NACA 16-015 (naca16015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 16-015 (naca16015-il) Reynolds number: 1,000,000 Max Cl/Cd: 50.48 at α=3.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca16015-il-1000000.txt Download as CSV file: xf-naca16015-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 16-015
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 -0.9715 0.10446 0.10192 -0.0603 1.0000 0.0088
-19.000 -1.0089 0.09381 0.09110 -0.0655 1.0000 0.0087
-18.750 -1.0414 0.08462 0.08174 -0.0697 1.0000 0.0087
-18.500 -1.0676 0.07711 0.07407 -0.0728 1.0000 0.0087
-18.250 -1.0868 0.07127 0.06808 -0.0746 1.0000 0.0087
-18.000 -1.1034 0.06630 0.06298 -0.0756 1.0000 0.0087
-17.750 -1.1177 0.06205 0.05860 -0.0758 1.0000 0.0088
-17.500 -1.1372 0.05754 0.05395 -0.0753 1.0000 0.0088
-17.250 -1.1599 0.05312 0.04936 -0.0739 1.0000 0.0089
-17.000 -1.1816 0.04923 0.04531 -0.0718 1.0000 0.0090
-16.750 -1.1972 0.04622 0.04218 -0.0693 1.0000 0.0092
-16.500 -1.2086 0.04381 0.03967 -0.0665 1.0000 0.0093
-16.250 -1.2162 0.04186 0.03763 -0.0636 1.0000 0.0094
-16.000 -1.2212 0.04023 0.03592 -0.0607 1.0000 0.0096
-15.750 -1.2190 0.03860 0.03421 -0.0590 0.9997 0.0097
-15.500 -1.2093 0.03702 0.03255 -0.0586 0.9991 0.0100
-15.250 -1.1998 0.03548 0.03091 -0.0580 0.9983 0.0102
-15.000 -1.1890 0.03408 0.02941 -0.0574 0.9976 0.0104
-14.750 -1.1769 0.03276 0.02800 -0.0568 0.9968 0.0107
-14.500 -1.1640 0.03146 0.02659 -0.0563 0.9960 0.0109
-14.250 -1.1488 0.03034 0.02537 -0.0559 0.9954 0.0112
-14.000 -1.1319 0.02935 0.02428 -0.0557 0.9948 0.0114
-13.750 -1.1192 0.02800 0.02281 -0.0549 0.9943 0.0117
-13.500 -1.1118 0.02653 0.02124 -0.0530 0.9930 0.0121
-13.250 -1.0970 0.02564 0.02030 -0.0520 0.9915 0.0125
-13.000 -1.0782 0.02493 0.01954 -0.0516 0.9901 0.0129
-12.750 -1.0581 0.02425 0.01882 -0.0514 0.9890 0.0134
-12.500 -1.0371 0.02360 0.01811 -0.0513 0.9880 0.0139
-12.250 -1.0149 0.02302 0.01746 -0.0514 0.9871 0.0144
-12.000 -0.9908 0.02256 0.01693 -0.0517 0.9864 0.0147
-11.750 -0.9751 0.02136 0.01566 -0.0508 0.9856 0.0157
-11.500 -0.9505 0.02084 0.01513 -0.0513 0.9850 0.0164
-11.250 -0.9248 0.02035 0.01461 -0.0519 0.9845 0.0171
-11.000 -0.8986 0.01988 0.01410 -0.0526 0.9841 0.0179
-10.750 -0.8714 0.01948 0.01364 -0.0534 0.9837 0.0185
-10.500 -0.8632 0.01882 0.01292 -0.0501 0.9797 0.0192
-10.250 -0.8422 0.01822 0.01232 -0.0496 0.9780 0.0203
-10.000 -0.8160 0.01788 0.01197 -0.0501 0.9769 0.0214
-9.750 -0.7892 0.01751 0.01157 -0.0507 0.9759 0.0224
-9.500 -0.7614 0.01718 0.01121 -0.0515 0.9752 0.0232
-9.250 -0.7382 0.01643 0.01040 -0.0515 0.9745 0.0246
-9.000 -0.7113 0.01592 0.00990 -0.0521 0.9739 0.0260
-8.750 -0.6825 0.01556 0.00952 -0.0531 0.9734 0.0274
-8.500 -0.6538 0.01521 0.00915 -0.0540 0.9728 0.0286
-8.250 -0.6249 0.01491 0.00882 -0.0549 0.9721 0.0293
-8.000 -0.6012 0.01424 0.00811 -0.0548 0.9713 0.0314
