NACA CYH (nacacyh-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA CYH (nacacyh-il) Reynolds number: 500,000 Max Cl/Cd: 86.96 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-nacacyh-il-500000-n5.txt Download as CSV file: xf-nacacyh-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -0.9907 0.04498 0.04197 -0.0615 1.0000 0.0174
-14.250 -1.0095 0.04039 0.03715 -0.0627 1.0000 0.0175
-14.000 -1.0112 0.03829 0.03495 -0.0615 1.0000 0.0176
-13.750 -1.0057 0.03697 0.03355 -0.0599 1.0000 0.0178
-13.500 -0.9933 0.03611 0.03263 -0.0585 1.0000 0.0181
-13.250 -0.9777 0.03538 0.03187 -0.0574 1.0000 0.0183
-13.000 -0.9617 0.03462 0.03105 -0.0563 1.0000 0.0186
-12.750 -0.9468 0.03363 0.02997 -0.0552 1.0000 0.0190
-12.500 -0.9330 0.03239 0.02859 -0.0540 1.0000 0.0194
-12.250 -0.9200 0.03091 0.02694 -0.0527 1.0000 0.0199
-12.000 -0.9070 0.02931 0.02513 -0.0513 1.0000 0.0204
-11.750 -0.8924 0.02784 0.02342 -0.0498 1.0000 0.0210
-11.500 -0.8754 0.02669 0.02206 -0.0485 1.0000 0.0214
-11.250 -0.8566 0.02583 0.02102 -0.0472 1.0000 0.0217
-11.000 -0.8417 0.02437 0.01945 -0.0456 1.0000 0.0222
-10.750 -0.8154 0.02356 0.01858 -0.0458 0.9918 0.0226
-10.500 -0.7854 0.02292 0.01787 -0.0466 0.9787 0.0231
-10.250 -0.7555 0.02228 0.01714 -0.0473 0.9631 0.0236
-10.000 -0.7277 0.02155 0.01628 -0.0475 0.9444 0.0242
-9.750 -0.7039 0.02078 0.01535 -0.0467 0.9202 0.0247
-9.500 -0.6818 0.02013 0.01451 -0.0455 0.8941 0.0252
-9.250 -0.6596 0.01954 0.01372 -0.0443 0.8695 0.0258
-9.000 -0.6367 0.01896 0.01293 -0.0432 0.8488 0.0262
-8.750 -0.6130 0.01836 0.01215 -0.0423 0.8315 0.0266
-8.500 -0.5886 0.01785 0.01146 -0.0415 0.8170 0.0268
-8.250 -0.5640 0.01729 0.01075 -0.0407 0.8043 0.0272
-8.000 -0.5406 0.01628 0.00960 -0.0399 0.7934 0.0278
-7.750 -0.5157 0.01567 0.00889 -0.0393 0.7838 0.0283
-7.500 -0.4902 0.01516 0.00830 -0.0387 0.7747 0.0287
-7.250 -0.4644 0.01471 0.00776 -0.0382 0.7667 0.0291
-7.000 -0.4384 0.01428 0.00725 -0.0377 0.7590 0.0295
-6.750 -0.4122 0.01388 0.00678 -0.0372 0.7523 0.0300
-6.500 -0.3858 0.01352 0.00635 -0.0368 0.7452 0.0305
-6.250 -0.3593 0.01320 0.00596 -0.0363 0.7390 0.0312
-6.000 -0.3325 0.01286 0.00556 -0.0360 0.7330 0.0317
-5.750 -0.3058 0.01255 0.00518 -0.0355 0.7260 0.0321
-5.500 -0.2790 0.01226 0.00483 -0.0352 0.7187 0.0326
-5.250 -0.2521 0.01199 0.00449 -0.0348 0.7111 0.0330
-5.000 -0.2250 0.01176 0.00420 -0.0345 0.7042 0.0333
-4.750 -0.1979 0.01150 0.00390 -0.0342 0.6968 0.0338
-4.500 -0.1711 0.01122 0.00356 -0.0338 0.6901 0.0347
-4.250 -0.1437 0.01098 0.00330 -0.0336 0.6833 0.0357
-4.000 -0.1164 0.01081 0.00308 -0.0333 0.6760 0.0368
-3.750 -0.0888 0.01063 0.00288 -0.0331 0.6681 0.0383
-3.500 -0.0613 0.01050 0.00270 -0.0329 0.6599 0.0401
-3.250 -0.0336 0.01034 0.00253 -0.0327 0.6517 0.0426
-3.000 -0.0061 0.01019 0.00238 -0.0325 0.6444 0.0481
-2.750 0.0213 0.00999 0.00226 -0.0323 0.6371 0.0650
-2.500 0.0488 0.00985 0.00215 -0.0322 0.6293 0.0826
-2.250 0.0764 0.00971 0.00205 -0.0320 0.6213 0.0991
-2.000 0.1036 0.00955 0.00196 -0.0319 0.6134 0.1263
-1.750 0.1306 0.00933 0.00189 -0.0317 0.6053 0.1700
-1.500 0.1574 0.00915 0.00183 -0.0316 0.5970 0.2195
-1.250 0.1844 0.00896 0.00180 -0.0314 0.5875 0.2693
-1.000 0.2109 0.00876 0.00176 -0.0312 0.5776 0.3289
-0.750 0.2364 0.00849 0.00172 -0.0309 0.5666 0.4136
-0.500 0.2609 0.00811 0.00169 -0.0304 0.5556 0.5263
-0.250 0.2737 0.00710 0.00179 -0.0268 0.5463 0.8578
0.000 0.3006 0.00715 0.00191 -0.0262 0.5348 0.9122
