NACA 63(3)-218 (naca633218-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(3)-218 (naca633218-il) Reynolds number: 500,000 Max Cl/Cd: 67.77 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca633218-il-500000.txt Download as CSV file: xf-naca633218-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0361 0.10589 0.10205 -0.0306 1.0000 0.0234
-19.500 -1.0421 0.10104 0.09710 -0.0333 1.0000 0.0236
-19.250 -1.0478 0.09636 0.09231 -0.0359 1.0000 0.0239
-19.000 -1.0530 0.09182 0.08765 -0.0382 1.0000 0.0241
-18.750 -1.0576 0.08747 0.08319 -0.0404 1.0000 0.0245
-18.500 -1.0611 0.08342 0.07902 -0.0424 1.0000 0.0248
-18.250 -1.0635 0.07959 0.07506 -0.0442 1.0000 0.0251
-18.000 -1.0651 0.07593 0.07129 -0.0458 1.0000 0.0254
-17.750 -1.0667 0.07233 0.06755 -0.0474 1.0000 0.0257
-17.500 -1.0664 0.06927 0.06440 -0.0482 1.0000 0.0262
-17.250 -1.0621 0.06684 0.06193 -0.0487 1.0000 0.0265
-17.000 -1.0575 0.06435 0.05943 -0.0496 1.0000 0.0270
-16.750 -1.0532 0.06182 0.05687 -0.0504 1.0000 0.0275
-16.500 -1.0482 0.05946 0.05445 -0.0510 1.0000 0.0279
-16.250 -1.0442 0.05693 0.05185 -0.0519 1.0000 0.0286
-16.000 -1.0392 0.05459 0.04943 -0.0525 1.0000 0.0292
-15.750 -1.0335 0.05238 0.04713 -0.0530 1.0000 0.0297
-15.500 -1.0274 0.05026 0.04491 -0.0534 1.0000 0.0302
-15.250 -1.0214 0.04833 0.04295 -0.0532 1.0000 0.0309
-15.000 -1.0144 0.04648 0.04110 -0.0532 1.0000 0.0316
-14.750 -1.0070 0.04463 0.03924 -0.0534 1.0000 0.0323
-14.500 -0.9987 0.04291 0.03749 -0.0534 1.0000 0.0331
-14.250 -0.9905 0.04121 0.03573 -0.0534 1.0000 0.0339
-14.000 -0.9813 0.03964 0.03409 -0.0534 1.0000 0.0346
-13.750 -0.9716 0.03814 0.03250 -0.0534 1.0000 0.0354
-13.500 -0.9360 0.03586 0.03016 -0.0595 0.9142 0.0369
-13.250 -0.9235 0.03452 0.02862 -0.0598 0.8648 0.0379
-13.000 -0.9158 0.03335 0.02729 -0.0588 0.8325 0.0389
-12.750 -0.9077 0.03214 0.02594 -0.0579 0.8090 0.0397
-12.500 -0.8979 0.03100 0.02466 -0.0571 0.7909 0.0406
-12.250 -0.8865 0.02999 0.02350 -0.0564 0.7735 0.0413
-12.000 -0.8834 0.02842 0.02186 -0.0551 0.7551 0.0422
-11.750 -0.8772 0.02707 0.02044 -0.0541 0.7399 0.0433
-11.500 -0.8678 0.02597 0.01926 -0.0531 0.7246 0.0444
-11.250 -0.8575 0.02495 0.01814 -0.0522 0.7078 0.0456
-11.000 -0.8468 0.02400 0.01707 -0.0511 0.6898 0.0466
-10.750 -0.8341 0.02318 0.01613 -0.0502 0.6732 0.0477
-10.500 -0.8290 0.02194 0.01480 -0.0486 0.6571 0.0490
-10.250 -0.8220 0.02086 0.01366 -0.0471 0.6405 0.0506
-10.000 -0.8115 0.02002 0.01274 -0.0457 0.6243 0.0520
-9.750 -0.8001 0.01929 0.01191 -0.0443 0.6073 0.0538
-9.500 -0.7872 0.01869 0.01119 -0.0429 0.5886 0.0554
-9.250 -0.7851 0.01779 0.01022 -0.0400 0.5692 0.0579
-9.000 -0.7767 0.01728 0.00961 -0.0377 0.5458 0.0605
-8.750 -0.7603 0.01688 0.00909 -0.0364 0.5196 0.0640
-8.500 -0.7490 0.01670 0.00850 -0.0346 0.3777 0.0690
-8.250 -0.7323 0.01623 0.00796 -0.0334 0.3521 0.0771
