NACA 63(3)-218 (naca633218-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(3)-218 (naca633218-il) Reynolds number: 1,000,000 Max Cl/Cd: 81.61 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633218-il-1000000.txt Download as CSV file: xf-naca633218-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-218
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1433 0.09117 0.08741 -0.0343 1.0000 0.0179
-19.500 -1.1468 0.08718 0.08333 -0.0362 1.0000 0.0181
-19.250 -1.1485 0.08347 0.07954 -0.0378 1.0000 0.0182
-19.000 -1.1514 0.07971 0.07570 -0.0394 1.0000 0.0184
-18.750 -1.1601 0.07529 0.07121 -0.0411 1.0000 0.0187
-18.500 -1.1665 0.07125 0.06710 -0.0427 1.0000 0.0189
-18.250 -1.1675 0.06792 0.06372 -0.0439 1.0000 0.0193
-18.000 -1.1666 0.06492 0.06068 -0.0449 1.0000 0.0196
-17.750 -1.1646 0.06210 0.05781 -0.0459 1.0000 0.0199
-17.500 -1.1608 0.05951 0.05517 -0.0467 1.0000 0.0204
-17.250 -1.1589 0.05676 0.05236 -0.0475 1.0000 0.0206
-17.000 -1.1542 0.05436 0.04991 -0.0481 1.0000 0.0210
-16.750 -1.1486 0.05213 0.04762 -0.0486 1.0000 0.0213
-16.500 -1.1037 0.04941 0.04439 -0.0574 0.8343 0.0219
-16.250 -1.1093 0.04644 0.04127 -0.0575 0.8074 0.0226
-16.000 -1.1070 0.04441 0.03907 -0.0573 0.7644 0.0230
-15.750 -1.1020 0.04255 0.03705 -0.0573 0.7326 0.0234
-15.500 -1.0963 0.04084 0.03516 -0.0571 0.6889 0.0239
-15.250 -1.0863 0.03956 0.03369 -0.0569 0.6442 0.0246
-15.000 -1.0791 0.03827 0.03206 -0.0565 0.5468 0.0251
-14.750 -1.0704 0.03748 0.03068 -0.0560 0.3294 0.0256
-14.500 -1.0612 0.03605 0.02918 -0.0558 0.3261 0.0259
-14.250 -1.0633 0.03379 0.02687 -0.0553 0.3242 0.0268
-14.000 -1.0569 0.03224 0.02528 -0.0548 0.3216 0.0273
-13.750 -1.0481 0.03091 0.02391 -0.0544 0.3196 0.0280
-13.500 -1.0382 0.02968 0.02264 -0.0538 0.3185 0.0286
-13.250 -1.0270 0.02858 0.02149 -0.0533 0.3180 0.0292
-13.000 -1.0147 0.02757 0.02044 -0.0527 0.3174 0.0299
-12.750 -1.0015 0.02665 0.01946 -0.0522 0.3166 0.0303
-12.500 -0.9968 0.02518 0.01794 -0.0511 0.3163 0.0310
-12.250 -0.9899 0.02391 0.01664 -0.0501 0.3159 0.0318
-12.000 -0.9790 0.02293 0.01564 -0.0491 0.3152 0.0326
-11.750 -0.9666 0.02207 0.01475 -0.0482 0.3148 0.0334
-11.500 -0.9539 0.02126 0.01390 -0.0473 0.3144 0.0342
-11.250 -0.9407 0.02051 0.01310 -0.0463 0.3139 0.0348
-11.000 -0.9263 0.01986 0.01240 -0.0453 0.3135 0.0353
-10.750 -0.9164 0.01900 0.01150 -0.0438 0.3131 0.0361
-10.500 -0.9080 0.01815 0.01061 -0.0420 0.3127 0.0371
-10.250 -0.8981 0.01747 0.00991 -0.0401 0.3124 0.0381
-10.000 -0.8900 0.01699 0.00940 -0.0376 0.3120 0.0389
-9.750 -0.8756 0.01661 0.00898 -0.0359 0.3117 0.0399
-9.500 -0.8567 0.01627 0.00860 -0.0349 0.3113 0.0408
-9.250 -0.8377 0.01589 0.00817 -0.0339 0.3110 0.0421
-9.000 -0.8186 0.01545 0.00773 -0.0330 0.3107 0.0443
-8.750 -0.7970 0.01512 0.00739 -0.0323 0.3104 0.0464
-8.500 -0.7741 0.01484 0.00707 -0.0318 0.3101 0.0483
