Joukovsky f=0% t=15% (joukowsk0015-jf) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=15% (joukowsk0015-jf) Reynolds number: 1,000,000 Max Cl/Cd: 81.98 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0015-jf-1000000-n5.txt Download as CSV file: xf-joukowsk0015-jf-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Joukovsky f=0% t=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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3203 0.10667 0.10294 0.0091 1.0000 0.0224
-19.500 -1.3377 0.09973 0.09589 0.0051 1.0000 0.0227
-19.250 -1.3545 0.09305 0.08911 0.0013 1.0000 0.0229
-19.000 -1.3698 0.08677 0.08272 -0.0022 1.0000 0.0231
-18.750 -1.3844 0.08077 0.07661 -0.0054 1.0000 0.0233
-18.500 -1.3976 0.07512 0.07086 -0.0084 1.0000 0.0237
-18.250 -1.4106 0.06966 0.06530 -0.0111 1.0000 0.0239
-18.000 -1.4215 0.06464 0.06018 -0.0136 1.0000 0.0243
-17.750 -1.4301 0.06011 0.05555 -0.0157 1.0000 0.0246
-17.500 -1.4379 0.05584 0.05119 -0.0176 1.0000 0.0248
-17.250 -1.4443 0.05190 0.04715 -0.0192 1.0000 0.0251
-17.000 -1.4513 0.04803 0.04319 -0.0206 1.0000 0.0253
-16.750 -1.4575 0.04435 0.03943 -0.0219 1.0000 0.0258
-16.500 -1.4609 0.04112 0.03612 -0.0228 1.0000 0.0261
-16.250 -1.4621 0.03824 0.03317 -0.0235 1.0000 0.0266
-16.000 -1.4618 0.03561 0.03048 -0.0240 1.0000 0.0270
-15.750 -1.4596 0.03328 0.02808 -0.0242 1.0000 0.0275
-15.500 -1.4558 0.03119 0.02592 -0.0242 1.0000 0.0280
-15.250 -1.4508 0.02933 0.02399 -0.0241 1.0000 0.0285
-15.000 -1.4448 0.02764 0.02224 -0.0237 1.0000 0.0290
-14.750 -1.4403 0.02594 0.02050 -0.0231 1.0000 0.0296
-14.500 -1.4341 0.02450 0.01901 -0.0223 1.0000 0.0304
-14.250 -1.4267 0.02327 0.01773 -0.0213 1.0000 0.0311
-14.000 -1.4185 0.02220 0.01662 -0.0200 1.0000 0.0319
-13.750 -1.4093 0.02130 0.01567 -0.0185 1.0000 0.0326
-13.500 -1.4011 0.02048 0.01480 -0.0166 1.0000 0.0333
-13.250 -1.3927 0.01975 0.01405 -0.0143 1.0000 0.0341
-13.000 -1.3792 0.01913 0.01341 -0.0126 1.0000 0.0352
-12.750 -1.3616 0.01857 0.01282 -0.0115 1.0000 0.0363
-12.500 -1.3424 0.01805 0.01227 -0.0105 1.0000 0.0374
-12.250 -1.3232 0.01748 0.01170 -0.0095 1.0000 0.0388
-12.000 -1.3025 0.01698 0.01118 -0.0087 1.0000 0.0402
-11.750 -1.2805 0.01653 0.01071 -0.0081 1.0000 0.0415
-11.500 -1.2583 0.01606 0.01023 -0.0074 1.0000 0.0431
-11.250 -1.2357 0.01560 0.00977 -0.0068 1.0000 0.0449
-11.000 -1.2120 0.01520 0.00937 -0.0063 1.0000 0.0468
-10.750 -1.1883 0.01477 0.00894 -0.0058 1.0000 0.0488
-10.500 -1.1640 0.01437 0.00854 -0.0054 1.0000 0.0510
-10.250 -1.1389 0.01403 0.00819 -0.0051 1.0000 0.0530
-10.000 -1.1142 0.01362 0.00780 -0.0047 1.0000 0.0557
-9.750 -1.0887 0.01328 0.00746 -0.0044 1.0000 0.0585
-9.500 -1.0570 0.01295 0.00711 -0.0053 0.9426 0.0616
-9.250 -1.0353 0.01273 0.00682 -0.0040 0.9060 0.0647
-9.000 -1.0118 0.01250 0.00652 -0.0031 0.8804 0.0679
