NACA 23015 (naca23015-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 23015 (naca23015-il) Reynolds number: 100,000 Max Cl/Cd: 39.14 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca23015-il-100000-n5.txt Download as CSV file: xf-naca23015-il-100000-n5.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 = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.7511 0.08649 0.08040 -0.0387 1.0000 0.0465
-13.500 -0.7924 0.07680 0.07049 -0.0452 1.0000 0.0463
-13.250 -0.8281 0.06954 0.06296 -0.0490 1.0000 0.0463
-13.000 -0.8606 0.06381 0.05694 -0.0505 1.0000 0.0464
-12.750 -0.8913 0.05917 0.05196 -0.0500 1.0000 0.0467
-12.500 -0.8965 0.05673 0.04943 -0.0487 1.0000 0.0472
-12.250 -0.8938 0.05500 0.04768 -0.0473 1.0000 0.0479
-12.000 -0.8955 0.05315 0.04573 -0.0453 1.0000 0.0486
-11.750 -0.9011 0.05115 0.04358 -0.0425 1.0000 0.0494
-11.500 -0.9057 0.04895 0.04116 -0.0396 1.0000 0.0503
-11.250 -0.9091 0.04659 0.03848 -0.0367 1.0000 0.0513
-11.000 -0.9123 0.04421 0.03569 -0.0334 1.0000 0.0524
-10.750 -0.9073 0.04227 0.03350 -0.0309 1.0000 0.0536
-10.500 -0.8929 0.04100 0.03222 -0.0295 1.0000 0.0547
-10.250 -0.8802 0.03967 0.03080 -0.0276 1.0000 0.0560
-10.000 -0.8685 0.03820 0.02915 -0.0255 1.0000 0.0573
-9.750 -0.8576 0.03672 0.02740 -0.0232 1.0000 0.0589
-9.500 -0.8463 0.03528 0.02566 -0.0207 1.0000 0.0605
-9.250 -0.8287 0.03407 0.02449 -0.0193 1.0000 0.0617
-9.000 -0.8119 0.03299 0.02337 -0.0177 1.0000 0.0631
-8.750 -0.7955 0.03196 0.02225 -0.0159 1.0000 0.0648
-8.500 -0.7789 0.03094 0.02109 -0.0141 1.0000 0.0666
-8.250 -0.7623 0.02997 0.01992 -0.0122 1.0000 0.0683
-8.000 -0.7435 0.02890 0.01891 -0.0108 1.0000 0.0697
-7.750 -0.7261 0.02806 0.01811 -0.0091 1.0000 0.0713
-7.500 -0.7091 0.02731 0.01733 -0.0073 1.0000 0.0733
-7.250 -0.6922 0.02658 0.01655 -0.0054 1.0000 0.0752
-7.000 -0.6752 0.02590 0.01578 -0.0035 1.0000 0.0770
-6.750 -0.6591 0.02514 0.01508 -0.0016 1.0000 0.0787
-6.500 -0.6440 0.02450 0.01451 0.0004 1.0000 0.0807
-6.250 -0.6279 0.02393 0.01396 0.0022 0.9997 0.0831
-6.000 -0.5908 0.02323 0.01322 0.0000 0.9937 0.0865
-5.750 -0.5561 0.02246 0.01249 -0.0018 0.9865 0.0898
-5.500 -0.5204 0.02180 0.01185 -0.0037 0.9795 0.0945
-5.000 -0.4516 0.02053 0.01060 -0.0070 0.9629 0.1060
-4.750 -0.4142 0.01989 0.01000 -0.0091 0.9557 0.1163
-4.500 -0.3826 0.01921 0.00942 -0.0101 0.9454 0.1330
-4.250 -0.3506 0.01811 0.00875 -0.0114 0.9369 0.1922
-4.000 -0.3274 0.01682 0.00835 -0.0111 0.9252 0.3604
-3.750 -0.3004 0.01627 0.00816 -0.0108 0.9130 0.4445
-3.500 -0.2690 0.01586 0.00798 -0.0111 0.9026 0.5082
-3.250 -0.2405 0.01556 0.00786 -0.0107 0.8893 0.5546
-3.000 -0.2128 0.01533 0.00777 -0.0101 0.8752 0.5994
-2.750 -0.1842 0.01513 0.00770 -0.0094 0.8613 0.6428
-2.500 -0.1547 0.01499 0.00765 -0.0088 0.8474 0.6811
-2.250 -0.1259 0.01490 0.00762 -0.0080 0.8322 0.7145
-2.000 -0.0973 0.01485 0.00759 -0.0072 0.8154 0.7404
-1.750 -0.0678 0.01481 0.00751 -0.0067 0.7982 0.7607
-1.500 -0.0382 0.01477 0.00741 -0.0063 0.7800 0.7778
-1.250 -0.0090 0.01475 0.00729 -0.0058 0.7595 0.7947
-0.750 0.0500 0.01482 0.00715 -0.0049 0.7134 0.8256
-0.500 0.0802 0.01491 0.00713 -0.0047 0.6901 0.8398
-0.250 0.1100 0.01501 0.00711 -0.0045 0.6676 0.8542
0.000 0.1389 0.01512 0.00710 -0.0041 0.6454 0.8689
0.250 0.1714 0.01528 0.00713 -0.0045 0.6226 0.8807
0.500 0.2033 0.01544 0.00717 -0.0049 0.5987 0.8925
