NACA CYH (nacacyh-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA CYH (nacacyh-il) Reynolds number: 1,000,000 Max Cl/Cd: 101.04 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-nacacyh-il-1000000-n5.txt Download as CSV file: xf-nacacyh-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA CYH
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
------ -------- --------- --------- -------- -------- --------
-17.250 -1.3140 0.03727 0.03419 -0.0711 1.0000 0.0104
-17.000 -1.3212 0.03455 0.03133 -0.0702 1.0000 0.0106
-16.750 -1.3238 0.03250 0.02913 -0.0683 1.0000 0.0108
-16.500 -1.3229 0.03083 0.02734 -0.0661 1.0000 0.0110
-16.250 -1.3178 0.02946 0.02589 -0.0637 1.0000 0.0114
-16.000 -1.3065 0.02830 0.02464 -0.0620 1.0000 0.0119
-15.750 -1.2924 0.02727 0.02355 -0.0605 1.0000 0.0123
-15.500 -1.2769 0.02631 0.02250 -0.0591 1.0000 0.0128
-15.250 -1.2605 0.02538 0.02148 -0.0577 1.0000 0.0132
-15.000 -1.2435 0.02447 0.02047 -0.0564 1.0000 0.0136
-14.750 -1.2253 0.02362 0.01952 -0.0551 1.0000 0.0140
-14.500 -1.2042 0.02303 0.01891 -0.0540 1.0000 0.0144
-14.250 -1.1821 0.02255 0.01840 -0.0531 1.0000 0.0149
-14.000 -1.1597 0.02208 0.01790 -0.0521 1.0000 0.0153
-13.750 -1.1373 0.02159 0.01736 -0.0512 1.0000 0.0158
-13.500 -1.1150 0.02108 0.01679 -0.0502 1.0000 0.0163
-13.250 -1.0927 0.02055 0.01619 -0.0493 1.0000 0.0167
-13.000 -1.0702 0.02003 0.01559 -0.0483 1.0000 0.0171
-12.750 -1.0474 0.01954 0.01502 -0.0473 1.0000 0.0174
-12.500 -1.0254 0.01895 0.01437 -0.0463 1.0000 0.0177
-12.250 -1.0023 0.01852 0.01392 -0.0453 1.0000 0.0181
-12.000 -0.9732 0.01815 0.01353 -0.0456 0.9923 0.0185
-11.750 -0.9419 0.01786 0.01320 -0.0462 0.9799 0.0188
-11.500 -0.9114 0.01757 0.01287 -0.0466 0.9640 0.0193
-11.250 -0.8851 0.01726 0.01249 -0.0461 0.9424 0.0197
-11.000 -0.8623 0.01694 0.01206 -0.0449 0.9137 0.0201
-10.750 -0.8397 0.01664 0.01161 -0.0436 0.8821 0.0205
-10.500 -0.8159 0.01638 0.01119 -0.0426 0.8532 0.0208
-10.250 -0.7912 0.01610 0.01076 -0.0417 0.8308 0.0212
-10.000 -0.7659 0.01583 0.01036 -0.0410 0.8125 0.0214
-9.750 -0.7401 0.01560 0.01002 -0.0404 0.7980 0.0216
-9.500 -0.7150 0.01518 0.00948 -0.0398 0.7855 0.0219
-9.250 -0.6912 0.01447 0.00868 -0.0390 0.7746 0.0224
-9.000 -0.6655 0.01408 0.00822 -0.0384 0.7654 0.0228
-8.750 -0.6394 0.01376 0.00783 -0.0379 0.7566 0.0232
-8.500 -0.6131 0.01342 0.00743 -0.0374 0.7492 0.0235
-8.250 -0.5866 0.01311 0.00706 -0.0370 0.7417 0.0238
-8.000 -0.5599 0.01283 0.00672 -0.0366 0.7355 0.0242
-7.750 -0.5332 0.01252 0.00636 -0.0362 0.7293 0.0245
-7.250 -0.4796 0.01191 0.00563 -0.0354 0.7178 0.0252
-7.000 -0.4526 0.01162 0.00528 -0.0350 0.7123 0.0255