-8.750 -0.9873 0.01223 0.00621 -0.0025 0.8586 0.0717
-8.500 -0.9618 0.01200 0.00593 -0.0020 0.8393 0.0753
-8.250 -0.9360 0.01174 0.00563 -0.0016 0.8213 0.0799
-8.000 -0.9096 0.01152 0.00537 -0.0013 0.8050 0.0840
-7.750 -0.8832 0.01127 0.00509 -0.0010 0.7889 0.0891
-7.250 -0.8292 0.01082 0.00460 -0.0005 0.7584 0.1000
-7.000 -0.8020 0.01060 0.00437 -0.0003 0.7446 0.1060
-6.750 -0.7745 0.01040 0.00414 -0.0002 0.7305 0.1124
-6.500 -0.7471 0.01018 0.00392 0.0000 0.7164 0.1197
-6.250 -0.7192 0.01000 0.00373 0.0001 0.7031 0.1265
-6.000 -0.6915 0.00980 0.00352 0.0002 0.6902 0.1347
-5.750 -0.6635 0.00962 0.00334 0.0003 0.6768 0.1427
-5.500 -0.6353 0.00946 0.00317 0.0003 0.6641 0.1509
-5.250 -0.6072 0.00928 0.00300 0.0004 0.6515 0.1606
-5.000 -0.5789 0.00913 0.00284 0.0004 0.6384 0.1696
-4.750 -0.5505 0.00898 0.00269 0.0005 0.6264 0.1795
-4.500 -0.5221 0.00883 0.00255 0.0005 0.6139 0.1899
-4.250 -0.4934 0.00870 0.00242 0.0005 0.6013 0.1995
-4.000 -0.4648 0.00858 0.00230 0.0005 0.5895 0.2105
-3.500 -0.4073 0.00834 0.00208 0.0005 0.5649 0.2325
-3.250 -0.3785 0.00825 0.00199 0.0005 0.5533 0.2437
-3.000 -0.3496 0.00814 0.00190 0.0005 0.5406 0.2557
-2.750 -0.3206 0.00806 0.00181 0.0005 0.5293 0.2667
-2.500 -0.2916 0.00799 0.00174 0.0004 0.5172 0.2786
-2.250 -0.2626 0.00791 0.00168 0.0004 0.5051 0.2907
-2.000 -0.2335 0.00785 0.00162 0.0004 0.4935 0.3019
-1.500 -0.1753 0.00774 0.00152 0.0003 0.4693 0.3262
-1.250 -0.1461 0.00770 0.00148 0.0002 0.4576 0.3378
-1.000 -0.1169 0.00768 0.00146 0.0002 0.4451 0.3498
-0.750 -0.0877 0.00764 0.00143 0.0002 0.4338 0.3624
-0.500 -0.0585 0.00763 0.00141 0.0001 0.4218 0.3737
-0.250 -0.0292 0.00762 0.00140 0.0001 0.4095 0.3858
0.000 0.0000 0.00761 0.00140 0.0000 0.3981 0.3981
0.250 0.0292 0.00762 0.00140 -0.0001 0.3857 0.4096
0.500 0.0585 0.00763 0.00141 -0.0001 0.3737 0.4217
0.750 0.0877 0.00764 0.00143 -0.0002 0.3624 0.4337
1.000 0.1169 0.00768 0.00146 -0.0002 0.3498 0.4451
1.250 0.1461 0.00770 0.00148 -0.0002 0.3378 0.4576
1.500 0.1753 0.00774 0.00152 -0.0003 0.3262 0.4693
2.000 0.2335 0.00785 0.00162 -0.0004 0.3019 0.4935
2.250 0.2626 0.00791 0.00168 -0.0004 0.2906 0.5049
2.500 0.2916 0.00799 0.00174 -0.0004 0.2786 0.5171
2.750 0.3206 0.00806 0.00181 -0.0005 0.2666 0.5294
3.000 0.3496 0.00814 0.00190 -0.0005 0.2556 0.5407
3.250 0.3785 0.00825 0.00199 -0.0005 0.2437 0.5532
3.500 0.4073 0.00834 0.00208 -0.0005 0.2323 0.5649
4.000 0.4648 0.00858 0.00230 -0.0005 0.2104 0.5895
4.250 0.4934 0.00870 0.00242 -0.0005 0.1997 0.6013
4.500 0.5221 0.00883 0.00255 -0.0005 0.1899 0.6139
4.750 0.5505 0.00898 0.00269 -0.0005 0.1795 0.6263
5.000 0.5789 0.00913 0.00284 -0.0004 0.1697 0.6384
5.250 0.6072 0.00928 0.00300 -0.0004 0.1606 0.6516
5.500 0.6353 0.00946 0.00317 -0.0003 0.1509 0.6641
5.750 0.6635 0.00963 0.00334 -0.0003 0.1426 0.6768