-8.000 -0.7148 0.01564 0.00741 -0.0323 0.3449 0.0910
-7.750 -0.6964 0.01500 0.00687 -0.0314 0.3432 0.1134
-7.500 -0.6768 0.01439 0.00638 -0.0307 0.3418 0.1412
-7.250 -0.6564 0.01376 0.00590 -0.0301 0.3405 0.1732
-7.000 -0.6359 0.01308 0.00541 -0.0295 0.3395 0.2146
-6.750 -0.6146 0.01241 0.00495 -0.0291 0.3387 0.2629
-6.500 -0.5919 0.01182 0.00455 -0.0288 0.3380 0.3112
-6.250 -0.5676 0.01136 0.00427 -0.0286 0.3373 0.3577
-6.000 -0.5414 0.01110 0.00410 -0.0286 0.3367 0.3920
-5.750 -0.5143 0.01095 0.00398 -0.0287 0.3356 0.4159
-5.500 -0.4867 0.01087 0.00390 -0.0288 0.3341 0.4347
-5.250 -0.4586 0.01083 0.00383 -0.0289 0.3326 0.4496
-5.000 -0.4304 0.01080 0.00377 -0.0291 0.3317 0.4621
-4.750 -0.4021 0.01077 0.00372 -0.0292 0.3312 0.4730
-4.500 -0.3737 0.01076 0.00369 -0.0294 0.3310 0.4869
-4.250 -0.3450 0.01080 0.00369 -0.0296 0.3308 0.4999
-4.000 -0.3167 0.01078 0.00369 -0.0297 0.3306 0.5094
-3.750 -0.2878 0.01082 0.00366 -0.0300 0.3304 0.5174
-3.500 -0.2592 0.01080 0.00365 -0.0301 0.3302 0.5242
-3.250 -0.2304 0.01082 0.00365 -0.0303 0.3301 0.5314
-3.000 -0.2016 0.01087 0.00364 -0.0306 0.3298 0.5393
-2.750 -0.1731 0.01089 0.00368 -0.0307 0.3294 0.5466
-2.500 -0.1442 0.01093 0.00368 -0.0309 0.3290 0.5526
-2.250 -0.1154 0.01095 0.00365 -0.0312 0.3286 0.5576
-2.000 -0.0869 0.01094 0.00367 -0.0313 0.3282 0.5626
-1.750 -0.0581 0.01098 0.00369 -0.0315 0.3277 0.5678
-1.500 -0.0292 0.01104 0.00369 -0.0318 0.3273 0.5729
-1.250 -0.0006 0.01104 0.00370 -0.0320 0.3271 0.5778
-1.000 0.0280 0.01107 0.00374 -0.0322 0.3268 0.5828
-0.750 0.0567 0.01113 0.00378 -0.0324 0.3266 0.5882
-0.500 0.0856 0.01120 0.00380 -0.0327 0.3263 0.5931
-0.250 0.1139 0.01120 0.00384 -0.0328 0.3260 0.5979
0.000 0.1425 0.01125 0.00390 -0.0330 0.3258 0.6028
0.250 0.1711 0.01132 0.00396 -0.0332 0.3255 0.6078
0.500 0.1999 0.01140 0.00400 -0.0335 0.3252 0.6124
0.750 0.2281 0.01141 0.00407 -0.0336 0.3249 0.6172
1.000 0.2565 0.01149 0.00416 -0.0337 0.3246 0.6222
1.250 0.2850 0.01158 0.00424 -0.0339 0.3242 0.6276
1.500 0.3135 0.01165 0.00431 -0.0342 0.3238 0.6324
1.750 0.3416 0.01171 0.00441 -0.0343 0.3235 0.6372
2.000 0.3698 0.01181 0.00452 -0.0344 0.3231 0.6423
2.250 0.3982 0.01192 0.00463 -0.0346 0.3226 0.6477
2.500 0.4262 0.01201 0.00474 -0.0347 0.3221 0.6529
2.750 0.4541 0.01212 0.00488 -0.0348 0.3216 0.6582
3.000 0.4818 0.01231 0.00507 -0.0349 0.3203 0.6638
3.250 0.5098 0.01254 0.00526 -0.0351 0.3191 0.6691
3.500 0.5375 0.01267 0.00545 -0.0352 0.3184 0.6743
3.750 0.5656 0.01274 0.00557 -0.0353 0.3179 0.6798
4.000 0.5938 0.01282 0.00569 -0.0354 0.3173 0.6859
4.250 0.6214 0.01288 0.00582 -0.0355 0.3159 0.6916
4.500 0.6488 0.01297 0.00598 -0.0355 0.3142 0.6974
4.750 0.6761 0.01311 0.00614 -0.0355 0.3118 0.7035
5.000 0.7030 0.01333 0.00635 -0.0355 0.3088 0.7092
5.250 0.7297 0.01368 0.00671 -0.0355 0.3060 0.7149