-6.750 -0.4256 0.01136 0.00496 -0.0346 0.7066 0.0258
-6.500 -0.3983 0.01111 0.00466 -0.0343 0.6997 0.0261
-6.250 -0.3711 0.01089 0.00439 -0.0340 0.6923 0.0264
-6.000 -0.3434 0.01070 0.00415 -0.0337 0.6863 0.0267
-5.750 -0.3158 0.01052 0.00393 -0.0335 0.6794 0.0269
-5.500 -0.2883 0.01033 0.00370 -0.0332 0.6729 0.0270
-5.250 -0.2611 0.01003 0.00335 -0.0329 0.6665 0.0275
-5.000 -0.2337 0.00980 0.00307 -0.0327 0.6599 0.0280
-4.750 -0.2060 0.00960 0.00284 -0.0324 0.6525 0.0286
-4.500 -0.1783 0.00944 0.00264 -0.0322 0.6449 0.0291
-4.250 -0.1504 0.00928 0.00246 -0.0321 0.6379 0.0297
-4.000 -0.1226 0.00916 0.00230 -0.0319 0.6288 0.0303
-3.750 -0.0946 0.00904 0.00215 -0.0318 0.6193 0.0310
-3.500 -0.0666 0.00894 0.00202 -0.0317 0.6107 0.0317
-3.250 -0.0385 0.00885 0.00189 -0.0316 0.6024 0.0325
-3.000 -0.0103 0.00877 0.00178 -0.0315 0.5948 0.0333
-2.750 0.0178 0.00868 0.00168 -0.0314 0.5862 0.0354
-2.500 0.0458 0.00859 0.00159 -0.0313 0.5780 0.0388
-2.250 0.0736 0.00850 0.00150 -0.0313 0.5682 0.0477
-2.000 0.1012 0.00836 0.00144 -0.0312 0.5579 0.0715
-1.750 0.1290 0.00830 0.00138 -0.0311 0.5470 0.0846
-1.500 0.1568 0.00822 0.00134 -0.0311 0.5361 0.1028
-1.250 0.1843 0.00810 0.00130 -0.0310 0.5257 0.1336
-1.000 0.2116 0.00799 0.00127 -0.0309 0.5149 0.1736
-0.750 0.2390 0.00790 0.00126 -0.0309 0.5032 0.2111
-0.500 0.2661 0.00778 0.00126 -0.0308 0.4905 0.2641
-0.250 0.2931 0.00769 0.00127 -0.0307 0.4765 0.3126
0.000 0.3197 0.00758 0.00129 -0.0306 0.4598 0.3748
0.250 0.3445 0.00731 0.00131 -0.0302 0.4415 0.4981
0.500 0.3587 0.00630 0.00136 -0.0275 0.4249 0.8430
0.750 0.3838 0.00634 0.00146 -0.0268 0.4057 0.8894
1.000 0.4096 0.00646 0.00156 -0.0262 0.3874 0.9179
1.250 0.4365 0.00659 0.00167 -0.0260 0.3720 0.9359
1.500 0.4644 0.00674 0.00178 -0.0259 0.3596 0.9504
1.750 0.4923 0.00690 0.00188 -0.0260 0.3484 0.9606
2.000 0.5225 0.00706 0.00198 -0.0266 0.3367 0.9662
2.250 0.5504 0.00720 0.00208 -0.0266 0.3270 0.9726
2.500 0.5825 0.00738 0.00220 -0.0278 0.3162 0.9758
2.750 0.6140 0.00754 0.00231 -0.0287 0.3062 0.9796
3.000 0.6440 0.00768 0.00242 -0.0293 0.2998 0.9841
3.250 0.6784 0.00783 0.00253 -0.0310 0.2916 0.9855
3.500 0.7107 0.00797 0.00265 -0.0323 0.2843 0.9867
3.750 0.7421 0.00809 0.00275 -0.0333 0.2783 0.9878
4.000 0.7728 0.00825 0.00287 -0.0342 0.2715 0.9892
4.250 0.8034 0.00837 0.00299 -0.0351 0.2648 0.9907
4.500 0.8334 0.00854 0.00312 -0.0359 0.2573 0.9923
4.750 0.8632 0.00867 0.00325 -0.0366 0.2509 0.9940
5.000 0.8943 0.00887 0.00341 -0.0378 0.2401 0.9949
5.250 0.9245 0.00915 0.00359 -0.0388 0.2191 0.9959
5.500 0.9525 0.00967 0.00390 -0.0395 0.1824 0.9973