-7.750 -0.5914 0.01399 0.00785 -0.0514 0.9663 0.0328
-7.500 -0.5675 0.01367 0.00751 -0.0511 0.9644 0.0344
-7.250 -0.5420 0.01335 0.00717 -0.0511 0.9628 0.0358
-7.000 -0.5160 0.01305 0.00684 -0.0513 0.9615 0.0369
-6.750 -0.4917 0.01260 0.00638 -0.0511 0.9602 0.0404
-6.500 -0.4656 0.01227 0.00606 -0.0512 0.9590 0.0433
-6.250 -0.4421 0.01203 0.00580 -0.0507 0.9571 0.0466
-6.000 -0.4271 0.01176 0.00558 -0.0483 0.9531 0.0542
-5.750 -0.4079 0.01138 0.00530 -0.0469 0.9504 0.0738
-5.500 -0.3872 0.01094 0.00499 -0.0458 0.9483 0.1042
-5.250 -0.3661 0.01046 0.00469 -0.0449 0.9464 0.1445
-5.000 -0.3459 0.00997 0.00439 -0.0438 0.9446 0.1936
-4.750 -0.3351 0.00954 0.00421 -0.0406 0.9407 0.2519
-4.500 -0.3251 0.00899 0.00395 -0.0372 0.9366 0.3248
-4.250 -0.3151 0.00829 0.00360 -0.0338 0.9335 0.4155
-4.000 -0.3081 0.00755 0.00323 -0.0297 0.9306 0.5125
-3.750 -0.3153 0.00707 0.00306 -0.0221 0.9246 0.5897
-3.500 -0.3220 0.00661 0.00287 -0.0143 0.9196 0.6610
-3.250 -0.3157 0.00625 0.00271 -0.0095 0.9166 0.7202
-3.000 -0.3036 0.00615 0.00271 -0.0059 0.9132 0.7530
-2.750 -0.2894 0.00608 0.00272 -0.0029 0.9093 0.7766
-2.500 -0.2683 0.00600 0.00267 -0.0014 0.9067 0.7971
-2.250 -0.2427 0.00594 0.00262 -0.0010 0.9047 0.8115
-2.000 -0.2149 0.00590 0.00260 -0.0011 0.9031 0.8244
-1.750 -0.1861 0.00589 0.00261 -0.0014 0.9015 0.8363
-1.500 -0.1657 0.00596 0.00269 0.0003 0.8983 0.8472
-1.250 -0.1462 0.00604 0.00280 0.0022 0.8949 0.8596
-1.000 -0.1195 0.00613 0.00291 0.0025 0.8924 0.8691
-0.750 -0.0891 0.00616 0.00293 0.0018 0.8905 0.8742
-0.500 -0.0546 0.00619 0.00297 0.0001 0.8890 0.8772
-0.250 -0.0219 0.00620 0.00298 -0.0012 0.8873 0.8802
0.000 0.0000 0.00623 0.00300 0.0000 0.8840 0.8840
0.250 0.0219 0.00621 0.00298 0.0012 0.8802 0.8873
0.500 0.0546 0.00619 0.00297 -0.0001 0.8772 0.8890
0.750 0.0891 0.00615 0.00293 -0.0018 0.8742 0.8905
1.000 0.1194 0.00613 0.00291 -0.0025 0.8691 0.8924
1.250 0.1462 0.00604 0.00280 -0.0022 0.8596 0.8949
1.500 0.1657 0.00596 0.00270 -0.0003 0.8472 0.8983
1.750 0.1862 0.00589 0.00261 0.0014 0.8364 0.9015
2.000 0.2147 0.00590 0.00260 0.0011 0.8242 0.9031
2.250 0.2428 0.00594 0.00262 0.0010 0.8117 0.9047
2.500 0.2683 0.00600 0.00267 0.0014 0.7970 0.9067
2.750 0.2894 0.00608 0.00272 0.0029 0.7767 0.9093
3.000 0.3036 0.00614 0.00271 0.0059 0.7530 0.9132
3.250 0.3155 0.00625 0.00271 0.0095 0.7194 0.9166
3.500 0.3219 0.00662 0.00287 0.0143 0.6607 0.9196
3.750 0.3150 0.00708 0.00306 0.0222 0.5887 0.9246
4.000 0.3083 0.00755 0.00323 0.0296 0.5126 0.9306
4.250 0.3153 0.00829 0.00360 0.0338 0.4157 0.9335
4.500 0.3252 0.00899 0.00395 0.0372 0.3242 0.9366
4.750 0.3354 0.00954 0.00421 0.0405 0.2517 0.9406
5.000 0.3462 0.00997 0.00439 0.0437 0.1935 0.9446
5.250 0.3664 0.01045 0.00469 0.0448 0.1443 0.9464
5.500 0.3874 0.01094 0.00499 0.0458 0.1042 0.9483
