0450 0.9999 0.0225
-15.250 -1.3256 0.02654 0.02139 -0.0436 0.9999 0.0231
-15.000 -1.3135 0.02566 0.02044 -0.0421 0.9999 0.0235
-14.750 -1.3082 0.02442 0.01916 -0.0399 0.9999 0.0241
-14.500 -1.2981 0.02356 0.01827 -0.0379 0.9999 0.0247
-14.250 -1.2867 0.02286 0.01754 -0.0359 0.9999 0.0253
-14.000 -1.2754 0.02223 0.01686 -0.0336 0.9999 0.0259
-13.750 -1.2623 0.02167 0.01624 -0.0315 0.9999 0.0265
-13.500 -1.2461 0.02112 0.01563 -0.0299 0.9999 0.0271
-13.250 -1.2316 0.02042 0.01493 -0.0281 0.9999 0.0279
-13.000 -1.2125 0.01997 0.01447 -0.0269 0.9999 0.0286
-12.750 -1.1922 0.01958 0.01405 -0.0257 0.9999 0.0294
-12.500 -1.1709 0.01923 0.01366 -0.0247 0.9999 0.0303
-12.250 -1.1507 0.01876 0.01315 -0.0236 0.9999 0.0311
-12.000 -1.1304 0.01828 0.01268 -0.0225 0.9999 0.0320
-11.750 -1.1076 0.01798 0.01237 -0.0217 0.9999 0.0328
-11.500 -1.0846 0.01767 0.01204 -0.0209 0.9999 0.0337
-11.250 -1.0611 0.01738 0.01171 -0.0202 0.9999 0.0345
-11.000 -1.0391 0.01694 0.01123 -0.0193 0.9999 0.0353
-10.750 -1.0167 0.01652 0.01083 -0.0184 0.9999 0.0362
-10.500 -0.9923 0.01628 0.01060 -0.0178 0.9999 0.0371
-10.250 -0.9679 0.01603 0.01034 -0.0172 0.9999 0.0381
-10.000 -0.9435 0.01579 0.01007 -0.0165 0.9999 0.0389
-9.750 -0.9192 0.01554 0.00978 -0.0159 0.9999 0.0396
-9.500 -0.8978 0.01500 0.00926 -0.0148 0.9999 0.0407
-9.250 -0.8741 0.01477 0.00905 -0.0141 0.9999 0.0416
-9.000 -0.8512 0.01456 0.00884 -0.0131 0.9999 0.0425
-8.750 -0.8293 0.01435 0.00862 -0.0120 0.9999 0.0434
-8.500 -0.8080 0.01420 0.00845 -0.0107 0.9999 0.0442
-8.250 -0.7894 0.01392 0.00815 -0.0090 0.9999 0.0450
-8.000 -0.7605 0.01347 0.00772 -0.0093 0.9986 0.0463
-7.750 -0.7274 0.01319 0.00745 -0.0104 0.9968 0.0474
-7.500 -0.6939 0.01292 0.00719 -0.0114 0.9951 0.0487
-7.250 -0.6598 0.01268 0.00694 -0.0126 0.9936 0.0498
-7.000 -0.6274 0.01233 0.00657 -0.0135 0.9909 0.0509
-6.750 -0.5965 0.01190 0.00616 -0.0141 0.9861 0.0525
-6.500 -0.5642 0.01164 0.00591 -0.0149 0.9815 0.0538
-6.250 -0.5362 0.01142 0.00568 -0.0148 0.9718 0.0551
-6.000 -0.5094 0.01124 0.00549 -0.0143 0.9606 0.0562
-5.750 -0.4841 0.01107 0.00529 -0.0136 0.9477 0.0573
-5.500 -0.4600 0.01076 0.00496 -0.0126 0.9337 0.0592
-5.250 -0.4350 0.01058 0.00476 -0.0118 0.9190 0.0608
-5.000 -0.4092 0.01043 0.00457 -0.0112 0.9031 0.0624
-4.750 -0.3828 0.01031 0.00440 -0.0107 0.8868 0.0640
-4.500 -0.3565 0.01012 0.00416 -0.0102 0.8699 0.0664
-4.250 -0.3300 0.00997 0.00397 -0.0097 0.8501 0.0691
