NACA 65(3)-618 (naca653618-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 65(3)-618 (naca653618-il) Reynolds number: 1,000,000 Max Cl/Cd: 128.41 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca653618-il-1000000-n5.txt Download as CSV file: xf-naca653618-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 65(3)-618
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 -0.9488 0.08351 0.08047 -0.0867 1.0000 0.0130
-19.500 -0.9664 0.07720 0.07403 -0.0902 1.0000 0.0131
-19.250 -0.9779 0.07205 0.06876 -0.0929 1.0000 0.0132
-19.000 -0.9873 0.06734 0.06395 -0.0953 1.0000 0.0134
-18.750 -0.9950 0.06308 0.05958 -0.0974 1.0000 0.0134
-18.500 -1.0004 0.05930 0.05569 -0.0991 1.0000 0.0136
-18.250 -1.0023 0.05609 0.05239 -0.1003 1.0000 0.0137
-18.000 -1.0035 0.05309 0.04930 -0.1014 1.0000 0.0138
-17.750 -1.0047 0.05023 0.04636 -0.1022 1.0000 0.0139
-17.500 -1.0051 0.04757 0.04363 -0.1028 1.0000 0.0141
-17.250 -1.0046 0.04512 0.04112 -0.1033 1.0000 0.0142
-17.000 -1.0001 0.04307 0.03901 -0.1036 0.9999 0.0144
-16.750 -0.9901 0.04092 0.03681 -0.1046 0.9874 0.0146
-16.500 -0.9696 0.03896 0.03480 -0.1077 0.9747 0.0148
-16.250 -0.9433 0.03697 0.03272 -0.1119 0.9646 0.0150
-16.000 -0.9116 0.03512 0.03079 -0.1169 0.9574 0.0153
-15.750 -0.8743 0.03346 0.02904 -0.1226 0.9496 0.0158
-15.500 -0.8367 0.03183 0.02729 -0.1284 0.9398 0.0162
-15.250 -0.8034 0.03034 0.02565 -0.1330 0.9242 0.0165
-15.000 -0.7812 0.02931 0.02446 -0.1347 0.9063 0.0167
-14.750 -0.7686 0.02823 0.02325 -0.1347 0.8902 0.0168
-14.500 -0.7607 0.02705 0.02197 -0.1340 0.8753 0.0171
-14.250 -0.7508 0.02604 0.02087 -0.1332 0.8627 0.0173
-14.000 -0.7398 0.02515 0.01990 -0.1324 0.8520 0.0175
-13.750 -0.7281 0.02432 0.01899 -0.1316 0.8417 0.0177
-13.500 -0.7146 0.02359 0.01819 -0.1308 0.8334 0.0180
-13.250 -0.7015 0.02285 0.01739 -0.1300 0.8247 0.0182
-13.000 -0.6880 0.02215 0.01661 -0.1291 0.8170 0.0184
-12.750 -0.6730 0.02154 0.01594 -0.1284 0.8090 0.0188
-12.500 -0.6591 0.02089 0.01522 -0.1274 0.8018 0.0190
-12.250 -0.6444 0.02026 0.01453 -0.1266 0.7948 0.0193
-12.000 -0.6304 0.01964 0.01383 -0.1255 0.7878 0.0195
-11.750 -0.6155 0.01903 0.01316 -0.1245 0.7820 0.0197
-11.500 -0.5996 0.01851 0.01257 -0.1236 0.7757 0.0199
-11.250 -0.5850 0.01795 0.01194 -0.1225 0.7692 0.0200
-11.000 -0.5733 0.01723 0.01117 -0.1211 0.7632 0.0203
-10.750 -0.5595 0.01664 0.01055 -0.1198 0.7569 0.0207
-10.250 -0.5289 0.01570 0.00953 -0.1173 0.7458 0.0213
-10.000 -0.5134 0.01527 0.00906 -0.1160 0.7404 0.0216
-9.750 -0.4997 0.01485 0.00859 -0.1142 0.7350 0.0219
-9.500 -0.4884 0.01448 0.00818 -0.1121 0.7304 0.0221
-9.250 -0.4718 0.01415 0.00781 -0.1108 0.7256 0.0225
-9.000 -0.4526 0.01384 0.00745 -0.1099 0.7205 0.0228
-8.750 -0.4325 0.01356 0.00711 -0.1090 0.7156 0.0232
-8.500 -0.4113 0.01325 0.00677 -0.1083 0.7115 0.0234
