S8036 (16%) (s8036-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: S8036 (16%) (s8036-il) Reynolds number: 500,000 Max Cl/Cd: 73.25 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s8036-il-500000-n5.txt Download as CSV file: xf-s8036-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S8036 (16%)
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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7210 0.13252 0.12938 -0.0316 1.0000 0.0083
-18.000 -0.7538 0.12114 0.11783 -0.0373 1.0000 0.0082
-17.750 -0.7901 0.10972 0.10624 -0.0433 1.0000 0.0083
-17.500 -0.8132 0.10109 0.09745 -0.0478 1.0000 0.0082
-17.250 -0.8276 0.09472 0.09100 -0.0510 1.0000 0.0081
-17.000 -0.8511 0.08647 0.08257 -0.0554 1.0000 0.0081
-16.750 -0.8697 0.07956 0.07552 -0.0590 1.0000 0.0081
-16.500 -0.8830 0.07376 0.06960 -0.0620 1.0000 0.0081
-16.250 -0.8966 0.06813 0.06382 -0.0648 1.0000 0.0081
-16.000 -0.9078 0.06320 0.05877 -0.0670 1.0000 0.0081
-15.750 -0.9172 0.05874 0.05415 -0.0689 1.0000 0.0082
-15.500 -0.9255 0.05473 0.05002 -0.0702 1.0000 0.0082
-15.250 -0.9332 0.05106 0.04623 -0.0711 1.0000 0.0083
-15.000 -0.9410 0.04760 0.04266 -0.0716 1.0000 0.0083
-14.750 -0.9451 0.04468 0.03964 -0.0718 1.0000 0.0083
-14.500 -0.9471 0.04213 0.03700 -0.0716 1.0000 0.0083
-14.250 -0.9498 0.03964 0.03441 -0.0712 1.0000 0.0084
-14.000 -0.9509 0.03741 0.03208 -0.0705 1.0000 0.0084
-13.750 -0.9508 0.03542 0.03002 -0.0697 1.0000 0.0086
-13.500 -0.9487 0.03369 0.02821 -0.0685 1.0000 0.0086
-13.250 -0.9471 0.03203 0.02648 -0.0671 1.0000 0.0088
-13.000 -0.9439 0.03058 0.02496 -0.0656 1.0000 0.0089
-12.750 -0.9418 0.02917 0.02347 -0.0636 1.0000 0.0089
-12.500 -0.9363 0.02809 0.02233 -0.0617 1.0000 0.0091
-12.250 -0.9335 0.02692 0.02109 -0.0593 1.0000 0.0091
-12.000 -0.9299 0.02591 0.02002 -0.0567 1.0000 0.0093
-11.750 -0.9263 0.02504 0.01908 -0.0539 1.0000 0.0094
-11.500 -0.9126 0.02399 0.01797 -0.0530 0.9987 0.0095
-11.250 -0.8867 0.02298 0.01687 -0.0542 0.9950 0.0098
-11.000 -0.8635 0.02205 0.01586 -0.0547 0.9899 0.0100
-10.750 -0.8436 0.02120 0.01494 -0.0544 0.9808 0.0102
-10.250 -0.8026 0.01958 0.01319 -0.0534 0.9472 0.0107
-10.000 -0.7648 0.01867 0.01224 -0.0565 0.9359 0.0112
-9.750 -0.7168 0.01779 0.01128 -0.0617 0.9264 0.0116
-9.500 -0.6641 0.01692 0.01033 -0.0678 0.9135 0.0125
-9.250 -0.6182 0.01617 0.00946 -0.0724 0.8922 0.0135
-9.000 -0.5888 0.01568 0.00886 -0.0733 0.8677 0.0142
-8.750 -0.5694 0.01532 0.00837 -0.0720 0.8463 0.0151
-8.500 -0.5536 0.01501 0.00793 -0.0699 0.8283 0.0161
-8.250 -0.5387 0.01472 0.00756 -0.0675 0.8129 0.0168
-8.000 -0.5226 0.01444 0.00721 -0.0654 0.7995 0.0183
-7.750 -0.5049 0.01415 0.00686 -0.0636 0.7888 0.0197
-7.500 -0.4865 0.01388 0.00652 -0.0618 0.7786 0.0217
