NACA 63-015A AIRFOIL (n63015a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63-015A AIRFOIL (n63015a-il) Reynolds number: 1,000,000 Max Cl/Cd: 66.87 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n63015a-il-1000000-n5.txt Download as CSV file: xf-n63015a-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63-015A AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1886 0.11333 0.11008 -0.0016 1.0000 0.0091
-19.500 -1.2064 0.10639 0.10301 -0.0050 1.0000 0.0092
-19.250 -1.2241 0.09963 0.09614 -0.0081 1.0000 0.0092
-19.000 -1.2404 0.09331 0.08970 -0.0110 1.0000 0.0093
-18.750 -1.2547 0.08737 0.08365 -0.0136 1.0000 0.0093
-18.500 -1.2681 0.08173 0.07790 -0.0160 1.0000 0.0094
-18.250 -1.2798 0.07652 0.07258 -0.0181 1.0000 0.0094
-18.000 -1.2895 0.07168 0.06763 -0.0199 1.0000 0.0095
-17.750 -1.2975 0.06720 0.06305 -0.0215 1.0000 0.0096
-17.500 -1.3042 0.06304 0.05879 -0.0229 1.0000 0.0096
-17.250 -1.3092 0.05921 0.05487 -0.0240 1.0000 0.0097
-17.000 -1.3127 0.05564 0.05121 -0.0250 1.0000 0.0097
-16.750 -1.3148 0.05237 0.04785 -0.0257 1.0000 0.0098
-16.500 -1.3157 0.04936 0.04475 -0.0263 1.0000 0.0099
-16.250 -1.3156 0.04653 0.04184 -0.0267 1.0000 0.0099
-16.000 -1.3143 0.04392 0.03915 -0.0269 1.0000 0.0100
-15.750 -1.3119 0.04151 0.03666 -0.0270 1.0000 0.0101
-15.500 -1.3081 0.03927 0.03434 -0.0270 1.0000 0.0102
-15.250 -1.3034 0.03717 0.03217 -0.0269 1.0000 0.0102
-15.000 -1.2977 0.03523 0.03015 -0.0267 1.0000 0.0103
-14.750 -1.2910 0.03340 0.02825 -0.0264 1.0000 0.0104
-14.500 -1.2834 0.03169 0.02647 -0.0260 1.0000 0.0105
-14.250 -1.2750 0.03011 0.02482 -0.0256 1.0000 0.0106
-14.000 -1.2654 0.02864 0.02328 -0.0251 1.0000 0.0107
-13.750 -1.2550 0.02730 0.02188 -0.0245 1.0000 0.0109
-13.500 -1.2438 0.02605 0.02057 -0.0238 1.0000 0.0110
-13.250 -1.2320 0.02489 0.01934 -0.0231 1.0000 0.0111
-13.000 -1.2199 0.02380 0.01820 -0.0223 1.0000 0.0113
-12.750 -1.2072 0.02278 0.01712 -0.0214 1.0000 0.0114
-12.500 -1.1940 0.02185 0.01613 -0.0204 1.0000 0.0114
-12.250 -1.1801 0.02100 0.01523 -0.0193 1.0000 0.0115
-12.000 -1.1657 0.02023 0.01440 -0.0182 1.0000 0.0116
-11.750 -1.1516 0.01947 0.01359 -0.0169 1.0000 0.0117
-11.500 -1.1384 0.01870 0.01278 -0.0153 1.0000 0.0120
-11.250 -1.1241 0.01804 0.01208 -0.0137 1.0000 0.0122
-11.000 -1.1091 0.01746 0.01148 -0.0121 1.0000 0.0125
-10.750 -1.0938 0.01695 0.01094 -0.0104 1.0000 0.0127
-10.500 -1.0767 0.01648 0.01043 -0.0089 1.0000 0.0130
-10.250 -1.0586 0.01603 0.00996 -0.0076 1.0000 0.0133
-10.000 -1.0380 0.01559 0.00951 -0.0067 0.9977 0.0136
-9.750 -1.0086 0.01513 0.00902 -0.0077 0.9861 0.0141
-9.500 -0.9784 0.01470 0.00855 -0.0088 0.9723 0.0145
-9.250 -0.9513 0.01424 0.00806 -0.0092 0.9523 0.0154
-9.000 -0.9282 0.01388 0.00765 -0.0086 0.9281 0.0162
-8.750 -0.9065 0.01358 0.00727 -0.0076 0.9033 0.0171