6.000 0.6915 0.00980 0.00352 -0.0002 0.1348 0.6902
6.250 0.7192 0.01000 0.00373 -0.0001 0.1264 0.7032
6.500 0.7471 0.01018 0.00392 0.0000 0.1196 0.7165
6.750 0.7745 0.01040 0.00414 0.0002 0.1123 0.7304
7.000 0.8020 0.01060 0.00437 0.0004 0.1059 0.7444
7.250 0.8292 0.01082 0.00460 0.0005 0.1000 0.7583
7.500 0.8563 0.01105 0.00484 0.0007 0.0943 0.7735
7.750 0.8831 0.01127 0.00509 0.0010 0.0891 0.7889
8.000 0.9096 0.01152 0.00537 0.0013 0.0840 0.8049
8.250 0.9360 0.01174 0.00563 0.0016 0.0798 0.8213
8.500 0.9617 0.01201 0.00593 0.0020 0.0752 0.8393
8.750 0.9873 0.01223 0.00621 0.0025 0.0717 0.8585
9.000 1.0118 0.01249 0.00652 0.0031 0.0679 0.8803
9.250 1.0354 0.01273 0.00682 0.0040 0.0647 0.9059
9.500 1.0570 0.01295 0.00711 0.0053 0.0616 0.9425
9.750 1.0887 0.01328 0.00746 0.0044 0.0585 1.0000
10.000 1.1142 0.01362 0.00780 0.0047 0.0557 1.0000
10.250 1.1389 0.01403 0.00819 0.0051 0.0530 1.0000
10.500 1.1639 0.01437 0.00854 0.0054 0.0510 1.0000
10.750 1.1882 0.01477 0.00894 0.0059 0.0488 1.0000
11.000 1.2119 0.01520 0.00936 0.0063 0.0469 1.0000
11.250 1.2356 0.01560 0.00977 0.0068 0.0448 1.0000
11.500 1.2583 0.01606 0.01023 0.0074 0.0430 1.0000
11.750 1.2805 0.01653 0.01071 0.0081 0.0415 1.0000
12.000 1.3026 0.01698 0.01118 0.0087 0.0402 1.0000
12.250 1.3233 0.01748 0.01169 0.0095 0.0387 1.0000
12.500 1.3424 0.01806 0.01228 0.0105 0.0373 1.0000
12.750 1.3617 0.01857 0.01282 0.0114 0.0363 1.0000
13.000 1.3793 0.01913 0.01341 0.0126 0.0351 1.0000
13.250 1.3928 0.01975 0.01405 0.0143 0.0341 1.0000
13.500 1.4012 0.02047 0.01480 0.0165 0.0333 1.0000
13.750 1.4095 0.02129 0.01566 0.0185 0.0326 1.0000
14.000 1.4186 0.02219 0.01661 0.0200 0.0319 1.0000
14.250 1.4271 0.02324 0.01771 0.0213 0.0313 1.0000
14.500 1.4346 0.02447 0.01899 0.0223 0.0305 1.0000
14.750 1.4410 0.02590 0.02045 0.0231 0.0298 1.0000
15.000 1.4455 0.02760 0.02220 0.0237 0.0289 1.0000
15.250 1.4512 0.02931 0.02397 0.0240 0.0285 1.0000
15.500 1.4567 0.03115 0.02588 0.0242 0.0281 1.0000
15.750 1.4604 0.03324 0.02804 0.0241 0.0275 1.0000
16.000 1.4628 0.03556 0.03042 0.0239 0.0270 1.0000
16.250 1.4634 0.03815 0.03308 0.0234 0.0266 1.0000
16.500 1.4622 0.04104 0.03604 0.0227 0.0261 1.0000
16.750 1.4583 0.04433 0.03941 0.0218 0.0257 1.0000
17.000 1.4532 0.04787 0.04303 0.0206 0.0254 1.0000
17.250 1.4465 0.05170 0.04695 0.0191 0.0250 1.0000
17.500 1.4401 0.05564 0.05098 0.0175 0.0248 1.0000
17.750 1.4322 0.05993 0.05536 0.0157 0.0246 1.0000
18.000 1.4237 0.06444 0.05997 0.0136 0.0241 1.0000
18.250 1.4126 0.06948 0.06512 0.0111 0.0239 1.0000
18.500 1.4001 0.07486 0.07060 0.0084 0.0236 1.0000
18.750 1.3865 0.08058 0.07642 0.0053 0.0233 1.0000
19.000 1.3722 0.08653 0.08248 0.0021 0.0232 1.0000
19.250 1.3570 0.09279 0.08885 -0.0013 0.0230 1.0000
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