-7.250 -0.4676 0.01360 0.00620 -0.0602 0.7695 0.0239
-7.000 -0.4482 0.01336 0.00590 -0.0587 0.7605 0.0272
-6.750 -0.4283 0.01309 0.00561 -0.0572 0.7528 0.0310
-6.500 -0.4082 0.01283 0.00533 -0.0558 0.7451 0.0356
-6.250 -0.3877 0.01258 0.00507 -0.0545 0.7383 0.0416
-6.000 -0.3668 0.01234 0.00482 -0.0532 0.7310 0.0487
-5.500 -0.3251 0.01183 0.00435 -0.0506 0.7182 0.0700
-5.250 -0.3042 0.01156 0.00413 -0.0493 0.7119 0.0852
-5.000 -0.2834 0.01130 0.00391 -0.0480 0.7063 0.1049
-4.750 -0.2621 0.01102 0.00371 -0.0468 0.7004 0.1269
-4.500 -0.2415 0.01072 0.00350 -0.0455 0.6947 0.1551
-4.000 -0.2015 0.01003 0.00309 -0.0426 0.6847 0.2373
-3.750 -0.1824 0.00964 0.00289 -0.0410 0.6793 0.2923
-3.500 -0.1645 0.00922 0.00270 -0.0392 0.6741 0.3592
-3.250 -0.1454 0.00886 0.00255 -0.0375 0.6695 0.4175
-3.000 -0.1248 0.00859 0.00245 -0.0360 0.6647 0.4665
-2.750 -0.1029 0.00842 0.00238 -0.0348 0.6597 0.5043
-2.500 -0.0800 0.00832 0.00233 -0.0337 0.6551 0.5358
-2.250 -0.0559 0.00823 0.00231 -0.0329 0.6502 0.5637
-2.000 -0.0315 0.00817 0.00228 -0.0320 0.6451 0.5852
-1.750 -0.0064 0.00816 0.00225 -0.0314 0.6402 0.6007
-1.500 0.0190 0.00814 0.00223 -0.0308 0.6353 0.6157
-1.250 0.0443 0.00812 0.00223 -0.0302 0.6299 0.6312
-1.000 0.0695 0.00810 0.00221 -0.0295 0.6246 0.6437
-0.750 0.0954 0.00811 0.00220 -0.0290 0.6198 0.6527
-0.500 0.1216 0.00810 0.00219 -0.0286 0.6144 0.6616
-0.250 0.1477 0.00810 0.00218 -0.0282 0.6090 0.6687
0.000 0.1737 0.00812 0.00218 -0.0278 0.6040 0.6755
0.250 0.2003 0.00813 0.00218 -0.0275 0.5985 0.6823
0.500 0.2263 0.00813 0.00219 -0.0270 0.5928 0.6885
0.750 0.2520 0.00816 0.00219 -0.0265 0.5872 0.6955
1.000 0.2783 0.00817 0.00221 -0.0262 0.5809 0.7024
1.250 0.3037 0.00819 0.00223 -0.0256 0.5742 0.7093
1.500 0.3294 0.00822 0.00225 -0.0251 0.5678 0.7164
1.750 0.3551 0.00824 0.00228 -0.0246 0.5606 0.7226
2.000 0.3801 0.00829 0.00232 -0.0240 0.5536 0.7296
2.250 0.4056 0.00831 0.00236 -0.0235 0.5452 0.7367
2.500 0.4299 0.00836 0.00240 -0.0228 0.5365 0.7440
2.750 0.4545 0.00840 0.00245 -0.0221 0.5259 0.7520
3.000 0.4784 0.00845 0.00250 -0.0212 0.5147 0.7599
3.250 0.5017 0.00852 0.00256 -0.0203 0.5035 0.7690
3.500 0.5254 0.00858 0.00264 -0.0194 0.4921 0.7779
3.750 0.5486 0.00866 0.00272 -0.0185 0.4800 0.7882
4.000 0.5713 0.00874 0.00281 -0.0174 0.4686 0.7985
4.250 0.5930 0.00885 0.00291 -0.0162 0.4545 0.8100
4.500 0.6144 0.00897 0.00303 -0.0149 0.4398 0.8233
4.750 0.6352 0.00910 0.00317 -0.0135 0.4212 0.8372
5.000 0.6554 0.00928 0.00333 -0.0121 0.3991 0.8531
5.250 0.6761 0.00951 0.00353 -0.0108 0.3763 0.8725
5.500 0.7020 0.00981 0.00380 -0.0107 0.3504 0.8943
5.750 0.7383 0.01024 0.00415 -0.0130 0.3225 0.9134
6.000 0.7805 0.01074 0.00456 -0.0166 0.2954 0.9274
6.250 0.8248 0.01126 0.00498 -0.0208 0.2689 0.9368
