AS5045 (15%) (as5045-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AS5045 (15%) (as5045-il) Reynolds number: 1,000,000 Max Cl/Cd: 81.91 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-as5045-il-1000000-n5.txt Download as CSV file: xf-as5045-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AS5045 (15%)
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
------ -------- --------- --------- -------- -------- --------
-15.250 -0.8608 0.09200 0.08901 -0.0184 0.7229 0.0046
-15.000 -0.9040 0.07882 0.07558 -0.0264 0.7221 0.0045
-14.500 -0.9535 0.06303 0.05937 -0.0347 0.7189 0.0045
-14.250 -0.9700 0.05757 0.05373 -0.0368 0.7173 0.0046
-14.000 -0.9826 0.05300 0.04898 -0.0382 0.7155 0.0046
-13.750 -0.9921 0.04904 0.04485 -0.0390 0.7137 0.0046
-13.500 -0.9980 0.04560 0.04124 -0.0394 0.7120 0.0047
-13.250 -1.0013 0.04255 0.03803 -0.0396 0.7102 0.0047
-13.000 -1.0018 0.03985 0.03517 -0.0395 0.7084 0.0048
-12.750 -0.9994 0.03746 0.03263 -0.0394 0.7067 0.0048
-12.500 -0.9950 0.03531 0.03033 -0.0391 0.7051 0.0049
-12.250 -0.9884 0.03336 0.02823 -0.0388 0.7035 0.0049
-12.000 -0.9799 0.03159 0.02633 -0.0385 0.7023 0.0050
-11.750 -0.9696 0.02997 0.02460 -0.0381 0.7010 0.0051
-11.500 -0.9576 0.02851 0.02303 -0.0378 0.6996 0.0051
-11.250 -0.9445 0.02714 0.02155 -0.0374 0.6980 0.0052
-11.000 -0.9299 0.02589 0.02020 -0.0371 0.6964 0.0052
-10.750 -0.9144 0.02473 0.01894 -0.0368 0.6949 0.0053
-10.500 -0.8995 0.02368 0.01779 -0.0363 0.6936 0.0053
-10.250 -0.8823 0.02269 0.01670 -0.0361 0.6923 0.0054
-10.000 -0.8623 0.02180 0.01572 -0.0361 0.6910 0.0054
-9.750 -0.8416 0.02099 0.01483 -0.0360 0.6898 0.0055
-9.500 -0.8201 0.02023 0.01399 -0.0358 0.6884 0.0055
-9.250 -0.7979 0.01953 0.01322 -0.0358 0.6872 0.0055
-9.000 -0.7778 0.01845 0.01206 -0.0355 0.6861 0.0056
-8.750 -0.7560 0.01755 0.01111 -0.0354 0.6850 0.0057
-8.500 -0.7328 0.01680 0.01030 -0.0354 0.6840 0.0058
-8.250 -0.7085 0.01615 0.00961 -0.0355 0.6829 0.0059
-8.000 -0.6835 0.01558 0.00899 -0.0357 0.6819 0.0060
-7.750 -0.6579 0.01505 0.00843 -0.0359 0.6808 0.0061
-7.500 -0.6317 0.01456 0.00791 -0.0361 0.6795 0.0062
-7.250 -0.6052 0.01411 0.00742 -0.0364 0.6783 0.0064
-7.000 -0.5782 0.01371 0.00700 -0.0367 0.6770 0.0066
-6.750 -0.5509 0.01333 0.00658 -0.0370 0.6759 0.0068
-6.500 -0.5234 0.01295 0.00617 -0.0374 0.6748 0.0070
-6.250 -0.4956 0.01259 0.00577 -0.0377 0.6737 0.0072
-6.000 -0.4676 0.01225 0.00540 -0.0381 0.6726 0.0074
-5.750 -0.4393 0.01195 0.00507 -0.0385 0.6714 0.0076