5.750 0.9804 0.01018 0.00426 -0.0403 0.1541 0.9987
6.000 1.0089 0.01060 0.00459 -0.0410 0.1346 0.9999
6.250 1.0289 0.01102 0.00491 -0.0400 0.1166 1.0000
6.500 1.0484 0.01142 0.00523 -0.0388 0.1020 1.0000
6.750 1.0683 0.01178 0.00553 -0.0377 0.0910 1.0000
7.000 1.0887 0.01212 0.00583 -0.0366 0.0824 1.0000
7.250 1.1090 0.01248 0.00615 -0.0357 0.0749 1.0000
7.500 1.1298 0.01280 0.00646 -0.0348 0.0688 1.0000
7.750 1.1501 0.01318 0.00681 -0.0338 0.0614 1.0000
8.000 1.1697 0.01364 0.00720 -0.0328 0.0522 1.0000
8.250 1.1867 0.01431 0.00776 -0.0315 0.0355 1.0000
8.500 1.2000 0.01529 0.00861 -0.0297 0.0155 1.0000
8.750 1.2197 0.01577 0.00911 -0.0288 0.0135 1.0000
9.000 1.2398 0.01622 0.00959 -0.0281 0.0124 1.0000
9.250 1.2597 0.01666 0.01006 -0.0273 0.0117 1.0000
9.500 1.2787 0.01716 0.01059 -0.0265 0.0109 1.0000
9.750 1.2963 0.01773 0.01119 -0.0255 0.0102 1.0000
10.000 1.3120 0.01831 0.01182 -0.0241 0.0096 1.0000
10.250 1.3274 0.01884 0.01238 -0.0228 0.0092 1.0000
10.500 1.3420 0.01944 0.01303 -0.0214 0.0089 1.0000
10.750 1.3559 0.02013 0.01376 -0.0201 0.0085 1.0000
11.000 1.3692 0.02090 0.01457 -0.0189 0.0082 1.0000
11.250 1.3817 0.02177 0.01550 -0.0178 0.0079 1.0000
11.500 1.3929 0.02280 0.01657 -0.0168 0.0075 1.0000
11.750 1.4022 0.02404 0.01788 -0.0157 0.0072 1.0000
12.000 1.4138 0.02515 0.01905 -0.0151 0.0071 1.0000
12.250 1.4246 0.02640 0.02036 -0.0145 0.0069 1.0000
12.500 1.4346 0.02778 0.02180 -0.0141 0.0068 1.0000
12.750 1.4437 0.02927 0.02337 -0.0137 0.0066 1.0000
13.000 1.4520 0.03089 0.02506 -0.0134 0.0064 1.0000
13.250 1.4594 0.03263 0.02686 -0.0132 0.0062 1.0000
13.500 1.4656 0.03452 0.02882 -0.0130 0.0060 1.0000
13.750 1.4705 0.03659 0.03096 -0.0129 0.0059 1.0000
14.000 1.4738 0.03884 0.03328 -0.0128 0.0057 1.0000
14.250 1.4752 0.04136 0.03588 -0.0129 0.0056 1.0000
14.500 1.4747 0.04414 0.03873 -0.0130 0.0055 1.0000
14.750 1.4716 0.04726 0.04195 -0.0132 0.0054 1.0000
15.000 1.4660 0.05081 0.04560 -0.0136 0.0053 1.0000
15.250 1.4625 0.05423 0.04912 -0.0142 0.0052 1.0000
15.500 1.4587 0.05781 0.05280 -0.0150 0.0052 1.0000
15.750 1.4537 0.06166 0.05675 -0.0159 0.0051 1.0000
16.000 1.4469 0.06587 0.06107 -0.0170 0.0051 1.0000
16.250 1.4390 0.07030 0.06560 -0.0183 0.0051 1.0000
16.500 1.4298 0.07506 0.07047 -0.0197 0.0050 1.0000
16.750 1.4192 0.08010 0.07561 -0.0213 0.0050 1.0000
17.000 1.4070 0.08545 0.08108 -0.0231 0.0049 1.0000
17.250 1.3944 0.09097 0.08671 -0.0250 0.0049 1.0000
17.500 1.3809 0.09674 0.09259 -0.0270 0.0049 1.0000
17.750 1.3663 0.10268 0.09864 -0.0292 0.0048 1.0000
18.000 1.3519 0.10869 0.10476 -0.0314 0.0048 1.0000
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