NACA 63-015A AIRFOIL (n63015a-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63-015A AIRFOIL (n63015a-il) Reynolds number: 500,000 Max Cl/Cd: 55.25 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n63015a-il-500000-n5.txt Download as CSV file: xf-n63015a-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0441 0.13855 0.13524 0.0097 1.0000 0.0118
-19.500 -1.0606 0.13090 0.12746 0.0053 1.0000 0.0118
-19.250 -1.0755 0.12380 0.12023 0.0014 1.0000 0.0119
-19.000 -1.0898 0.11700 0.11331 -0.0022 1.0000 0.0119
-18.750 -1.1029 0.11063 0.10682 -0.0055 1.0000 0.0120
-18.500 -1.1150 0.10452 0.10059 -0.0086 1.0000 0.0120
-18.250 -1.1261 0.09875 0.09470 -0.0114 1.0000 0.0121
-18.000 -1.1364 0.09326 0.08910 -0.0140 1.0000 0.0121
-17.750 -1.1454 0.08808 0.08381 -0.0163 1.0000 0.0122
-17.500 -1.1534 0.08318 0.07879 -0.0184 1.0000 0.0122
-17.250 -1.1602 0.07856 0.07406 -0.0204 1.0000 0.0123
-17.000 -1.1662 0.07420 0.06959 -0.0221 1.0000 0.0124
-16.750 -1.1710 0.07010 0.06539 -0.0236 1.0000 0.0124
-16.500 -1.1745 0.06627 0.06145 -0.0249 1.0000 0.0125
-16.250 -1.1773 0.06266 0.05774 -0.0260 1.0000 0.0126
-16.000 -1.1791 0.05928 0.05426 -0.0270 1.0000 0.0127
-15.750 -1.1798 0.05610 0.05098 -0.0277 1.0000 0.0128
-15.500 -1.1795 0.05316 0.04794 -0.0284 1.0000 0.0129
-15.250 -1.1786 0.05038 0.04507 -0.0288 1.0000 0.0131
-15.000 -1.1765 0.04781 0.04240 -0.0291 1.0000 0.0132
-14.750 -1.1737 0.04536 0.03986 -0.0292 1.0000 0.0134
-14.500 -1.1702 0.04306 0.03745 -0.0293 1.0000 0.0136
-14.250 -1.1658 0.04087 0.03517 -0.0292 1.0000 0.0137
-14.000 -1.1607 0.03879 0.03301 -0.0290 1.0000 0.0139
-13.750 -1.1550 0.03682 0.03094 -0.0287 1.0000 0.0140
-13.500 -1.1484 0.03498 0.02900 -0.0284 1.0000 0.0141
-13.250 -1.1410 0.03324 0.02718 -0.0279 1.0000 0.0143
-13.000 -1.1327 0.03162 0.02548 -0.0274 1.0000 0.0144
-12.750 -1.1235 0.03012 0.02389 -0.0268 1.0000 0.0146
-12.500 -1.1151 0.02860 0.02229 -0.0260 1.0000 0.0147
-12.250 -1.1075 0.02706 0.02069 -0.0251 1.0000 0.0150
-12.000 -1.0979 0.02574 0.01931 -0.0242 1.0000 0.0152
-11.750 -1.0869 0.02458 0.01810 -0.0232 1.0000 0.0155
-11.500 -1.0749 0.02355 0.01702 -0.0221 1.0000 0.0158
-11.250 -1.0622 0.02261 0.01603 -0.0209 1.0000 0.0161
-11.000 -1.0488 0.02176 0.01512 -0.0196 1.0000 0.0164
-10.750 -1.0350 0.02099 0.01430 -0.0183 1.0000 0.0169
-10.500 -1.0209 0.02029 0.01355 -0.0168 1.0000 0.0173
-10.250 -1.0066 0.01966 0.01287 -0.0151 1.0000 0.0178
-10.000 -0.9934 0.01904 0.01221 -0.0132 1.0000 0.0183
-9.750 -0.9805 0.01841 0.01155 -0.0111 1.0000 0.0189
-9.500 -0.9649 0.01787 0.01099 -0.0095 1.0000 0.0196
-9.250 -0.9490 0.01738 0.01048 -0.0077 1.0000 0.0205
-9.000 -0.9322 0.01693 0.00999 -0.0061 0.9992 0.0214
-8.750 -0.9024 0.01636 0.00939 -0.0073 0.9891 0.0228