5.500 0.7559 0.01361 0.00677 -0.0353 0.3027 0.7215
5.750 0.7820 0.01369 0.00687 -0.0352 0.2976 0.7279
6.000 0.8071 0.01373 0.00699 -0.0348 0.2921 0.7339
6.250 0.8337 0.01366 0.00703 -0.0347 0.2871 0.7404
6.500 0.8603 0.01369 0.00709 -0.0346 0.2831 0.7471
6.750 0.8883 0.01355 0.00713 -0.0346 0.2766 0.7536
7.250 0.9366 0.01382 0.00719 -0.0338 0.2061 0.7674
7.500 0.9538 0.01436 0.00776 -0.0324 0.1993 0.7745
7.750 0.9725 0.01483 0.00826 -0.0312 0.1937 0.7823
8.000 0.9909 0.01522 0.00874 -0.0299 0.1878 0.7895
8.250 1.0078 0.01564 0.00921 -0.0283 0.1822 0.7975
8.500 1.0260 0.01591 0.00955 -0.0269 0.1750 0.8054
8.750 1.0435 0.01618 0.00990 -0.0254 0.1669 0.8141
9.000 1.0618 0.01649 0.01023 -0.0241 0.1529 0.8232
9.250 1.0739 0.01704 0.01070 -0.0221 0.1285 0.8330
9.500 1.0793 0.01793 0.01149 -0.0194 0.1088 0.8439
9.750 1.0825 0.01896 0.01248 -0.0167 0.0941 0.8570
10.000 1.0854 0.01999 0.01354 -0.0140 0.0817 0.8717
10.500 1.0897 0.02213 0.01578 -0.0087 0.0655 0.9177
10.750 1.1017 0.02337 0.01710 -0.0085 0.0596 1.0000
11.000 1.1088 0.02488 0.01858 -0.0077 0.0555 1.0000
11.250 1.1169 0.02633 0.02005 -0.0069 0.0526 1.0000
11.500 1.1249 0.02781 0.02155 -0.0062 0.0501 1.0000
11.750 1.1289 0.02963 0.02338 -0.0054 0.0481 1.0000
12.000 1.1326 0.03154 0.02533 -0.0047 0.0466 1.0000
12.250 1.1404 0.03317 0.02702 -0.0042 0.0452 1.0000
12.500 1.1466 0.03497 0.02886 -0.0037 0.0439 1.0000
12.750 1.1511 0.03695 0.03089 -0.0033 0.0427 1.0000
13.000 1.1528 0.03925 0.03321 -0.0030 0.0416 1.0000
13.250 1.1499 0.04206 0.03606 -0.0026 0.0406 1.0000
13.500 1.1572 0.04400 0.03807 -0.0026 0.0398 1.0000
13.750 1.1636 0.04608 0.04021 -0.0026 0.0387 1.0000
14.000 1.1685 0.04835 0.04254 -0.0027 0.0379 1.0000
14.250 1.1732 0.05068 0.04492 -0.0029 0.0369 1.0000
14.500 1.1754 0.05335 0.04762 -0.0031 0.0360 1.0000
14.750 1.1741 0.05642 0.05071 -0.0034 0.0350 1.0000
15.000 1.1786 0.05891 0.05326 -0.0038 0.0343 1.0000
15.250 1.1846 0.06133 0.05576 -0.0042 0.0336 1.0000
15.500 1.1902 0.06380 0.05830 -0.0047 0.0328 1.0000
15.750 1.1953 0.06641 0.06096 -0.0053 0.0318 1.0000
16.000 1.1995 0.06912 0.06369 -0.0060 0.0310 1.0000
16.250 1.2015 0.07207 0.06665 -0.0067 0.0302 1.0000
16.500 1.2048 0.07485 0.06948 -0.0073 0.0294 1.0000
16.750 1.2101 0.07762 0.07235 -0.0082 0.0287 1.0000
17.000 1.2156 0.08036 0.07517 -0.0091 0.0279 1.0000
17.250 1.2199 0.08327 0.07813 -0.0101 0.0272 1.0000
17.500 1.2245 0.08616 0.08105 -0.0111 0.0265 1.0000
17.750 1.2281 0.08915 0.08407 -0.0121 0.0259 1.0000
18.000 1.2326 0.09167 0.08658 -0.0126 0.0252 1.0000
18.250 1.2366 0.09485 0.08987 -0.0139 0.0248 1.0000
18.500 1.2400 0.09806 0.09318 -0.0152 0.0243 1.0000
18.750 1.2438 0.10119 0.09640 -0.0165 0.0239 1.0000
19.000 1.2469 0.10449 0.09978 -0.0180 0.0233 1.0000
19.250 1.2502 0.10775 0.10311 -0.0194 0.0229 1.0000
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