5.750 0.4081 0.01138 0.00529 0.0468 0.0734 0.9504
6.000 0.4274 0.01176 0.00558 0.0482 0.0540 0.9531
6.250 0.4425 0.01203 0.00580 0.0506 0.0464 0.9571
6.500 0.4660 0.01227 0.00606 0.0511 0.0433 0.9590
6.750 0.4920 0.01259 0.00638 0.0510 0.0404 0.9602
7.000 0.5163 0.01305 0.00684 0.0512 0.0369 0.9615
7.250 0.5423 0.01334 0.00716 0.0511 0.0357 0.9628
7.500 0.5678 0.01366 0.00750 0.0510 0.0344 0.9644
7.750 0.5917 0.01399 0.00785 0.0513 0.0329 0.9664
8.000 0.6017 0.01424 0.00811 0.0548 0.0315 0.9713
8.250 0.6254 0.01491 0.00882 0.0548 0.0293 0.9722
8.500 0.6543 0.01521 0.00914 0.0539 0.0286 0.9728
8.750 0.6829 0.01556 0.00952 0.0530 0.0274 0.9734
9.000 0.7118 0.01592 0.00989 0.0521 0.0260 0.9740
9.250 0.7387 0.01642 0.01039 0.0514 0.0246 0.9745
9.500 0.7621 0.01716 0.01119 0.0513 0.0232 0.9753
9.750 0.7899 0.01750 0.01156 0.0506 0.0224 0.9760
10.000 0.8169 0.01786 0.01195 0.0499 0.0213 0.9769
10.250 0.8428 0.01822 0.01232 0.0495 0.0203 0.9781
10.500 0.8640 0.01879 0.01289 0.0499 0.0192 0.9798
10.750 0.8723 0.01947 0.01363 0.0532 0.0185 0.9837
11.000 0.8995 0.01987 0.01409 0.0524 0.0179 0.9841
11.250 0.9258 0.02034 0.01460 0.0517 0.0171 0.9846
11.500 0.9516 0.02082 0.01511 0.0511 0.0164 0.9851
11.750 0.9762 0.02135 0.01565 0.0506 0.0157 0.9856
12.000 0.9922 0.02253 0.01690 0.0514 0.0147 0.9864
12.250 1.0164 0.02298 0.01742 0.0511 0.0144 0.9872
12.500 1.0387 0.02355 0.01805 0.0510 0.0139 0.9881
12.750 1.0595 0.02422 0.01878 0.0511 0.0134 0.9891
13.000 1.0796 0.02491 0.01952 0.0513 0.0129 0.9903
13.250 1.0983 0.02563 0.02028 0.0518 0.0125 0.9916
13.500 1.1129 0.02651 0.02123 0.0528 0.0121 0.9932
13.750 1.1201 0.02806 0.02287 0.0547 0.0116 0.9943
14.000 1.1341 0.02930 0.02423 0.0553 0.0114 0.9949
14.250 1.1510 0.03030 0.02533 0.0555 0.0112 0.9954
14.500 1.1660 0.03144 0.02657 0.0559 0.0109 0.9961
14.750 1.1794 0.03269 0.02793 0.0564 0.0106 0.9969
15.000 1.1915 0.03401 0.02934 0.0570 0.0104 0.9977
15.250 1.2022 0.03542 0.03085 0.0576 0.0102 0.9984
15.500 1.2120 0.03695 0.03248 0.0582 0.0099 0.9992
15.750 1.2215 0.03855 0.03416 0.0586 0.0097 0.9998
16.000 1.2219 0.04013 0.03582 0.0607 0.0096 1.0000
16.250 1.2166 0.04179 0.03756 0.0636 0.0094 1.0000
16.500 1.2092 0.04371 0.03956 0.0665 0.0093 1.0000
16.750 1.1976 0.04613 0.04209 0.0693 0.0092 1.0000
17.000 1.1819 0.04915 0.04523 0.0718 0.0090 1.0000
17.250 1.1622 0.05283 0.04906 0.0739 0.0089 1.0000
17.500 1.1401 0.05716 0.05355 0.0753 0.0088 1.0000
17.750 1.1190 0.06184 0.05839 0.0758 0.0088 1.0000
18.000 1.1057 0.06597 0.06265 0.0756 0.0087 1.0000
18.250 1.0891 0.07094 0.06775 0.0747 0.0087 1.0000
18.500 1.0690 0.07691 0.07386 0.0728 0.0087 1.0000
18.750 1.0443 0.08419 0.08130 0.0698 0.0087 1.0000
19.000 1.0125 0.09328 0.09056 0.0656 0.0087 1.0000
19.250 0.9725 0.10444 0.10190 0.0602 0.0088 1.0000
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