-8.250 -0.7525 0.01444 0.00669 -0.0312 0.3098 0.0526
-8.000 -0.7296 0.01409 0.00635 -0.0307 0.3095 0.0585
-7.750 -0.7069 0.01369 0.00600 -0.0302 0.3092 0.0684
-7.500 -0.6839 0.01328 0.00566 -0.0298 0.3090 0.0831
-7.250 -0.6608 0.01284 0.00532 -0.0295 0.3087 0.1026
-7.000 -0.6368 0.01247 0.00504 -0.0292 0.3078 0.1236
-6.750 -0.6128 0.01208 0.00476 -0.0290 0.3068 0.1484
-6.500 -0.5882 0.01170 0.00450 -0.0288 0.3061 0.1762
-6.250 -0.5638 0.01121 0.00418 -0.0287 0.3059 0.2148
-6.000 -0.5391 0.01071 0.00388 -0.0286 0.3058 0.2599
-5.750 -0.5135 0.01028 0.00362 -0.0287 0.3057 0.3035
-5.500 -0.4873 0.00991 0.00341 -0.0288 0.3056 0.3451
-5.250 -0.4600 0.00967 0.00328 -0.0289 0.3055 0.3791
-5.000 -0.4319 0.00953 0.00320 -0.0291 0.3054 0.4020
-4.750 -0.4035 0.00944 0.00314 -0.0294 0.3052 0.4195
-4.500 -0.3748 0.00939 0.00309 -0.0296 0.3051 0.4337
-4.250 -0.3459 0.00936 0.00306 -0.0299 0.3050 0.4458
-4.000 -0.3172 0.00931 0.00304 -0.0301 0.3049 0.4594
-3.750 -0.2882 0.00929 0.00302 -0.0304 0.3045 0.4708
-3.500 -0.2590 0.00929 0.00301 -0.0307 0.3040 0.4814
-3.250 -0.2301 0.00926 0.00299 -0.0310 0.3035 0.4902
-3.000 -0.2009 0.00928 0.00300 -0.0312 0.3032 0.4975
-2.750 -0.1718 0.00930 0.00300 -0.0315 0.3029 0.5036
-2.500 -0.1428 0.00931 0.00301 -0.0318 0.3027 0.5113
-2.250 -0.1135 0.00936 0.00304 -0.0321 0.3025 0.5186
-2.000 -0.0846 0.00936 0.00305 -0.0324 0.3022 0.5252
-1.750 -0.0555 0.00939 0.00307 -0.0326 0.3019 0.5303
-1.500 -0.0263 0.00944 0.00309 -0.0329 0.3016 0.5351
-1.250 0.0028 0.00947 0.00311 -0.0332 0.3013 0.5397
-1.000 0.0318 0.00949 0.00315 -0.0335 0.3009 0.5450
-0.750 0.0608 0.00953 0.00318 -0.0337 0.3005 0.5500
-0.500 0.0900 0.00959 0.00322 -0.0340 0.3002 0.5546
-0.250 0.1189 0.00962 0.00326 -0.0343 0.2997 0.5600
0.000 0.1478 0.00966 0.00331 -0.0345 0.2993 0.5652
0.250 0.1768 0.00972 0.00336 -0.0348 0.2989 0.5702
0.500 0.2058 0.00980 0.00342 -0.0351 0.2984 0.5742
0.750 0.2345 0.00984 0.00348 -0.0353 0.2979 0.5794
1.000 0.2632 0.00990 0.00355 -0.0355 0.2974 0.5842
1.250 0.2918 0.00999 0.00363 -0.0358 0.2968 0.5888
1.500 0.3204 0.01011 0.00373 -0.0360 0.2961 0.5930
1.750 0.3485 0.01022 0.00386 -0.0361 0.2954 0.5985
2.000 0.3763 0.01039 0.00406 -0.0362 0.2946 0.6036
2.250 0.4056 0.01040 0.00408 -0.0365 0.2941 0.6084
2.500 0.4350 0.01039 0.00408 -0.0369 0.2935 0.6127
2.750 0.4641 0.01036 0.00410 -0.0371 0.2927 0.6181
3.000 0.4932 0.01036 0.00415 -0.0374 0.2919 0.6234
3.250 0.5222 0.01039 0.00419 -0.0377 0.2910 0.6285
3.500 0.5514 0.01039 0.00422 -0.0380 0.2896 0.6337
3.750 0.5805 0.01036 0.00423 -0.0383 0.2878 0.6394
4.000 0.6095 0.01037 0.00426 -0.0385 0.2862 0.6448
4.250 0.6379 0.01045 0.00432 -0.0387 0.2840 0.6495
4.500 0.6680 0.01035 0.00428 -0.0391 0.2819 0.6552
4.750 0.6988 0.01021 0.00420 -0.0397 0.2774 0.6609
5.000 0.7293 0.01012 0.00412 -0.0401 0.2720 0.6666