0.250 0.3315 0.00727 0.00201 -0.0265 0.5221 0.9355
0.500 0.3634 0.00741 0.00209 -0.0272 0.5086 0.9509
0.750 0.3963 0.00759 0.00219 -0.0282 0.4930 0.9632
1.000 0.4280 0.00776 0.00227 -0.0290 0.4755 0.9712
1.250 0.4634 0.00794 0.00235 -0.0307 0.4567 0.9751
1.500 0.4992 0.00812 0.00244 -0.0325 0.4371 0.9785
1.750 0.5314 0.00831 0.00253 -0.0336 0.4175 0.9828
2.000 0.5668 0.00851 0.00264 -0.0355 0.3985 0.9855
2.750 0.6657 0.00913 0.00300 -0.0397 0.3512 0.9929
3.000 0.6960 0.00934 0.00313 -0.0405 0.3373 0.9944
3.250 0.7273 0.00951 0.00326 -0.0416 0.3266 0.9957
3.500 0.7580 0.00971 0.00340 -0.0426 0.3177 0.9972
3.750 0.7887 0.00987 0.00354 -0.0435 0.3078 0.9986
4.000 0.8191 0.01005 0.00370 -0.0445 0.2999 0.9999
4.250 0.8433 0.01019 0.00384 -0.0440 0.2939 1.0000
4.500 0.8662 0.01037 0.00401 -0.0433 0.2877 1.0000
4.750 0.8894 0.01051 0.00417 -0.0427 0.2812 1.0000
5.000 0.9121 0.01070 0.00434 -0.0419 0.2737 1.0000
5.250 0.9350 0.01087 0.00452 -0.0412 0.2674 1.0000
5.500 0.9576 0.01105 0.00470 -0.0405 0.2595 1.0000
5.750 0.9800 0.01127 0.00491 -0.0398 0.2483 1.0000
6.000 1.0012 0.01157 0.00513 -0.0389 0.2297 1.0000
6.250 1.0209 0.01200 0.00542 -0.0378 0.2008 1.0000
6.500 1.0392 0.01254 0.00580 -0.0365 0.1726 1.0000
6.750 1.0577 0.01306 0.00622 -0.0353 0.1522 1.0000
7.000 1.0766 0.01355 0.00663 -0.0341 0.1348 1.0000
7.250 1.0954 0.01407 0.00707 -0.0330 0.1185 1.0000
7.500 1.1145 0.01457 0.00751 -0.0319 0.1052 1.0000
7.750 1.1341 0.01505 0.00796 -0.0310 0.0951 1.0000
8.000 1.1532 0.01558 0.00844 -0.0300 0.0849 1.0000
8.250 1.1721 0.01612 0.00895 -0.0290 0.0766 1.0000
8.500 1.1920 0.01658 0.00941 -0.0282 0.0698 1.0000
8.750 1.2106 0.01712 0.00995 -0.0273 0.0626 1.0000
9.000 1.2279 0.01775 0.01053 -0.0262 0.0529 1.0000
9.250 1.2397 0.01871 0.01136 -0.0244 0.0327 1.0000
9.500 1.2442 0.01999 0.01253 -0.0216 0.0177 1.0000
9.750 1.2557 0.02077 0.01336 -0.0198 0.0156 1.0000
10.000 1.2676 0.02159 0.01424 -0.0182 0.0144 1.0000
10.250 1.2785 0.02254 0.01526 -0.0167 0.0135 1.0000
10.500 1.2886 0.02362 0.01641 -0.0153 0.0127 1.0000
10.750 1.3006 0.02462 0.01749 -0.0144 0.0123 1.0000
11.000 1.3115 0.02577 0.01872 -0.0135 0.0118 1.0000
11.250 1.3214 0.02705 0.02009 -0.0127 0.0113 1.0000
11.500 1.3302 0.02850 0.02163 -0.0120 0.0109 1.0000
11.750 1.3375 0.03015 0.02337 -0.0115 0.0104 1.0000
12.000 1.3426 0.03207 0.02537 -0.0110 0.0101 1.0000
12.250 1.3445 0.03438 0.02777 -0.0105 0.0097 1.0000
12.500 1.3496 0.03643 0.02992 -0.0103 0.0095 1.0000
12.750 1.3537 0.03863 0.03222 -0.0102 0.0093 1.0000
13.000 1.3561 0.04105 0.03474 -0.0102 0.0091 1.0000
13.250 1.3572 0.04368 0.03747 -0.0103 0.0089 1.0000
13.500 1.3567 0.04654 0.04044 -0.0105 0.0087 1.0000
13.750 1.3546 0.04967 0.04368 -0.0109 0.0086 1.0000
14.000 1.3512 0.05305 0.04717 -0.0114 0.0084 1.0000
14.250 1.3468 0.05667 0.05089 -0.0121 0.0083 1.0000
14.500 1.3414 0.06056 0.05490 -0.0130 0.0082 1.0000
14.750 1.3351 0.06472 0.05917 -0.0141 0.0081 1.0000
15.000 1.3277 0.06915 0.06371 -0.0153 0.0080 1.0000
15.250 1.3192 0.07385 0.06852 -0.0168 0.0079 1.0000
15.500 1.3100 0.07880 0.07358 -0.0184 0.0078 1.0000
15.750 1.2998 0.08393 0.07882 -0.0201 0.0077 1.0000
16.000 1.2888 0.08931 0.08431 -0.0219 0.0076 1.0000
16.250 1.2775 0.09479 0.08990 -0.0239 0.0076 1.0000
16.500 1.2659 0.10038 0.09559 -0.0259 0.0075 1.0000
16.750 1.2539 0.10610 0.10141 -0.0281 0.0074 1.0000
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