-8.500 -0.8728 0.01580 0.00883 -0.0084 0.9773 0.0248
-8.250 -0.8425 0.01534 0.00832 -0.0094 0.9638 0.0269
-8.000 -0.8140 0.01483 0.00781 -0.0101 0.9480 0.0300
-7.750 -0.7874 0.01444 0.00737 -0.0102 0.9296 0.0332
-7.500 -0.7641 0.01404 0.00694 -0.0096 0.9100 0.0376
-7.250 -0.7415 0.01369 0.00656 -0.0088 0.8910 0.0428
-7.000 -0.7189 0.01335 0.00618 -0.0080 0.8735 0.0500
-6.750 -0.6962 0.01301 0.00583 -0.0073 0.8578 0.0593
-6.500 -0.6731 0.01267 0.00548 -0.0066 0.8434 0.0706
-6.000 -0.6261 0.01199 0.00483 -0.0054 0.8181 0.1009
-5.750 -0.6033 0.01156 0.00449 -0.0048 0.8071 0.1278
-5.500 -0.5809 0.01109 0.00414 -0.0041 0.7968 0.1642
-5.000 -0.5357 0.01009 0.00347 -0.0028 0.7779 0.2535
-4.750 -0.5134 0.00957 0.00315 -0.0021 0.7689 0.3079
-4.500 -0.4907 0.00911 0.00289 -0.0014 0.7608 0.3655
-4.250 -0.4668 0.00876 0.00271 -0.0009 0.7523 0.4140
-4.000 -0.4412 0.00857 0.00258 -0.0005 0.7448 0.4444
-3.750 -0.4147 0.00843 0.00247 -0.0003 0.7369 0.4653
-3.500 -0.3879 0.00833 0.00237 -0.0002 0.7296 0.4822
-3.250 -0.3607 0.00823 0.00228 -0.0001 0.7219 0.4977
-3.000 -0.3338 0.00815 0.00220 0.0001 0.7147 0.5168
-2.750 -0.3066 0.00807 0.00214 0.0002 0.7074 0.5337
-2.500 -0.2794 0.00801 0.00208 0.0003 0.7000 0.5469
-2.250 -0.2519 0.00795 0.00202 0.0003 0.6932 0.5591
-2.000 -0.2241 0.00791 0.00197 0.0003 0.6857 0.5702
-1.750 -0.1964 0.00788 0.00193 0.0004 0.6789 0.5799
-1.500 -0.1684 0.00785 0.00189 0.0003 0.6716 0.5873
-1.000 -0.1122 0.00782 0.00182 0.0002 0.6575 0.6015
-0.750 -0.0844 0.00780 0.00180 0.0002 0.6505 0.6086
-0.500 -0.0560 0.00780 0.00178 0.0001 0.6436 0.6157
-0.250 -0.0281 0.00778 0.00177 0.0001 0.6363 0.6224
0.000 0.0000 0.00779 0.00177 0.0000 0.6297 0.6297
0.250 0.0281 0.00778 0.00177 -0.0001 0.6224 0.6363
0.500 0.0560 0.00780 0.00178 -0.0001 0.6157 0.6436
0.750 0.0844 0.00780 0.00180 -0.0002 0.6086 0.6504
1.000 0.1122 0.00782 0.00182 -0.0002 0.6015 0.6575
1.500 0.1684 0.00785 0.00189 -0.0003 0.5872 0.6715
1.750 0.1964 0.00788 0.00193 -0.0004 0.5799 0.6788
2.000 0.2241 0.00791 0.00197 -0.0003 0.5702 0.6857
2.250 0.2519 0.00795 0.00202 -0.0003 0.5591 0.6932
2.500 0.2794 0.00801 0.00208 -0.0003 0.5469 0.7000
2.750 0.3066 0.00807 0.00214 -0.0002 0.5338 0.7074
3.000 0.3338 0.00815 0.00220 -0.0001 0.5169 0.7147
3.250 0.3607 0.00823 0.00228 0.0001 0.4977 0.7219
3.500 0.3879 0.00833 0.00237 0.0002 0.4822 0.7296
3.750 0.4147 0.00843 0.00247 0.0003 0.4654 0.7370
4.000 0.4412 0.00856 0.00258 0.0005 0.4445 0.7448
4.250 0.4668 0.00876 0.00271 0.0009 0.4138 0.7524
4.500 0.4907 0.00911 0.00289 0.0014 0.3656 0.7609
4.750 0.5134 0.00957 0.00315 0.0021 0.3082 0.7690
5.000 0.5357 0.01009 0.00346 0.0028 0.2535 0.7779
5.250 0.5583 0.01058 0.00379 0.0035 0.2075 0.7869
5.750 0.6033 0.01156 0.00449 0.0048 0.1278 0.8072