-8.500 -0.8841 0.01332 0.00691 -0.0068 0.8813 0.0180
-8.250 -0.8614 0.01302 0.00655 -0.0060 0.8620 0.0195
-8.000 -0.8379 0.01275 0.00622 -0.0055 0.8450 0.0213
-7.500 -0.7895 0.01222 0.00559 -0.0045 0.8162 0.0258
-7.250 -0.7647 0.01197 0.00530 -0.0042 0.8043 0.0284
-7.000 -0.7398 0.01172 0.00502 -0.0038 0.7935 0.0319
-6.750 -0.7148 0.01146 0.00475 -0.0035 0.7830 0.0363
-6.500 -0.6895 0.01121 0.00449 -0.0032 0.7741 0.0419
-6.250 -0.6642 0.01096 0.00424 -0.0029 0.7648 0.0491
-6.000 -0.6387 0.01070 0.00399 -0.0027 0.7566 0.0580
-5.750 -0.6132 0.01045 0.00376 -0.0024 0.7483 0.0685
-5.500 -0.5876 0.01018 0.00353 -0.0022 0.7408 0.0816
-5.250 -0.5624 0.00989 0.00329 -0.0019 0.7327 0.1002
-5.000 -0.5376 0.00953 0.00305 -0.0016 0.7257 0.1275
-4.500 -0.4888 0.00875 0.00255 -0.0008 0.7110 0.2040
-4.250 -0.4639 0.00838 0.00233 -0.0005 0.7036 0.2425
-4.000 -0.4398 0.00797 0.00210 0.0000 0.6967 0.2930
-3.750 -0.4162 0.00748 0.00187 0.0005 0.6897 0.3587
-3.500 -0.3909 0.00720 0.00172 0.0008 0.6823 0.4010
-3.250 -0.3638 0.00705 0.00163 0.0009 0.6759 0.4254
-3.000 -0.3365 0.00693 0.00154 0.0009 0.6686 0.4444
-2.750 -0.3089 0.00684 0.00147 0.0009 0.6619 0.4608
-2.500 -0.2815 0.00673 0.00141 0.0009 0.6548 0.4818
-2.250 -0.2541 0.00665 0.00136 0.0009 0.6481 0.5012
-2.000 -0.2261 0.00658 0.00131 0.0009 0.6412 0.5145
-1.750 -0.1982 0.00653 0.00127 0.0008 0.6341 0.5276
-1.500 -0.1700 0.00649 0.00124 0.0007 0.6276 0.5393
-1.250 -0.1418 0.00646 0.00121 0.0006 0.6204 0.5505
-1.000 -0.1138 0.00643 0.00119 0.0006 0.6139 0.5593
-0.750 -0.0851 0.00642 0.00117 0.0004 0.6070 0.5664
-0.250 -0.0284 0.00640 0.00115 0.0001 0.5935 0.5801
0.000 0.0000 0.00640 0.00115 0.0000 0.5865 0.5865
0.250 0.0284 0.00640 0.00115 -0.0001 0.5801 0.5935
0.750 0.0852 0.00642 0.00117 -0.0004 0.5664 0.6070
1.000 0.1138 0.00643 0.00119 -0.0006 0.5593 0.6139
1.250 0.1419 0.00646 0.00121 -0.0006 0.5505 0.6204
1.500 0.1701 0.00649 0.00124 -0.0007 0.5393 0.6276
1.750 0.1982 0.00653 0.00127 -0.0008 0.5275 0.6341
2.000 0.2261 0.00658 0.00131 -0.0009 0.5146 0.6411
2.250 0.2541 0.00665 0.00136 -0.0009 0.5011 0.6480
2.500 0.2815 0.00673 0.00141 -0.0009 0.4817 0.6548
2.750 0.3089 0.00684 0.00147 -0.0009 0.4610 0.6620
3.000 0.3365 0.00693 0.00154 -0.0009 0.4442 0.6687
3.250 0.3638 0.00705 0.00163 -0.0009 0.4254 0.6759
3.500 0.3908 0.00721 0.00173 -0.0008 0.4001 0.6824
3.750 0.4162 0.00748 0.00187 -0.0005 0.3587 0.6897
4.000 0.4398 0.00797 0.00210 0.0000 0.2931 0.6967
4.250 0.4639 0.00838 0.00233 0.0005 0.2428 0.7036
4.500 0.4888 0.00874 0.00255 0.0008 0.2043 0.7110
4.750 0.5129 0.00916 0.00280 0.0013 0.1615 0.7181
5.000 0.5375 0.00954 0.00305 0.0016 0.1272 0.7257
5.250 0.5624 0.00989 0.00329 0.0019 0.1001 0.7328
5.500 0.5876 0.01018 0.00353 0.0022 0.0815 0.7409