-4.000 -0.3033 0.00988 0.00381 -0.0093 0.8279 0.0717
-3.750 -0.2764 0.00977 0.00363 -0.0089 0.8056 0.0757
-3.500 -0.2491 0.00966 0.00347 -0.0086 0.7835 0.0816
-3.250 -0.2220 0.00947 0.00331 -0.0084 0.7632 0.0978
-3.000 -0.1966 0.00886 0.00302 -0.0081 0.7446 0.1936
-2.750 -0.1720 0.00807 0.00276 -0.0078 0.7266 0.3447
-2.500 -0.1452 0.00778 0.00265 -0.0076 0.7066 0.4114
-2.250 -0.1179 0.00760 0.00258 -0.0075 0.6860 0.4613
-2.000 -0.0903 0.00748 0.00252 -0.0074 0.6660 0.4993
-1.750 -0.0626 0.00739 0.00248 -0.0072 0.6446 0.5355
-1.500 -0.0350 0.00732 0.00244 -0.0071 0.6217 0.5706
-1.250 -0.0074 0.00726 0.00242 -0.0070 0.5994 0.6075
-0.750 0.0481 0.00719 0.00242 -0.0067 0.5585 0.6742
-0.500 0.0759 0.00719 0.00243 -0.0066 0.5377 0.7004
-0.250 0.1038 0.00721 0.00244 -0.0065 0.5163 0.7244
0.000 0.1317 0.00725 0.00247 -0.0063 0.4955 0.7467
0.250 0.1593 0.00728 0.00250 -0.0062 0.4761 0.7716
0.500 0.1871 0.00733 0.00254 -0.0060 0.4569 0.7920
0.750 0.2146 0.00738 0.00259 -0.0058 0.4378 0.8135
1.000 0.2419 0.00745 0.00265 -0.0056 0.4181 0.8350
1.250 0.2693 0.00755 0.00271 -0.0053 0.3982 0.8515
1.500 0.2967 0.00765 0.00277 -0.0051 0.3798 0.8666
1.750 0.3240 0.00776 0.00284 -0.0049 0.3625 0.8816
2.000 0.3507 0.00786 0.00292 -0.0045 0.3459 0.8965
2.250 0.3772 0.00798 0.00301 -0.0041 0.3299 0.9104
2.500 0.4036 0.00812 0.00309 -0.0037 0.3138 0.9237
2.750 0.4296 0.00826 0.00319 -0.0032 0.2980 0.9371
3.000 0.4550 0.00841 0.00328 -0.0025 0.2834 0.9491
3.250 0.4812 0.00853 0.00336 -0.0021 0.2716 0.9600
3.500 0.5082 0.00866 0.00345 -0.0018 0.2614 0.9704
3.750 0.5371 0.00883 0.00356 -0.0019 0.2515 0.9786
4.000 0.5686 0.00897 0.00367 -0.0026 0.2441 0.9844
4.250 0.6011 0.00916 0.00381 -0.0036 0.2363 0.9887
4.500 0.6336 0.00934 0.00396 -0.0045 0.2305 0.9927
4.750 0.6681 0.00951 0.00411 -0.0059 0.2251 0.9941
5.000 0.7021 0.00974 0.00429 -0.0072 0.2182 0.9956
5.250 0.7362 0.00991 0.00445 -0.0085 0.2137 0.9973
5.500 0.7700 0.01008 0.00461 -0.0097 0.2094 0.9991
5.750 0.7992 0.01026 0.00476 -0.0101 0.2047 1.0001
6.000 0.8202 0.01041 0.00488 -0.0089 0.1997 1.0001
6.250 0.8432 0.01047 0.00495 -0.0080 0.1971 1.0001
6.500 0.8667 0.01057 0.00505 -0.0073 0.1935 1.0001
6.750 0.8907 0.01073 0.00518 -0.0067 0.1894 1.0001
7.000 0.9150 0.01097 0.00538 -0.0061 0.1843 1.0001
7.250 0.9411 0.01107 0.00550 -0.0058 0.1816 1.0001
7.500 0.9671 0.01122 0.00565 -0.0056 0.1778 1.0001
7.750 0.9928 0.01142 0.00583 -0.0053 0.1735 1.0001