-8.250 -0.3892 0.01297 0.00644 -0.1077 0.7069 0.0236
-8.000 -0.3680 0.01263 0.00607 -0.1071 0.7026 0.0241
-7.750 -0.3456 0.01235 0.00575 -0.1066 0.6987 0.0246
-7.500 -0.3217 0.01207 0.00546 -0.1063 0.6953 0.0251
-7.250 -0.2973 0.01183 0.00520 -0.1060 0.6915 0.0255
-7.000 -0.2726 0.01161 0.00495 -0.1059 0.6875 0.0260
-6.750 -0.2477 0.01141 0.00471 -0.1057 0.6834 0.0266
-6.500 -0.2220 0.01121 0.00449 -0.1056 0.6800 0.0271
-6.250 -0.1959 0.01102 0.00427 -0.1056 0.6765 0.0276
-6.000 -0.1699 0.01081 0.00405 -0.1056 0.6729 0.0283
-5.750 -0.1437 0.01061 0.00384 -0.1056 0.6695 0.0293
-5.500 -0.1173 0.01046 0.00366 -0.1057 0.6662 0.0304
-5.250 -0.0903 0.01030 0.00349 -0.1058 0.6634 0.0317
-5.000 -0.0628 0.01015 0.00333 -0.1060 0.6606 0.0331
-4.750 -0.0355 0.00998 0.00317 -0.1062 0.6573 0.0355
-4.500 -0.0081 0.00985 0.00302 -0.1064 0.6539 0.0378
-4.250 0.0192 0.00970 0.00288 -0.1066 0.6506 0.0424
-4.000 0.0466 0.00955 0.00275 -0.1069 0.6476 0.0506
-3.750 0.0743 0.00930 0.00260 -0.1072 0.6453 0.0727
-3.500 0.1019 0.00902 0.00244 -0.1076 0.6427 0.1068
-3.250 0.1295 0.00867 0.00227 -0.1081 0.6399 0.1592
-3.000 0.1572 0.00825 0.00209 -0.1088 0.6371 0.2318
-2.750 0.1850 0.00773 0.00188 -0.1095 0.6342 0.3268
-2.250 0.2430 0.00684 0.00165 -0.1113 0.6290 0.5308
-2.000 0.2726 0.00681 0.00167 -0.1118 0.6266 0.5589
-1.750 0.3020 0.00681 0.00170 -0.1123 0.6242 0.5765
-1.500 0.3313 0.00681 0.00173 -0.1127 0.6217 0.5874
-1.250 0.3605 0.00684 0.00173 -0.1131 0.6193 0.5918
-1.000 0.3895 0.00688 0.00173 -0.1135 0.6168 0.5939
-0.750 0.4183 0.00692 0.00174 -0.1139 0.6142 0.5963
-0.500 0.4478 0.00692 0.00176 -0.1144 0.6121 0.5989
-0.250 0.4771 0.00693 0.00177 -0.1148 0.6099 0.6012
0.000 0.5063 0.00695 0.00180 -0.1153 0.6076 0.6037
0.250 0.5353 0.00698 0.00182 -0.1157 0.6053 0.6063
0.500 0.5642 0.00702 0.00185 -0.1161 0.6029 0.6088
0.750 0.5929 0.00707 0.00189 -0.1164 0.6004 0.6110
1.250 0.6505 0.00715 0.00197 -0.1171 0.5961 0.6153
1.500 0.6796 0.00717 0.00202 -0.1176 0.5941 0.6179
1.750 0.7085 0.00721 0.00208 -0.1180 0.5918 0.6208
2.000 0.7372 0.00725 0.00214 -0.1183 0.5893 0.6236
2.250 0.7657 0.00730 0.00220 -0.1187 0.5869 0.6261
2.500 0.7940 0.00736 0.00226 -0.1189 0.5845 0.6285
2.750 0.8217 0.00745 0.00233 -0.1191 0.5816 0.6306
3.000 0.8503 0.00747 0.00240 -0.1195 0.5782 0.6334
3.250 0.8784 0.00751 0.00248 -0.1197 0.5736 0.6362
3.500 0.9058 0.00758 0.00256 -0.1198 0.5689 0.6394
3.750 0.9326 0.00768 0.00266 -0.1198 0.5644 0.6426
4.000 0.9604 0.00773 0.00274 -0.1201 0.5583 0.6457
4.250 0.9853 0.00786 0.00284 -0.1197 0.5476 0.6483
4.500 1.0115 0.00794 0.00294 -0.1196 0.5372 0.6512
4.750 1.0363 0.00807 0.00306 -0.1192 0.5253 0.6545
5.000 1.0575 0.00831 0.00323 -0.1181 0.5027 0.6578
5.250 1.0731 0.00873 0.00349 -0.1161 0.4661 0.6612
5.500 1.0824 0.00937 0.00390 -0.1128 0.4182 0.6647
