AVISTAR (avistar-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: AVISTAR (avistar-il) Reynolds number: 100,000 Max Cl/Cd: 49.14 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-avistar-il-100000.txt Download as CSV file: xf-avistar-il-100000.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 = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.750 -0.4497 0.10465 0.09950 -0.0443 1.0000 0.1514
-9.500 -0.3914 0.10211 0.09688 -0.0363 1.0000 0.1568
-9.250 -0.3974 0.09922 0.09406 -0.0381 1.0000 0.1654
-9.000 -0.4121 0.09485 0.08979 -0.0404 1.0000 0.1705
-8.750 -0.3878 0.09299 0.08793 -0.0376 1.0000 0.1769
-8.500 -0.4521 0.08924 0.08441 -0.0428 1.0000 0.1843
-8.250 -0.4033 0.08689 0.08201 -0.0379 1.0000 0.1909
-8.000 -0.4189 0.08500 0.08024 -0.0362 1.0000 0.1978
-7.750 -0.4723 0.08372 0.07915 -0.0323 1.0000 0.1995
-7.500 -0.5253 0.08249 0.07802 -0.0272 1.0000 0.2001
-7.250 -0.6016 0.08058 0.07606 -0.0236 1.0000 0.2018
-7.000 -0.5412 0.07858 0.07423 -0.0201 1.0000 0.2101
-6.750 -0.5845 0.07624 0.07188 -0.0176 1.0000 0.2172
-6.500 -0.5909 0.07361 0.06931 -0.0146 1.0000 0.2242
-6.250 -0.5930 0.07049 0.06614 -0.0154 0.9965 0.2401
-6.000 -0.5650 0.06789 0.06355 -0.0166 0.9910 0.2590
-5.750 -0.5351 0.06561 0.06128 -0.0176 0.9853 0.2797
-5.250 -0.5276 0.04082 0.03317 -0.0299 0.9647 0.1228
-5.000 -0.4881 0.03777 0.02931 -0.0312 0.9591 0.1060
-4.750 -0.4592 0.03502 0.02639 -0.0318 0.9515 0.1020
-4.500 -0.4203 0.03283 0.02355 -0.0334 0.9453 0.0964
-4.250 -0.3869 0.03148 0.02192 -0.0343 0.9376 0.0960
-4.000 -0.3480 0.03005 0.02033 -0.0364 0.9306 0.0967
-3.750 -0.2986 0.02865 0.01877 -0.0402 0.9265 0.0965
-3.500 -0.2714 0.02774 0.01781 -0.0400 0.9161 0.0968
-3.250 -0.2233 0.02654 0.01662 -0.0436 0.9110 0.0985
-3.000 -0.1902 0.02581 0.01593 -0.0446 0.9021 0.1018
-2.750 -0.1484 0.02496 0.01510 -0.0470 0.8952 0.1049
-2.500 -0.1028 0.02398 0.01418 -0.0500 0.8910 0.1081
-2.250 -0.0838 0.02354 0.01380 -0.0483 0.8785 0.1120
-2.000 -0.0431 0.02284 0.01308 -0.0503 0.8730 0.1213
-1.750 -0.0230 0.02248 0.01278 -0.0487 0.8605 0.1318
-1.500 0.0099 0.02117 0.01207 -0.0493 0.8545 0.2217
-1.250 0.0144 0.01959 0.01247 -0.0443 0.8423 0.6568
-1.000 0.0662 0.01926 0.01275 -0.0456 0.8377 0.8519
-0.750 0.1532 0.01954 0.01292 -0.0540 0.8353 0.9266
-0.500 0.2543 0.01997 0.01314 -0.0663 0.8300 0.9579
-0.250 0.3595 0.02000 0.01300 -0.0804 0.8229 0.9904
0.000 0.4101 0.01956 0.01243 -0.0850 0.8153 1.0000
0.250 0.4251 0.01959 0.01241 -0.0836 0.8012 1.0000
0.500 0.4419 0.01955 0.01230 -0.0821 0.7897 1.0000
0.750 0.4602 0.01941 0.01207 -0.0807 0.7796 1.0000
1.000 0.4761 0.01954 0.01217 -0.0792 0.7678 1.0000
1.250 0.4965 0.01939 0.01193 -0.0779 0.7599 1.0000
1.500 0.5117 0.01962 0.01215 -0.0763 0.7481 1.0000
1.750 0.5337 0.01938 0.01180 -0.0748 0.7406 1.0000
2.000 0.5491 0.01952 0.01192 -0.0729 0.7277 1.0000
2.250 0.5699 0.01935 0.01169 -0.0712 0.7177 1.0000