6.500 0.8632 0.01181 0.00543 -0.0237 0.2436 0.9471
6.750 0.8948 0.01233 0.00585 -0.0251 0.2214 0.9595
7.250 0.9390 0.01322 0.00662 -0.0237 0.1906 0.9876
7.500 0.9649 0.01371 0.00703 -0.0239 0.1753 0.9944
7.750 0.9957 0.01416 0.00743 -0.0252 0.1624 0.9987
8.000 1.0115 0.01454 0.00777 -0.0234 0.1534 1.0000
8.250 1.0188 0.01485 0.00807 -0.0197 0.1464 1.0000
8.500 1.0259 0.01523 0.00842 -0.0161 0.1399 1.0000
8.750 1.0354 0.01560 0.00878 -0.0130 0.1331 1.0000
9.000 1.0436 0.01607 0.00923 -0.0098 0.1267 1.0000
9.250 1.0550 0.01647 0.00965 -0.0072 0.1217 1.0000
9.500 1.0643 0.01700 0.01016 -0.0045 0.1159 1.0000
9.750 1.0750 0.01752 0.01069 -0.0020 0.1112 1.0000
10.000 1.0859 0.01808 0.01126 0.0002 0.1063 1.0000
10.250 1.0953 0.01876 0.01193 0.0026 0.1016 1.0000
10.500 1.1068 0.01940 0.01259 0.0045 0.0974 1.0000
10.750 1.1176 0.02011 0.01331 0.0064 0.0935 1.0000
11.000 1.1275 0.02092 0.01413 0.0083 0.0901 1.0000
11.250 1.1388 0.02171 0.01495 0.0100 0.0871 1.0000
11.500 1.1500 0.02253 0.01581 0.0115 0.0840 1.0000
11.750 1.1603 0.02346 0.01676 0.0129 0.0813 1.0000
12.000 1.1693 0.02452 0.01783 0.0144 0.0784 1.0000
12.250 1.1806 0.02547 0.01884 0.0157 0.0763 1.0000
12.500 1.1914 0.02648 0.01989 0.0168 0.0743 1.0000
12.750 1.2012 0.02759 0.02104 0.0180 0.0720 1.0000
13.000 1.2098 0.02882 0.02230 0.0191 0.0698 1.0000
13.250 1.2172 0.03018 0.02368 0.0202 0.0676 1.0000
13.500 1.2275 0.03134 0.02491 0.0211 0.0660 1.0000
13.750 1.2368 0.03261 0.02624 0.0219 0.0643 1.0000
14.000 1.2448 0.03400 0.02769 0.0228 0.0625 1.0000
14.250 1.2515 0.03554 0.02926 0.0236 0.0607 1.0000
14.500 1.2566 0.03724 0.03099 0.0244 0.0590 1.0000
14.750 1.2650 0.03870 0.03253 0.0250 0.0577 1.0000
15.000 1.2724 0.04029 0.03418 0.0255 0.0559 1.0000
15.250 1.2786 0.04202 0.03597 0.0260 0.0543 1.0000
15.500 1.2838 0.04387 0.03788 0.0265 0.0528 1.0000
15.750 1.2871 0.04596 0.04000 0.0269 0.0513 1.0000
16.000 1.2915 0.04799 0.04210 0.0271 0.0500 1.0000
16.250 1.2975 0.04990 0.04409 0.0273 0.0485 1.0000
16.500 1.3016 0.05204 0.04629 0.0275 0.0469 1.0000
16.750 1.3039 0.05440 0.04871 0.0275 0.0457 1.0000
17.000 1.3049 0.05697 0.05132 0.0274 0.0444 1.0000
17.250 1.3069 0.05946 0.05388 0.0273 0.0428 1.0000
17.500 1.3092 0.06197 0.05648 0.0271 0.0415 1.0000
17.750 1.3102 0.06467 0.05925 0.0268 0.0405 1.0000
18.000 1.3096 0.06760 0.06224 0.0263 0.0390 1.0000
18.250 1.3071 0.07082 0.06553 0.0257 0.0381 1.0000
18.500 1.3035 0.07426 0.06904 0.0250 0.0374 1.0000
18.750 1.3029 0.07734 0.07222 0.0243 0.0365 1.0000
19.000 1.3013 0.08059 0.07556 0.0235 0.0353 1.0000
19.250 1.2975 0.08418 0.07923 0.0226 0.0343 1.0000
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Polar data table (+)
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