8.000 1.0183 0.01167 0.00606 -0.0050 0.1691 1.0001
8.250 1.0448 0.01180 0.00622 -0.0049 0.1663 1.0001
8.500 1.0708 0.01199 0.00641 -0.0047 0.1626 1.0001
8.750 1.0962 0.01224 0.00663 -0.0044 0.1581 1.0001
9.000 1.1218 0.01247 0.00687 -0.0042 0.1543 1.0001
9.250 1.1476 0.01266 0.00707 -0.0039 0.1504 1.0001
9.500 1.1726 0.01292 0.00731 -0.0036 0.1452 1.0001
9.750 1.1975 0.01318 0.00757 -0.0033 0.1404 1.0001
10.000 1.2224 0.01344 0.00782 -0.0030 0.1351 1.0001
10.250 1.2462 0.01378 0.00813 -0.0026 0.1291 1.0001
10.500 1.2704 0.01406 0.00842 -0.0022 0.1232 1.0001
10.750 1.2933 0.01445 0.00877 -0.0016 0.1164 1.0001
11.000 1.3157 0.01485 0.00915 -0.0010 0.1092 1.0001
11.250 1.3375 0.01527 0.00955 -0.0003 0.1024 1.0001
11.500 1.3579 0.01578 0.01003 0.0005 0.0954 1.0001
11.750 1.3778 0.01630 0.01052 0.0015 0.0892 1.0001
12.000 1.3972 0.01680 0.01102 0.0025 0.0839 1.0001
12.250 1.4146 0.01741 0.01161 0.0037 0.0788 1.0001
12.500 1.4329 0.01791 0.01213 0.0049 0.0750 1.0001
12.750 1.4480 0.01857 0.01278 0.0065 0.0711 1.0001
13.000 1.4636 0.01914 0.01338 0.0080 0.0683 1.0001
13.250 1.4752 0.01979 0.01405 0.0101 0.0656 1.0001
13.500 1.4811 0.02065 0.01494 0.0129 0.0630 1.0001
13.750 1.4918 0.02137 0.01571 0.0150 0.0613 1.0001
14.000 1.5017 0.02221 0.01659 0.0169 0.0595 1.0001
14.250 1.5095 0.02325 0.01766 0.0188 0.0577 1.0001
14.500 1.5141 0.02457 0.01902 0.0208 0.0559 1.0001
14.750 1.5250 0.02555 0.02007 0.0221 0.0549 1.0001
15.000 1.5338 0.02674 0.02132 0.0233 0.0538 1.0001
15.250 1.5405 0.02814 0.02278 0.0245 0.0527 1.0001
15.500 1.5450 0.02983 0.02452 0.0256 0.0516 1.0001
15.750 1.5460 0.03193 0.02668 0.0265 0.0504 1.0001
16.000 1.5477 0.03410 0.02893 0.0271 0.0495 1.0001
16.250 1.5540 0.03592 0.03083 0.0275 0.0487 1.0001
16.500 1.5578 0.03806 0.03305 0.0276 0.0479 1.0001
16.750 1.5586 0.04061 0.03568 0.0276 0.0470 1.0001
17.000 1.5564 0.04360 0.03875 0.0274 0.0462 1.0001
17.250 1.5504 0.04712 0.04235 0.0268 0.0456 1.0001
17.500 1.5399 0.05135 0.04667 0.0259 0.0449 1.0001
17.750 1.5239 0.05647 0.05191 0.0244 0.0443 1.0001
18.000 1.5142 0.06086 0.05641 0.0231 0.0440 1.0001
18.250 1.5045 0.06537 0.06104 0.0217 0.0436 1.0001
18.500 1.4921 0.07034 0.06612 0.0200 0.0433 1.0001
18.750 1.4758 0.07591 0.07181 0.0180 0.0429 1.0001
19.000 1.4587 0.08167 0.07769 0.0158 0.0426 1.0001
19.250 1.4393 0.08789 0.08402 0.0133 0.0423 1.0001
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