5.500 0.7804 0.01066 0.00439 -0.0398 0.2021 0.6783
5.750 0.8057 0.01094 0.00468 -0.0395 0.1979 0.6842
6.000 0.8319 0.01115 0.00491 -0.0394 0.1945 0.6894
6.250 0.8582 0.01131 0.00513 -0.0393 0.1914 0.6957
6.500 0.8835 0.01154 0.00540 -0.0390 0.1878 0.7022
6.750 0.9081 0.01184 0.00570 -0.0387 0.1839 0.7078
7.000 0.9349 0.01193 0.00587 -0.0386 0.1810 0.7143
7.250 0.9606 0.01210 0.00608 -0.0384 0.1765 0.7208
7.500 0.9850 0.01237 0.00634 -0.0380 0.1713 0.7268
7.750 1.0112 0.01247 0.00650 -0.0379 0.1647 0.7337
8.000 1.0356 0.01269 0.00671 -0.0375 0.1528 0.7405
8.250 1.0556 0.01316 0.00701 -0.0365 0.1245 0.7467
8.500 1.0718 0.01375 0.00750 -0.0350 0.1029 0.7541
8.750 1.0881 0.01429 0.00799 -0.0335 0.0887 0.7616
9.000 1.1002 0.01482 0.00848 -0.0312 0.0757 0.7688
9.250 1.1087 0.01539 0.00902 -0.0283 0.0653 0.7769
9.500 1.1175 0.01604 0.00964 -0.0258 0.0572 0.7850
9.750 1.1267 0.01670 0.01033 -0.0234 0.0511 0.7943
10.000 1.1357 0.01746 0.01110 -0.0213 0.0466 0.8036
10.250 1.1471 0.01813 0.01183 -0.0195 0.0440 0.8138
10.500 1.1559 0.01899 0.01272 -0.0176 0.0414 0.8243
10.750 1.1665 0.01979 0.01359 -0.0159 0.0398 0.8364
11.000 1.1776 0.02058 0.01446 -0.0144 0.0385 0.8500
11.250 1.1864 0.02151 0.01547 -0.0128 0.0372 0.8663
11.500 1.1926 0.02257 0.01662 -0.0109 0.0359 0.8887
11.750 1.1958 0.02364 0.01787 -0.0086 0.0347 0.9388
12.000 1.2145 0.02467 0.01898 -0.0092 0.0340 1.0000
12.250 1.2253 0.02586 0.02021 -0.0085 0.0332 1.0000
12.500 1.2351 0.02714 0.02152 -0.0077 0.0323 1.0000
12.750 1.2433 0.02859 0.02300 -0.0070 0.0315 1.0000
13.000 1.2491 0.03026 0.02469 -0.0062 0.0307 1.0000
13.250 1.2507 0.03231 0.02679 -0.0054 0.0298 1.0000
13.500 1.2593 0.03387 0.02840 -0.0050 0.0294 1.0000
13.750 1.2687 0.03537 0.02995 -0.0046 0.0287 1.0000
14.000 1.2764 0.03707 0.03169 -0.0043 0.0281 1.0000
14.250 1.2830 0.03894 0.03361 -0.0040 0.0274 1.0000
14.500 1.2883 0.04097 0.03567 -0.0038 0.0267 1.0000
14.750 1.2906 0.04335 0.03809 -0.0037 0.0259 1.0000
15.000 1.2888 0.04626 0.04105 -0.0037 0.0252 1.0000
15.250 1.2962 0.04828 0.04313 -0.0038 0.0248 1.0000
15.500 1.3026 0.05042 0.04533 -0.0040 0.0243 1.0000
15.750 1.3091 0.05261 0.04758 -0.0043 0.0236 1.0000
16.000 1.3144 0.05498 0.04999 -0.0046 0.0230 1.0000
16.250 1.3181 0.05758 0.05263 -0.0051 0.0224 1.0000
16.500 1.3168 0.06082 0.05591 -0.0057 0.0218 1.0000
16.750 1.3138 0.06436 0.05951 -0.0065 0.0211 1.0000
17.000 1.3201 0.06681 0.06203 -0.0071 0.0208 1.0000
17.250 1.3245 0.06956 0.06484 -0.0079 0.0203 1.0000
17.500 1.3285 0.07237 0.06770 -0.0087 0.0197 1.0000
17.750 1.3317 0.07534 0.07073 -0.0096 0.0192 1.0000
18.000 1.3322 0.07871 0.07416 -0.0107 0.0189 1.0000
18.250 1.3321 0.08223 0.07771 -0.0120 0.0183 1.0000
18.500 1.3261 0.08663 0.08217 -0.0136 0.0179 1.0000
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