2.500 0.5904 0.01926 0.01155 -0.0696 0.7072 1.0000
2.750 0.6100 0.01941 0.01167 -0.0682 0.6974 1.0000
3.000 0.6330 0.01939 0.01162 -0.0670 0.6890 1.0000
3.250 0.6532 0.01963 0.01185 -0.0657 0.6798 1.0000
3.500 0.6770 0.01964 0.01183 -0.0647 0.6714 1.0000
3.750 0.6981 0.01988 0.01210 -0.0635 0.6622 1.0000
4.000 0.7228 0.01987 0.01207 -0.0625 0.6535 1.0000
4.250 0.7443 0.01992 0.01212 -0.0610 0.6412 1.0000
4.500 0.7690 0.01954 0.01168 -0.0595 0.6260 1.0000
4.750 0.7930 0.01916 0.01122 -0.0579 0.6084 1.0000
5.000 0.8164 0.01895 0.01095 -0.0563 0.5913 1.0000
5.250 0.8388 0.01883 0.01079 -0.0547 0.5735 1.0000
5.500 0.8603 0.01878 0.01069 -0.0530 0.5545 1.0000
5.750 0.8810 0.01877 0.01064 -0.0511 0.5342 1.0000
6.000 0.9007 0.01877 0.01059 -0.0491 0.5116 1.0000
6.250 0.9179 0.01885 0.01063 -0.0467 0.4857 1.0000
6.500 0.9327 0.01898 0.01069 -0.0440 0.4544 1.0000
6.750 0.9449 0.01924 0.01092 -0.0409 0.4156 1.0000
7.000 0.9550 0.01970 0.01122 -0.0375 0.3602 1.0000
7.250 0.9568 0.02074 0.01171 -0.0331 0.2869 1.0000
7.500 0.9559 0.02222 0.01267 -0.0287 0.2134 1.0000
7.750 0.9418 0.02454 0.01414 -0.0229 0.1072 1.0000
8.000 0.9399 0.02604 0.01541 -0.0186 0.0914 1.0000
8.250 0.9427 0.02721 0.01658 -0.0150 0.0852 1.0000
8.500 0.9437 0.02858 0.01795 -0.0115 0.0813 1.0000
8.750 0.9484 0.02984 0.01929 -0.0087 0.0789 1.0000
9.000 0.9529 0.03120 0.02074 -0.0061 0.0769 1.0000
9.250 0.9566 0.03271 0.02232 -0.0037 0.0752 1.0000
9.500 0.9598 0.03434 0.02399 -0.0015 0.0739 1.0000
9.750 0.9633 0.03604 0.02570 0.0006 0.0727 1.0000
10.000 0.9692 0.03770 0.02733 0.0026 0.0717 1.0000
10.250 0.9823 0.03895 0.02858 0.0041 0.0706 1.0000
10.500 0.9992 0.04005 0.02969 0.0054 0.0692 1.0000
10.750 1.0205 0.04105 0.03067 0.0065 0.0676 1.0000
11.000 1.0491 0.04195 0.03153 0.0071 0.0664 1.0000
11.250 1.0861 0.04291 0.03245 0.0070 0.0657 1.0000
11.500 1.1284 0.04418 0.03375 0.0062 0.0653 1.0000
11.750 1.1707 0.04589 0.03554 0.0049 0.0653 1.0000
12.000 1.2033 0.04792 0.03777 0.0044 0.0656 1.0000
12.250 1.2275 0.05012 0.04020 0.0046 0.0657 1.0000
12.500 1.2439 0.05240 0.04271 0.0056 0.0656 1.0000
12.750 1.2535 0.05475 0.04531 0.0072 0.0657 1.0000
13.000 1.2560 0.05723 0.04808 0.0095 0.0661 1.0000
13.250 1.2551 0.06000 0.05118 0.0118 0.0669 1.0000
13.500 1.2534 0.06308 0.05455 0.0139 0.0680 1.0000
13.750 1.2524 0.06646 0.05818 0.0155 0.0691 1.0000
14.000 1.2593 0.07041 0.06232 0.0163 0.0704 1.0000
14.250 1.2753 0.07401 0.06609 0.0167 0.0721 1.0000
14.500 1.2299 0.07693 0.06940 0.0201 0.0727 1.0000
14.750 1.1807 0.08172 0.07461 0.0213 0.0736 1.0000
15.000 1.1340 0.08816 0.08140 0.0205 0.0748 1.0000
15.250 1.0895 0.09585 0.08938 0.0180 0.0759 1.0000
15.500 1.0452 0.10486 0.09865 0.0139 0.0772 1.0000
15.750 0.9977 0.11590 0.10988 0.0079 0.0786 1.0000
16.000 1.0068 0.12011 0.11414 0.0078 0.0816 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AVISTAR (avistar-il)