-5.500 -0.4107 0.01164 0.00473 -0.0390 0.6705 0.0078
-5.250 -0.3820 0.01130 0.00438 -0.0394 0.6695 0.0083
-5.000 -0.3531 0.01103 0.00411 -0.0399 0.6684 0.0088
-4.750 -0.3240 0.01081 0.00388 -0.0404 0.6674 0.0093
-4.500 -0.2947 0.01060 0.00366 -0.0409 0.6663 0.0099
-4.250 -0.2654 0.01039 0.00345 -0.0414 0.6651 0.0109
-4.000 -0.2359 0.01019 0.00325 -0.0419 0.6637 0.0130
-3.750 -0.2064 0.00995 0.00306 -0.0424 0.6624 0.0213
-3.500 -0.1768 0.00957 0.00282 -0.0432 0.6612 0.0567
-3.250 -0.1463 0.00836 0.00228 -0.0451 0.6599 0.2333
-3.000 -0.1148 0.00735 0.00186 -0.0470 0.6584 0.3902
-2.750 -0.0828 0.00654 0.00163 -0.0487 0.6566 0.5500
-2.500 -0.0525 0.00650 0.00164 -0.0492 0.6547 0.5755
-2.250 -0.0223 0.00649 0.00165 -0.0497 0.6526 0.5906
-2.000 0.0079 0.00649 0.00164 -0.0501 0.6501 0.5985
-1.750 0.0380 0.00648 0.00161 -0.0506 0.6475 0.6034
-1.500 0.0681 0.00648 0.00160 -0.0510 0.6448 0.6080
-1.250 0.0980 0.00649 0.00157 -0.0514 0.6420 0.6116
-1.000 0.1281 0.00650 0.00155 -0.0519 0.6391 0.6142
-0.750 0.1583 0.00650 0.00153 -0.0523 0.6358 0.6167
-0.500 0.1883 0.00648 0.00152 -0.0528 0.6323 0.6192
-0.250 0.2183 0.00648 0.00152 -0.0532 0.6283 0.6216
0.000 0.2481 0.00649 0.00151 -0.0536 0.6245 0.6242
0.250 0.2782 0.00649 0.00152 -0.0541 0.6199 0.6268
0.500 0.3081 0.00650 0.00152 -0.0545 0.6138 0.6289
0.750 0.3380 0.00651 0.00150 -0.0549 0.6070 0.6304
1.000 0.3678 0.00652 0.00149 -0.0553 0.5978 0.6316
1.250 0.3975 0.00655 0.00149 -0.0557 0.5874 0.6328
1.500 0.4270 0.00658 0.00149 -0.0561 0.5735 0.6342
1.750 0.4561 0.00665 0.00151 -0.0564 0.5547 0.6356
2.000 0.4849 0.00679 0.00156 -0.0566 0.5302 0.6367
2.250 0.5131 0.00700 0.00166 -0.0568 0.4972 0.6380
2.500 0.5410 0.00726 0.00178 -0.0570 0.4626 0.6393
2.750 0.5689 0.00753 0.00193 -0.0572 0.4310 0.6407
3.000 0.5965 0.00783 0.00209 -0.0573 0.3964 0.6420
3.250 0.6238 0.00816 0.00227 -0.0575 0.3602 0.6432
3.750 0.6791 0.00870 0.00260 -0.0578 0.3071 0.6456
4.000 0.7065 0.00899 0.00279 -0.0579 0.2820 0.6468
4.250 0.7340 0.00926 0.00296 -0.0580 0.2600 0.6479
4.500 0.7616 0.00950 0.00314 -0.0582 0.2413 0.6491
4.750 0.7883 0.00982 0.00337 -0.0582 0.2162 0.6503
5.000 0.8146 0.01018 0.00361 -0.0582 0.1907 0.6515
5.500 0.8685 0.01074 0.00407 -0.0583 0.1601 0.6541
6.000 0.9220 0.01129 0.00454 -0.0583 0.1349 0.6567
6.250 0.9484 0.01159 0.00480 -0.0583 0.1229 0.6579
6.500 0.9747 0.01190 0.00507 -0.0583 0.1121 0.6591
6.750 1.0007 0.01222 0.00535 -0.0582 0.1021 0.6603
7.000 1.0263 0.01257 0.00565 -0.0581 0.0917 0.6616
7.250 1.0522 0.01289 0.00595 -0.0580 0.0838 0.6629