5.750 0.6131 0.01045 0.00376 0.0025 0.0683 0.7484
6.000 0.6386 0.01070 0.00399 0.0027 0.0580 0.7566
6.250 0.6641 0.01096 0.00424 0.0030 0.0491 0.7648
6.500 0.6895 0.01121 0.00449 0.0032 0.0419 0.7740
6.750 0.7148 0.01146 0.00475 0.0035 0.0363 0.7831
7.000 0.7398 0.01172 0.00502 0.0038 0.0319 0.7936
7.250 0.7646 0.01197 0.00530 0.0042 0.0285 0.8044
7.500 0.7894 0.01222 0.00559 0.0045 0.0258 0.8163
8.000 0.8378 0.01275 0.00622 0.0055 0.0213 0.8450
8.250 0.8613 0.01302 0.00655 0.0061 0.0195 0.8621
8.500 0.8840 0.01331 0.00691 0.0068 0.0180 0.8814
8.750 0.9065 0.01358 0.00727 0.0076 0.0171 0.9034
9.000 0.9282 0.01388 0.00765 0.0086 0.0162 0.9282
9.250 0.9513 0.01424 0.00806 0.0092 0.0153 0.9523
9.500 0.9785 0.01470 0.00855 0.0088 0.0146 0.9724
9.750 1.0087 0.01513 0.00901 0.0077 0.0141 0.9862
10.000 1.0381 0.01559 0.00951 0.0067 0.0136 0.9978
10.250 1.0587 0.01603 0.00996 0.0076 0.0133 1.0000
10.500 1.0769 0.01648 0.01043 0.0089 0.0130 1.0000
10.750 1.0940 0.01695 0.01094 0.0103 0.0127 1.0000
11.000 1.1094 0.01746 0.01147 0.0120 0.0125 1.0000
11.250 1.1244 0.01804 0.01208 0.0136 0.0122 1.0000
11.500 1.1389 0.01869 0.01277 0.0152 0.0120 1.0000
11.750 1.1522 0.01946 0.01359 0.0168 0.0117 1.0000
12.000 1.1663 0.02023 0.01440 0.0181 0.0116 1.0000
12.250 1.1808 0.02100 0.01522 0.0192 0.0115 1.0000
12.500 1.1947 0.02185 0.01613 0.0203 0.0115 1.0000
12.750 1.2080 0.02277 0.01711 0.0212 0.0114 1.0000
13.000 1.2207 0.02378 0.01818 0.0222 0.0113 1.0000
13.250 1.2329 0.02487 0.01933 0.0230 0.0111 1.0000
13.500 1.2448 0.02603 0.02054 0.0237 0.0110 1.0000
13.750 1.2560 0.02727 0.02186 0.0243 0.0109 1.0000
14.000 1.2666 0.02861 0.02326 0.0249 0.0107 1.0000
14.250 1.2762 0.03007 0.02478 0.0254 0.0106 1.0000
14.500 1.2846 0.03166 0.02644 0.0258 0.0105 1.0000
14.750 1.2923 0.03336 0.02821 0.0262 0.0104 1.0000
15.000 1.2992 0.03518 0.03009 0.0265 0.0103 1.0000
15.250 1.3050 0.03713 0.03212 0.0267 0.0102 1.0000
15.500 1.3099 0.03921 0.03427 0.0268 0.0102 1.0000
15.750 1.3138 0.04144 0.03658 0.0268 0.0101 1.0000
16.000 1.3162 0.04386 0.03908 0.0267 0.0100 1.0000
16.250 1.3175 0.04645 0.04176 0.0264 0.0099 1.0000
16.500 1.3178 0.04927 0.04466 0.0260 0.0099 1.0000
16.750 1.3169 0.05229 0.04777 0.0255 0.0098 1.0000
17.000 1.3149 0.05554 0.05111 0.0247 0.0097 1.0000
17.250 1.3114 0.05911 0.05477 0.0238 0.0097 1.0000
17.500 1.3065 0.06294 0.05869 0.0226 0.0096 1.0000
17.750 1.3000 0.06708 0.06293 0.0213 0.0095 1.0000
18.000 1.2918 0.07158 0.06754 0.0197 0.0095 1.0000
18.250 1.2821 0.07644 0.07249 0.0178 0.0094 1.0000
18.500 1.2705 0.08163 0.07780 0.0157 0.0094 1.0000
18.750 1.2569 0.08731 0.08359 0.0133 0.0093 1.0000
19.000 1.2424 0.09328 0.08967 0.0107 0.0093 1.0000
19.250 1.2262 0.09962 0.09612 0.0078 0.0092 1.0000
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