6.000 0.6261 0.01199 0.00483 0.0054 0.1009 0.8181
6.500 0.6731 0.01267 0.00548 0.0066 0.0706 0.8434
6.750 0.6961 0.01301 0.00583 0.0073 0.0594 0.8578
7.000 0.7189 0.01335 0.00618 0.0080 0.0500 0.8735
7.250 0.7415 0.01369 0.00656 0.0088 0.0428 0.8911
7.500 0.7640 0.01404 0.00694 0.0096 0.0375 0.9101
7.750 0.7874 0.01444 0.00737 0.0102 0.0332 0.9297
8.000 0.8141 0.01483 0.00781 0.0101 0.0300 0.9480
8.250 0.8425 0.01534 0.00832 0.0094 0.0269 0.9638
8.500 0.8729 0.01580 0.00883 0.0083 0.0248 0.9774
8.750 0.9025 0.01636 0.00939 0.0073 0.0228 0.9892
9.000 0.9323 0.01693 0.00999 0.0061 0.0214 0.9993
9.250 0.9491 0.01738 0.01047 0.0077 0.0205 1.0000
9.500 0.9650 0.01786 0.01099 0.0094 0.0196 1.0000
9.750 0.9806 0.01841 0.01155 0.0111 0.0189 1.0000
10.000 0.9936 0.01904 0.01220 0.0132 0.0183 1.0000
10.250 1.0069 0.01966 0.01286 0.0151 0.0178 1.0000
10.500 1.0212 0.02029 0.01355 0.0167 0.0173 1.0000
10.750 1.0354 0.02099 0.01430 0.0182 0.0169 1.0000
11.000 1.0492 0.02176 0.01512 0.0196 0.0164 1.0000
11.250 1.0626 0.02261 0.01603 0.0208 0.0161 1.0000
11.500 1.0754 0.02354 0.01701 0.0220 0.0158 1.0000
11.750 1.0875 0.02457 0.01809 0.0231 0.0155 1.0000
12.000 1.0986 0.02573 0.01930 0.0241 0.0152 1.0000
12.250 1.1082 0.02704 0.02067 0.0250 0.0150 1.0000
12.500 1.1159 0.02859 0.02227 0.0259 0.0147 1.0000
12.750 1.1244 0.03010 0.02386 0.0267 0.0146 1.0000
13.000 1.1337 0.03160 0.02545 0.0272 0.0144 1.0000
13.250 1.1420 0.03322 0.02716 0.0278 0.0143 1.0000
13.500 1.1495 0.03495 0.02897 0.0282 0.0141 1.0000
13.750 1.1563 0.03679 0.03091 0.0285 0.0140 1.0000
14.000 1.1620 0.03876 0.03297 0.0288 0.0139 1.0000
14.250 1.1672 0.04083 0.03513 0.0290 0.0137 1.0000
14.500 1.1716 0.04302 0.03741 0.0291 0.0136 1.0000
14.750 1.1753 0.04532 0.03982 0.0290 0.0134 1.0000
15.000 1.1783 0.04774 0.04233 0.0289 0.0132 1.0000
15.250 1.1803 0.05033 0.04502 0.0286 0.0131 1.0000
15.500 1.1813 0.05310 0.04788 0.0281 0.0129 1.0000
15.750 1.1818 0.05603 0.05091 0.0275 0.0128 1.0000
16.000 1.1811 0.05920 0.05418 0.0267 0.0127 1.0000
16.250 1.1794 0.06258 0.05766 0.0258 0.0126 1.0000
16.500 1.1767 0.06619 0.06137 0.0246 0.0125 1.0000
16.750 1.1732 0.07002 0.06531 0.0233 0.0124 1.0000
17.000 1.1685 0.07412 0.06951 0.0218 0.0124 1.0000
17.250 1.1626 0.07847 0.07397 0.0201 0.0123 1.0000
17.500 1.1558 0.08309 0.07871 0.0181 0.0122 1.0000
17.750 1.1479 0.08799 0.08371 0.0160 0.0122 1.0000
18.000 1.1388 0.09319 0.08903 0.0136 0.0121 1.0000
18.250 1.1285 0.09868 0.09463 0.0111 0.0120 1.0000
18.500 1.1175 0.10446 0.10053 0.0083 0.0120 1.0000
18.750 1.1053 0.11060 0.10678 0.0052 0.0119 1.0000
19.000 1.0921 0.11699 0.11329 0.0019 0.0119 1.0000
19.250 1.0778 0.12380 0.12024 -0.0018 0.0119 1.0000
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