5.750 1.0806 0.01017 0.00443 -0.1075 0.3642 0.6682
6.000 1.0784 0.01109 0.00511 -0.1023 0.3132 0.6723
6.250 1.0778 0.01202 0.00583 -0.0977 0.2680 0.6765
6.500 1.0784 0.01296 0.00659 -0.0934 0.2281 0.6806
6.750 1.0813 0.01390 0.00736 -0.0898 0.1951 0.6843
7.000 1.0838 0.01491 0.00824 -0.0863 0.1629 0.6882
7.250 1.0873 0.01596 0.00917 -0.0831 0.1345 0.6927
7.500 1.0914 0.01705 0.01015 -0.0801 0.1084 0.6973
7.750 1.0969 0.01815 0.01116 -0.0775 0.0860 0.7017
8.000 1.1047 0.01920 0.01214 -0.0754 0.0700 0.7062
8.250 1.1120 0.02030 0.01320 -0.0732 0.0546 0.7114
8.500 1.1194 0.02147 0.01431 -0.0712 0.0406 0.7168
8.750 1.1307 0.02245 0.01527 -0.0697 0.0338 0.7216
9.000 1.1420 0.02344 0.01627 -0.0683 0.0290 0.7265
9.250 1.1551 0.02435 0.01721 -0.0671 0.0265 0.7319
9.500 1.1680 0.02530 0.01819 -0.0659 0.0245 0.7374
9.750 1.1813 0.02625 0.01917 -0.0648 0.0229 0.7424
10.000 1.1933 0.02730 0.02025 -0.0637 0.0214 0.7483
10.250 1.2072 0.02825 0.02125 -0.0628 0.0204 0.7548
10.500 1.2198 0.02931 0.02235 -0.0618 0.0193 0.7608
10.750 1.2321 0.03041 0.02349 -0.0608 0.0183 0.7678
11.000 1.2445 0.03154 0.02467 -0.0599 0.0175 0.7748
11.250 1.2574 0.03263 0.02581 -0.0591 0.0167 0.7814
11.500 1.2691 0.03385 0.02708 -0.0582 0.0158 0.7888
11.750 1.2806 0.03511 0.02838 -0.0574 0.0152 0.7958
12.000 1.2921 0.03640 0.02972 -0.0566 0.0146 0.8038
12.250 1.3040 0.03767 0.03105 -0.0559 0.0141 0.8120
12.500 1.3157 0.03896 0.03242 -0.0552 0.0136 0.8211
12.750 1.3263 0.04038 0.03389 -0.0545 0.0131 0.8306
13.000 1.3369 0.04180 0.03537 -0.0538 0.0127 0.8408
13.250 1.3461 0.04338 0.03702 -0.0531 0.0123 0.8511
13.500 1.3566 0.04485 0.03856 -0.0524 0.0119 0.8627
13.750 1.3664 0.04635 0.04015 -0.0518 0.0116 0.8768
14.000 1.3749 0.04792 0.04182 -0.0510 0.0114 0.8954
14.250 1.3828 0.04938 0.04339 -0.0499 0.0111 0.9257
14.750 1.4009 0.05285 0.04701 -0.0493 0.0106 1.0000
15.250 1.4173 0.05677 0.05101 -0.0488 0.0102 1.0000
15.500 1.4240 0.05894 0.05322 -0.0486 0.0099 1.0000
15.750 1.4311 0.06111 0.05545 -0.0485 0.0098 1.0000
16.000 1.4391 0.06320 0.05759 -0.0484 0.0097 1.0000
16.250 1.4458 0.06548 0.05994 -0.0484 0.0095 1.0000
16.500 1.4528 0.06775 0.06226 -0.0485 0.0094 1.0000
16.750 1.4588 0.07015 0.06473 -0.0486 0.0093 1.0000
17.000 1.4642 0.07267 0.06731 -0.0488 0.0092 1.0000
17.250 1.4694 0.07525 0.06996 -0.0490 0.0091 1.0000
17.500 1.4742 0.07793 0.07271 -0.0493 0.0090 1.0000
17.750 1.4784 0.08072 0.07556 -0.0497 0.0089 1.0000
18.000 1.4822 0.08358 0.07849 -0.0502 0.0088 1.0000
18.250 1.4849 0.08662 0.08161 -0.0508 0.0087 1.0000
18.500 1.4876 0.08972 0.08477 -0.0514 0.0086 1.0000
18.750 1.4893 0.09299 0.08811 -0.0522 0.0085 1.0000
19.000 1.4912 0.09626 0.09146 -0.0530 0.0085 1.0000
19.250 1.4915 0.09983 0.09510 -0.0540 0.0083 1.0000
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