AVISTAR (avistar-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: AVISTAR (avistar-il) Reynolds number: 200,000 Max Cl/Cd: 59.45 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-avistar-il-200000-n5.txt Download as CSV file: xf-avistar-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AVISTAR
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.750 -0.4798 0.08874 0.08475 -0.0466 1.0000 0.0312
-10.500 -0.5025 0.07749 0.07350 -0.0546 1.0000 0.0307
-10.250 -0.5454 0.06576 0.06161 -0.0644 1.0000 0.0303
-10.000 -0.5786 0.05998 0.05567 -0.0666 1.0000 0.0301
-9.750 -0.6090 0.05672 0.05231 -0.0637 1.0000 0.0300
-9.500 -0.6274 0.05300 0.04837 -0.0620 0.9905 0.0300
-9.250 -0.6286 0.04845 0.04348 -0.0627 0.9759 0.0302
-9.000 -0.6242 0.04450 0.03914 -0.0628 0.9637 0.0304
-8.750 -0.6186 0.04067 0.03482 -0.0620 0.9527 0.0311
-8.500 -0.6122 0.03687 0.03031 -0.0606 0.9432 0.0318
-8.250 -0.5949 0.03491 0.02818 -0.0600 0.9341 0.0321
-8.000 -0.5729 0.03331 0.02643 -0.0600 0.9271 0.0324
-7.750 -0.5537 0.03187 0.02483 -0.0591 0.9174 0.0326
-7.250 -0.5139 0.02911 0.02166 -0.0571 0.8969 0.0334
-7.000 -0.4935 0.02782 0.02013 -0.0560 0.8876 0.0339
-6.750 -0.4728 0.02670 0.01879 -0.0549 0.8788 0.0347
-6.500 -0.4508 0.02556 0.01739 -0.0539 0.8726 0.0355
-6.250 -0.4285 0.02449 0.01604 -0.0529 0.8655 0.0362
-6.000 -0.4049 0.02349 0.01482 -0.0521 0.8588 0.0366
-5.750 -0.3801 0.02248 0.01376 -0.0517 0.8532 0.0370
-5.500 -0.3555 0.02169 0.01293 -0.0512 0.8463 0.0375
-5.250 -0.3306 0.02096 0.01214 -0.0507 0.8399 0.0381
-5.000 -0.3054 0.02030 0.01141 -0.0502 0.8345 0.0389
-4.750 -0.2803 0.01971 0.01077 -0.0498 0.8278 0.0399
-4.500 -0.2552 0.01915 0.01010 -0.0492 0.8211 0.0410
-4.250 -0.2297 0.01861 0.00945 -0.0486 0.8153 0.0417
-4.000 -0.2052 0.01793 0.00881 -0.0480 0.8080 0.0423
-3.750 -0.1810 0.01735 0.00825 -0.0474 0.8011 0.0430
-3.500 -0.1566 0.01686 0.00774 -0.0467 0.7954 0.0439
-3.250 -0.1325 0.01643 0.00733 -0.0460 0.7877 0.0450
-3.000 -0.1080 0.01607 0.00692 -0.0453 0.7806 0.0466
-2.750 -0.0834 0.01574 0.00654 -0.0446 0.7735 0.0479
-2.500 -0.0605 0.01526 0.00610 -0.0436 0.7650 0.0491
-2.250 -0.0364 0.01491 0.00571 -0.0428 0.7578 0.0504
-2.000 -0.0120 0.01462 0.00542 -0.0421 0.7487 0.0520
-1.750 0.0131 0.01437 0.00510 -0.0415 0.7409 0.0539
-1.500 0.0378 0.01411 0.00482 -0.0408 0.7317 0.0566
-1.250 0.0631 0.01388 0.00455 -0.0402 0.7231 0.0600
-1.000 0.0885 0.01370 0.00433 -0.0396 0.7130 0.0635
-0.750 0.1138 0.01348 0.00408 -0.0390 0.7035 0.0701
-0.500 0.1312 0.01249 0.00380 -0.0373 0.6924 0.2452
-0.250 0.1431 0.01138 0.00368 -0.0343 0.6825 0.5006
0.000 0.1603 0.01090 0.00372 -0.0318 0.6719 0.6383
0.250 0.1830 0.01069 0.00374 -0.0304 0.6615 0.7167
0.500 0.2093 0.01055 0.00372 -0.0297 0.6512 0.7712
0.750 0.2431 0.01046 0.00379 -0.0306 0.6397 0.8250
1.000 0.2865 0.01048 0.00386 -0.0336 0.6286 0.8777
1.250 0.3364 0.01058 0.00393 -0.0381 0.6168 0.9177
1.500 0.3852 0.01071 0.00401 -0.0426 0.6036 0.9351
1.750 0.4289 0.01086 0.00405 -0.0460 0.5893 0.9422
2.000 0.4683 0.01102 0.00412 -0.0485 0.5761 0.9502
2.250 0.5071 0.01120 0.00421 -0.0508 0.5639 0.9577
2.500 0.5445 0.01137 0.00433 -0.0529 0.5527 0.9658
2.750 0.5795 0.01157 0.00446 -0.0545 0.5437 0.9768
3.000 0.6142 0.01180 0.00467 -0.0562 0.5340 0.9925
3.250 0.6553 0.01202 0.00482 -0.0592 0.5191 1.0000
