AUGUST 160 (august160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AUGUST 160 (august160-il) Reynolds number: 1,000,000 Max Cl/Cd: 117.23 at α=11° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-august160-il-1000000.txt Download as CSV file: xf-august160-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AUGUST 160
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.1192 0.11917 0.11575 -0.0374 0.4897 0.0123
-12.500 -0.1141 0.11616 0.11272 -0.0387 0.4851 0.0122
-12.250 -0.1888 0.11992 0.11627 -0.0416 0.5021 0.0117
-12.000 -0.1813 0.11698 0.11331 -0.0430 0.4956 0.0122
-11.750 -0.1760 0.11338 0.10968 -0.0447 0.4892 0.0128
-11.500 -0.1780 0.10780 0.10410 -0.0479 0.4870 0.0135
-11.250 -0.1739 0.10398 0.10029 -0.0497 0.4826 0.0135
-11.000 -0.1734 0.09915 0.09545 -0.0521 0.4785 0.0136
-10.750 -0.1693 0.09548 0.09178 -0.0538 0.4734 0.0136
-10.250 -0.0948 0.08255 0.07900 -0.0507 0.4473 0.0142
-10.000 -0.0927 0.07901 0.07547 -0.0517 0.4440 0.0143
-9.750 -0.0906 0.07556 0.07201 -0.0528 0.4398 0.0144
-9.500 -0.0900 0.07189 0.06833 -0.0539 0.4356 0.0145
-9.250 -0.0909 0.06806 0.06449 -0.0551 0.4319 0.0148
-9.000 -0.0931 0.06399 0.06044 -0.0565 0.4294 0.0150
-8.750 -0.0991 0.05935 0.05581 -0.0583 0.4277 0.0151
-8.500 -0.1086 0.05432 0.05081 -0.0605 0.4255 0.0155
-8.250 -0.1219 0.04912 0.04564 -0.0634 0.4241 0.0154
-8.000 -0.1580 0.04238 0.03891 -0.0685 0.4248 0.0152
-7.750 -0.1862 0.03784 0.03431 -0.0670 0.4239 0.0153
-7.500 -0.2022 0.03277 0.02913 -0.0659 0.4222 0.0152
-7.250 -0.2657 0.01873 0.01433 -0.0601 0.4268 0.0170
-7.000 -0.2530 0.01719 0.01270 -0.0586 0.4219 0.0171
-6.750 -0.2385 0.01594 0.01134 -0.0572 0.4164 0.0173
-6.500 -0.2219 0.01497 0.01029 -0.0559 0.4112 0.0176
-6.250 -0.2224 0.01150 0.00615 -0.0518 0.4090 0.0201
-6.000 -0.2021 0.01046 0.00510 -0.0509 0.4044 0.0204
-5.750 -0.1815 0.00972 0.00429 -0.0500 0.3992 0.0207
-5.500 -0.1608 0.00904 0.00351 -0.0490 0.3937 0.0213
-5.250 -0.1505 0.01731 0.01061 -0.0470 0.3935 0.0160
-5.000 -0.1269 0.01610 0.00926 -0.0459 0.3902 0.0155
-4.750 -0.1027 0.01502 0.00801 -0.0448 0.3860 0.0151
-4.500 -0.0774 0.01463 0.00753 -0.0441 0.3815 0.0155
-4.250 -0.0528 0.01401 0.00679 -0.0432 0.3763 0.0154
-4.000 -0.0274 0.01338 0.00610 -0.0424 0.3737 0.0153
-3.750 -0.0022 0.01290 0.00557 -0.0416 0.3705 0.0152
-3.500 0.0229 0.01249 0.00511 -0.0408 0.3670 0.0153
-3.250 0.0479 0.01217 0.00473 -0.0400 0.3630 0.0156
-3.000 0.0727 0.01192 0.00442 -0.0391 0.3587 0.0159
-2.750 0.0988 0.01168 0.00415 -0.0385 0.3568 0.0163
-2.500 0.1247 0.01145 0.00390 -0.0378 0.3546 0.0164
-2.250 0.1501 0.01117 0.00360 -0.0371 0.3521 0.0169
-2.000 0.1755 0.01094 0.00334 -0.0364 0.3494 0.0173
-1.750 0.2014 0.01080 0.00318 -0.0358 0.3467 0.0178
-1.500 0.2274 0.01071 0.00305 -0.0352 0.3435 0.0183
-1.250 0.2535 0.01065 0.00296 -0.0346 0.3407 0.0188
-1.000 0.2804 0.01054 0.00285 -0.0342 0.3394 0.0195
-0.750 0.3070 0.01044 0.00274 -0.0337 0.3377 0.0208
-0.500 0.3338 0.01036 0.00266 -0.0333 0.3358 0.0227
-0.250 0.3595 0.01021 0.00259 -0.0327 0.3338 0.0461
0.000 0.3827 0.00987 0.00255 -0.0317 0.3317 0.1480
0.250 0.4057 0.00958 0.00254 -0.0308 0.3297 0.2469
0.500 0.4258 0.00917 0.00256 -0.0293 0.3273 0.3984
0.750 0.4423 0.00873 0.00262 -0.0271 0.3245 0.5761
1.000 0.4487 0.00797 0.00265 -0.0224 0.3239 0.8081
1.250 0.4740 0.00788 0.00283 -0.0214 0.3228 0.9117
1.500 0.5027 0.00798 0.00295 -0.0212 0.3215 0.9410
1.750 0.5358 0.00812 0.00309 -0.0219 0.3200 0.9585