7.500 1.0775 0.01324 0.00627 -0.0578 0.0760 0.6639
7.750 1.1026 0.01359 0.00661 -0.0576 0.0693 0.6652
8.000 1.1279 0.01391 0.00694 -0.0574 0.0638 0.6665
8.250 1.1521 0.01432 0.00732 -0.0571 0.0572 0.6678
8.500 1.1769 0.01466 0.00767 -0.0568 0.0530 0.6690
8.750 1.2006 0.01508 0.00809 -0.0565 0.0482 0.6703
9.000 1.2247 0.01545 0.00848 -0.0561 0.0450 0.6717
9.250 1.2477 0.01589 0.00892 -0.0557 0.0414 0.6731
9.500 1.2708 0.01631 0.00937 -0.0552 0.0387 0.6746
9.750 1.2936 0.01673 0.00981 -0.0547 0.0367 0.6761
10.000 1.3154 0.01721 0.01030 -0.0541 0.0345 0.6776
10.250 1.3365 0.01771 0.01082 -0.0533 0.0324 0.6789
10.500 1.3579 0.01816 0.01131 -0.0527 0.0310 0.6800
10.750 1.3780 0.01866 0.01185 -0.0518 0.0294 0.6814
11.000 1.3963 0.01927 0.01248 -0.0508 0.0274 0.6830
11.250 1.4145 0.01982 0.01308 -0.0497 0.0259 0.6845
11.500 1.4277 0.02040 0.01369 -0.0478 0.0243 0.6861
11.750 1.4413 0.02112 0.01445 -0.0462 0.0228 0.6877
12.000 1.4551 0.02192 0.01529 -0.0449 0.0217 0.6894
12.250 1.4695 0.02273 0.01617 -0.0437 0.0209 0.6911
12.500 1.4829 0.02368 0.01718 -0.0428 0.0200 0.6928
12.750 1.4956 0.02479 0.01834 -0.0421 0.0191 0.6943
13.000 1.5076 0.02604 0.01963 -0.0414 0.0182 0.6958
13.250 1.5198 0.02733 0.02099 -0.0409 0.0175 0.6977
13.500 1.5321 0.02861 0.02234 -0.0405 0.0169 0.6998
13.750 1.5434 0.02998 0.02379 -0.0400 0.0163 0.7021
14.000 1.5534 0.03147 0.02534 -0.0394 0.0155 0.7044
14.250 1.5618 0.03308 0.02700 -0.0388 0.0148 0.7066
14.500 1.5695 0.03478 0.02876 -0.0382 0.0141 0.7087
14.750 1.5775 0.03642 0.03048 -0.0377 0.0137 0.7108
15.250 1.5899 0.04009 0.03430 -0.0365 0.0126 0.7154
15.500 1.5939 0.04213 0.03642 -0.0359 0.0121 0.7181
15.750 1.5962 0.04437 0.03873 -0.0354 0.0116 0.7208
16.000 1.5983 0.04666 0.04111 -0.0349 0.0111 0.7237
16.250 1.6006 0.04896 0.04351 -0.0345 0.0108 0.7265
16.500 1.6014 0.05147 0.04611 -0.0343 0.0104 0.7296
16.750 1.6015 0.05422 0.04896 -0.0342 0.0100 0.7333
17.000 1.6006 0.05721 0.05204 -0.0343 0.0096 0.7373
17.250 1.5983 0.06045 0.05537 -0.0346 0.0092 0.7414
17.500 1.5945 0.06399 0.05902 -0.0350 0.0089 0.7458
17.750 1.5911 0.06762 0.06276 -0.0357 0.0086 0.7513
18.000 1.5867 0.07147 0.06673 -0.0366 0.0084 0.7575
18.250 1.5806 0.07567 0.07106 -0.0376 0.0081 0.7651
18.500 1.5724 0.08026 0.07578 -0.0390 0.0078 0.7743
18.750 1.5630 0.08516 0.08083 -0.0406 0.0076 0.7866
19.000 1.5508 0.09058 0.08641 -0.0425 0.0074 0.8034
19.250 1.5375 0.09627 0.09233 -0.0447 0.0072 0.8427
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