3.500 0.6765 0.01216 0.00487 -0.0581 0.5036 1.0000
3.750 0.6977 0.01232 0.00495 -0.0569 0.4872 1.0000
4.000 0.7190 0.01250 0.00505 -0.0558 0.4700 1.0000
4.250 0.7405 0.01269 0.00518 -0.0547 0.4523 1.0000
4.500 0.7618 0.01290 0.00533 -0.0535 0.4299 1.0000
4.750 0.7823 0.01316 0.00549 -0.0522 0.4032 1.0000
5.000 0.7994 0.01361 0.00570 -0.0503 0.3505 1.0000
5.250 0.8096 0.01456 0.00615 -0.0475 0.2746 1.0000
5.500 0.8216 0.01548 0.00674 -0.0450 0.2194 1.0000
5.750 0.8157 0.01763 0.00797 -0.0400 0.0627 1.0000
6.000 0.8291 0.01843 0.00865 -0.0376 0.0464 1.0000
6.250 0.8455 0.01900 0.00922 -0.0357 0.0420 1.0000
6.500 0.8624 0.01953 0.00978 -0.0339 0.0392 1.0000
6.750 0.8783 0.02009 0.01037 -0.0320 0.0370 1.0000
7.000 0.8926 0.02073 0.01104 -0.0298 0.0355 1.0000
7.250 0.9076 0.02131 0.01167 -0.0278 0.0344 1.0000
7.500 0.9204 0.02194 0.01237 -0.0254 0.0334 1.0000
7.750 0.9296 0.02262 0.01310 -0.0225 0.0326 1.0000
8.000 0.9373 0.02338 0.01390 -0.0194 0.0319 1.0000
8.250 0.9440 0.02427 0.01483 -0.0165 0.0314 1.0000
8.500 0.9487 0.02537 0.01598 -0.0136 0.0309 1.0000
8.750 0.9561 0.02643 0.01709 -0.0113 0.0304 1.0000
9.000 0.9644 0.02752 0.01824 -0.0092 0.0298 1.0000
9.250 0.9724 0.02871 0.01948 -0.0073 0.0292 1.0000
9.500 0.9801 0.02999 0.02080 -0.0055 0.0286 1.0000
9.750 0.9877 0.03133 0.02219 -0.0038 0.0280 1.0000
10.000 0.9953 0.03275 0.02364 -0.0023 0.0275 1.0000
10.250 1.0026 0.03425 0.02516 -0.0009 0.0271 1.0000
10.500 1.0100 0.03579 0.02671 0.0005 0.0268 1.0000
10.750 1.0177 0.03737 0.02829 0.0018 0.0265 1.0000
11.000 1.0268 0.03888 0.02981 0.0030 0.0263 1.0000
11.250 1.0377 0.04027 0.03126 0.0041 0.0260 1.0000
11.500 1.0491 0.04166 0.03270 0.0051 0.0257 1.0000
11.750 1.0611 0.04302 0.03413 0.0061 0.0254 1.0000
12.000 1.0737 0.04437 0.03553 0.0071 0.0252 1.0000
12.250 1.0869 0.04571 0.03693 0.0081 0.0249 1.0000
12.500 1.1001 0.04709 0.03837 0.0089 0.0246 1.0000
12.750 1.1129 0.04851 0.03986 0.0098 0.0243 1.0000
13.000 1.1253 0.04997 0.04138 0.0105 0.0239 1.0000
13.250 1.1371 0.05149 0.04295 0.0112 0.0235 1.0000
13.500 1.1486 0.05306 0.04458 0.0119 0.0232 1.0000
13.750 1.1600 0.05467 0.04623 0.0125 0.0229 1.0000
14.000 1.1727 0.05626 0.04786 0.0132 0.0227 1.0000
14.250 1.1878 0.05782 0.04946 0.0138 0.0224 1.0000
14.500 1.1952 0.05993 0.05170 0.0145 0.0223 1.0000
14.750 1.1999 0.06227 0.05424 0.0150 0.0222 1.0000
15.000 1.2031 0.06481 0.05696 0.0155 0.0220 1.0000
15.250 1.2045 0.06754 0.05988 0.0158 0.0219 1.0000
15.500 1.2041 0.07051 0.06303 0.0160 0.0218 1.0000
15.750 1.2020 0.07373 0.06644 0.0160 0.0217 1.0000
16.000 1.1978 0.07724 0.07015 0.0158 0.0216 1.0000
16.250 1.1917 0.08105 0.07415 0.0153 0.0215 1.0000
16.500 1.1840 0.08517 0.07849 0.0145 0.0215 1.0000
16.750 1.1745 0.08966 0.08318 0.0134 0.0214 1.0000
17.000 1.1632 0.09454 0.08826 0.0119 0.0214 1.0000
17.250 1.1501 0.09985 0.09377 0.0099 0.0213 1.0000
17.500 1.1354 0.10563 0.09976 0.0075 0.0213 1.0000
17.750 1.1189 0.11197 0.10630 0.0045 0.0213 1.0000
18.000 1.1008 0.11888 0.11342 0.0009 0.0212 1.0000
18.250 1.0809 0.12649 0.12123 -0.0033 0.0212 1.0000
18.500 1.0588 0.13507 0.13001 -0.0084 0.0213 1.0000
18.750 1.0324 0.14527 0.14043 -0.0149 0.0213 1.0000
19.000 0.9987 0.15833 0.15371 -0.0233 0.0215 1.0000
19.250 0.9414 0.18065 0.17628 -0.0372 0.0219 1.0000
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