2.000 0.5681 0.00825 0.00319 -0.0226 0.3185 0.9670
2.250 0.6069 0.00839 0.00329 -0.0248 0.3167 0.9702
2.500 0.6437 0.00856 0.00341 -0.0266 0.3150 0.9752
2.750 0.6844 0.00874 0.00354 -0.0293 0.3131 0.9774
3.000 0.7241 0.00895 0.00369 -0.0318 0.3106 0.9787
3.250 0.7635 0.00922 0.00391 -0.0343 0.3079 0.9805
3.500 0.8018 0.00932 0.00400 -0.0364 0.3072 0.9828
3.750 0.8356 0.00942 0.00409 -0.0377 0.3062 0.9861
4.000 0.8773 0.00951 0.00416 -0.0406 0.3047 0.9873
4.250 0.9134 0.00960 0.00423 -0.0424 0.3032 0.9884
4.500 0.9486 0.00967 0.00429 -0.0441 0.3014 0.9898
4.750 0.9812 0.00976 0.00436 -0.0452 0.2996 0.9911
5.000 1.0113 0.00986 0.00444 -0.0458 0.2977 0.9924
5.250 1.0413 0.01001 0.00457 -0.0465 0.2957 0.9939
5.500 1.0723 0.01019 0.00472 -0.0474 0.2940 0.9951
5.750 1.1077 0.01041 0.00493 -0.0492 0.2921 0.9967
6.000 1.1461 0.01049 0.00502 -0.0516 0.2916 0.9986
6.250 1.1766 0.01058 0.00514 -0.0524 0.2910 0.9995
6.500 1.2053 0.01068 0.00525 -0.0528 0.2902 1.0000
6.750 1.2267 0.01080 0.00540 -0.0517 0.2896 1.0000
7.000 1.2480 0.01092 0.00554 -0.0506 0.2888 1.0000
7.250 1.2690 0.01104 0.00568 -0.0495 0.2879 1.0000
7.500 1.2894 0.01118 0.00584 -0.0482 0.2871 1.0000
7.750 1.3096 0.01132 0.00600 -0.0469 0.2864 1.0000
8.000 1.3295 0.01145 0.00616 -0.0456 0.2855 1.0000
8.250 1.3493 0.01157 0.00630 -0.0443 0.2842 1.0000
8.500 1.3683 0.01172 0.00646 -0.0428 0.2831 1.0000
8.750 1.3867 0.01187 0.00662 -0.0412 0.2815 1.0000
9.000 1.4041 0.01207 0.00682 -0.0394 0.2795 1.0000
9.250 1.4208 0.01236 0.00711 -0.0376 0.2774 1.0000
9.500 1.4406 0.01252 0.00731 -0.0364 0.2768 1.0000
9.750 1.4621 0.01263 0.00746 -0.0354 0.2759 1.0000
10.000 1.4837 0.01279 0.00767 -0.0345 0.2752 1.0000
10.250 1.5058 0.01293 0.00785 -0.0338 0.2739 1.0000
10.500 1.5281 0.01308 0.00803 -0.0331 0.2725 1.0000
10.750 1.5502 0.01324 0.00824 -0.0324 0.2710 1.0000
11.000 1.5720 0.01341 0.00843 -0.0317 0.2692 1.0000
11.250 1.5929 0.01363 0.00867 -0.0308 0.2674 1.0000
11.500 1.6122 0.01391 0.00896 -0.0298 0.2648 1.0000
11.750 1.6309 0.01425 0.00931 -0.0287 0.2623 1.0000
12.000 1.6524 0.01440 0.00953 -0.0280 0.2609 1.0000
12.250 1.6721 0.01458 0.00978 -0.0270 0.2593 1.0000
12.500 1.6914 0.01479 0.01004 -0.0259 0.2573 1.0000
12.750 1.7098 0.01505 0.01034 -0.0248 0.2553 1.0000
13.000 1.7267 0.01537 0.01069 -0.0236 0.2524 1.0000
13.250 1.7416 0.01581 0.01115 -0.0222 0.2498 1.0000
13.500 1.7584 0.01621 0.01161 -0.0212 0.2475 1.0000
13.750 1.7784 0.01649 0.01197 -0.0206 0.2450 1.0000
14.000 1.7959 0.01691 0.01243 -0.0199 0.2407 1.0000
14.250 1.8091 0.01755 0.01310 -0.0188 0.2363 1.0000
14.500 1.8237 0.01819 0.01379 -0.0180 0.2316 1.0000
14.750 1.8332 0.01918 0.01479 -0.0170 0.2228 1.0000
15.000 1.8359 0.02076 0.01637 -0.0159 0.2118 1.0000
15.250 1.8300 0.02326 0.01886 -0.0150 0.2003 1.0000
15.500 1.8191 0.02656 0.02218 -0.0147 0.1890 1.0000
15.750 1.7911 0.03182 0.02746 -0.0149 0.1743 1.0000
16.000 1.7575 0.03787 0.03356 -0.0153 0.1653 1.0000
16.250 1.7259 0.04381 0.03958 -0.0158 0.1604 1.0000
16.500 1.6904 0.05022 0.04609 -0.0164 0.1562 1.0000
16.750 1.6537 0.05693 0.05289 -0.0172 0.1521 1.0000
17.000 1.6160 0.06408 0.06013 -0.0183 0.1488 1.0000
17.250 1.5854 0.07059 0.06672 -0.0195 0.1445 1.0000
17.500 1.5558 0.07712 0.07333 -0.0208 0.1386 1.0000
17.750 1.5231 0.08421 0.08048 -0.0224 0.1333 1.0000
18.000 1.4886 0.09167 0.08797 -0.0242 0.1242 1.0000
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