0.750 0.2328 0.01559 0.00719 -0.0049 0.5755 0.9055
1.000 0.2679 0.01580 0.00725 -0.0060 0.5516 0.9150
1.250 0.3002 0.01600 0.00731 -0.0066 0.5281 0.9257
1.500 0.3337 0.01621 0.00738 -0.0076 0.5045 0.9359
1.750 0.3703 0.01643 0.00746 -0.0093 0.4805 0.9440
2.000 0.4037 0.01666 0.00754 -0.0104 0.4580 0.9539
2.250 0.4428 0.01688 0.00764 -0.0128 0.4350 0.9606
2.500 0.4770 0.01712 0.00776 -0.0143 0.4139 0.9696
2.750 0.5155 0.01735 0.00787 -0.0166 0.3927 0.9762
3.000 0.5515 0.01761 0.00801 -0.0186 0.3736 0.9838
3.250 0.5890 0.01786 0.00816 -0.0209 0.3563 0.9905
3.500 0.6265 0.01812 0.00833 -0.0232 0.3408 0.9967
3.750 0.6554 0.01840 0.00850 -0.0239 0.3281 1.0000
4.000 0.6745 0.01864 0.00871 -0.0225 0.3172 1.0000
4.250 0.6934 0.01892 0.00892 -0.0211 0.3081 1.0000
4.500 0.7124 0.01921 0.00917 -0.0197 0.2996 1.0000
4.750 0.7311 0.01954 0.00944 -0.0183 0.2923 1.0000
5.000 0.7503 0.01985 0.00975 -0.0168 0.2846 1.0000
5.250 0.7688 0.02022 0.01004 -0.0153 0.2781 1.0000
5.500 0.7881 0.02056 0.01041 -0.0139 0.2715 1.0000
5.750 0.8072 0.02094 0.01078 -0.0125 0.2655 1.0000
6.000 0.8260 0.02137 0.01112 -0.0110 0.2605 1.0000
6.250 0.8455 0.02176 0.01158 -0.0096 0.2548 1.0000
6.500 0.8646 0.02218 0.01201 -0.0082 0.2492 1.0000
6.750 0.8837 0.02263 0.01241 -0.0069 0.2445 1.0000
7.000 0.9031 0.02311 0.01293 -0.0055 0.2396 1.0000
7.250 0.9221 0.02357 0.01345 -0.0041 0.2342 1.0000
7.500 0.9410 0.02404 0.01391 -0.0027 0.2294 1.0000
7.750 0.9602 0.02458 0.01442 -0.0014 0.2250 1.0000
8.000 0.9785 0.02509 0.01506 0.0000 0.2197 1.0000
8.250 0.9971 0.02560 0.01560 0.0014 0.2148 1.0000
8.500 1.0163 0.02616 0.01609 0.0026 0.2105 1.0000
8.750 1.0338 0.02674 0.01684 0.0041 0.2054 1.0000
9.000 1.0513 0.02729 0.01748 0.0055 0.2001 1.0000
9.250 1.0692 0.02784 0.01801 0.0068 0.1956 1.0000
9.500 1.0859 0.02848 0.01875 0.0083 0.1908 1.0000
9.750 1.1015 0.02911 0.01952 0.0098 0.1854 1.0000
10.000 1.1174 0.02968 0.02011 0.0113 0.1807 1.0000
10.250 1.1323 0.03037 0.02086 0.0129 0.1762 1.0000
10.500 1.1450 0.03109 0.02177 0.0147 0.1708 1.0000
10.750 1.1577 0.03174 0.02245 0.0165 0.1662 1.0000
11.000 1.1687 0.03248 0.02324 0.0184 0.1620 1.0000
11.250 1.1759 0.03336 0.02431 0.0208 0.1569 1.0000
11.500 1.1836 0.03418 0.02520 0.0230 0.1525 1.0000
11.750 1.1914 0.03510 0.02615 0.0249 0.1486 1.0000
12.000 1.1964 0.03636 0.02761 0.0267 0.1436 1.0000
12.250 1.2017 0.03754 0.02888 0.0284 0.1393 1.0000
12.500 1.2069 0.03882 0.03018 0.0298 0.1357 1.0000
12.750 1.2086 0.04062 0.03220 0.0310 0.1310 1.0000
13.000 1.2107 0.04237 0.03405 0.0319 0.1271 1.0000
13.250 1.2134 0.04411 0.03577 0.0326 0.1240 1.0000
13.500 1.2106 0.04673 0.03863 0.0330 0.1199 1.0000
13.750 1.2081 0.04936 0.04139 0.0331 0.1164 1.0000
14.000 1.2062 0.05197 0.04406 0.0329 0.1136 1.0000
14.250 1.2011 0.05520 0.04740 0.0325 0.1107 1.0000
14.500 1.1912 0.05923 0.05163 0.0314 0.1077 1.0000
14.750 1.1818 0.06331 0.05584 0.0301 0.1051 1.0000
15.000 1.1744 0.06720 0.05979 0.0288 0.1029 1.0000
15.250 1.1661 0.07135 0.06400 0.0273 0.1008 1.0000
15.500 1.1412 0.07839 0.07128 0.0242 0.0987 1.0000
15.750 1.1127 0.08632 0.07942 0.0204 0.0967 1.0000
16.000 1.0841 0.09463 0.08788 0.0162 0.0947 1.0000
16.250 1.0773 0.09920 0.09248 0.0142 0.0926 1.0000
16.500 1.0644 0.10498 0.09830 0.0116 0.0908 1.0000
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