CLARK YH AIRFOIL (clarkyh-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: CLARK YH AIRFOIL (clarkyh-il) Reynolds number: 500,000 Max Cl/Cd: 77.74 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-clarkyh-il-500000-n5.txt Download as CSV file: xf-clarkyh-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: CLARK YH AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-16.500 -0.9041 0.10131 0.09854 -0.0115 1.0000 0.0119
-16.250 -0.9764 0.08468 0.08180 -0.0221 1.0000 0.0115
-16.000 -1.1335 0.04830 0.04490 -0.0535 1.0000 0.0103
-15.750 -1.1616 0.04061 0.03691 -0.0593 1.0000 0.0103
-15.500 -1.1724 0.03717 0.03329 -0.0592 1.0000 0.0104
-15.250 -1.1769 0.03474 0.03070 -0.0576 1.0000 0.0105
-15.000 -1.1768 0.03282 0.02864 -0.0555 1.0000 0.0107
-14.750 -1.1721 0.03117 0.02684 -0.0534 1.0000 0.0110
-14.500 -1.1626 0.02965 0.02517 -0.0517 1.0000 0.0112
-14.250 -1.1505 0.02828 0.02366 -0.0502 1.0000 0.0116
-14.000 -1.1363 0.02704 0.02227 -0.0487 1.0000 0.0119
-13.750 -1.1214 0.02580 0.02091 -0.0472 1.0000 0.0122
-13.500 -1.1055 0.02461 0.01960 -0.0459 1.0000 0.0127
-13.250 -1.0876 0.02359 0.01848 -0.0446 1.0000 0.0132
-13.000 -1.0683 0.02268 0.01746 -0.0435 1.0000 0.0139
-12.750 -1.0482 0.02183 0.01650 -0.0423 1.0000 0.0145
-12.500 -1.0278 0.02098 0.01555 -0.0412 1.0000 0.0152
-12.000 -0.9778 0.01934 0.01375 -0.0407 0.9705 0.0171
-11.750 -0.9511 0.01867 0.01295 -0.0406 0.9543 0.0181
-11.500 -0.9273 0.01800 0.01220 -0.0399 0.9402 0.0195
-11.250 -0.9047 0.01746 0.01158 -0.0387 0.9276 0.0212
-11.000 -0.8818 0.01697 0.01099 -0.0376 0.9166 0.0229
-10.750 -0.8581 0.01657 0.01056 -0.0367 0.9079 0.0252
-10.500 -0.8341 0.01621 0.01011 -0.0357 0.8986 0.0274
-10.250 -0.8090 0.01598 0.00986 -0.0348 0.8896 0.0298
-10.000 -0.7837 0.01581 0.00960 -0.0340 0.8807 0.0323
-9.750 -0.7580 0.01556 0.00925 -0.0333 0.8731 0.0343
-9.500 -0.7324 0.01533 0.00898 -0.0326 0.8660 0.0360
-9.250 -0.7059 0.01518 0.00879 -0.0321 0.8599 0.0378
-9.000 -0.6794 0.01500 0.00853 -0.0315 0.8537 0.0396
-8.500 -0.6262 0.01468 0.00802 -0.0304 0.8401 0.0424
-8.250 -0.6009 0.01428 0.00755 -0.0297 0.8336 0.0436
-8.000 -0.5753 0.01390 0.00713 -0.0291 0.8274 0.0451
-7.750 -0.5491 0.01363 0.00681 -0.0286 0.8200 0.0465
-7.500 -0.5228 0.01338 0.00649 -0.0280 0.8129 0.0480
-7.250 -0.4962 0.01312 0.00617 -0.0275 0.8051 0.0494
-7.000 -0.4697 0.01289 0.00586 -0.0270 0.7983 0.0505
-6.750 -0.4427 0.01265 0.00556 -0.0266 0.7906 0.0513
-6.500 -0.4160 0.01245 0.00529 -0.0261 0.7825 0.0518
-6.250 -0.3902 0.01202 0.00481 -0.0256 0.7731 0.0531
-6.000 -0.3640 0.01170 0.00444 -0.0250 0.7634 0.0541
-5.750 -0.3374 0.01143 0.00412 -0.0246 0.7521 0.0551
-5.500 -0.3106 0.01119 0.00384 -0.0241 0.7392 0.0563
-5.250 -0.2838 0.01099 0.00357 -0.0237 0.7237 0.0573
-5.000 -0.2570 0.01083 0.00331 -0.0233 0.7050 0.0582
-4.750 -0.2303 0.01070 0.00308 -0.0228 0.6853 0.0590
-4.500 -0.2035 0.01061 0.00288 -0.0224 0.6658 0.0599
-4.250 -0.1767 0.01054 0.00269 -0.0220 0.6478 0.0608
-4.000 -0.1497 0.01047 0.00254 -0.0217 0.6326 0.0622
-3.750 -0.1228 0.01039 0.00240 -0.0213 0.6195 0.0650
-3.500 -0.0958 0.01030 0.00229 -0.0210 0.6076 0.0692
-3.250 -0.0690 0.01014 0.00221 -0.0208 0.5973 0.0909
-3.000 -0.0417 0.01007 0.00212 -0.0205 0.5876 0.1006
-2.750 -0.0142 0.01003 0.00204 -0.0203 0.5769 0.1079
-2.500 0.0130 0.00994 0.00194 -0.0201 0.5662 0.1158
-2.250 0.0400 0.00986 0.00186 -0.0199 0.5551 0.1268
-2.000 0.0664 0.00970 0.00187 -0.0196 0.5429 0.1777
-1.750 0.0941 0.00970 0.00184 -0.0195 0.5310 0.1892
-1.500 0.1215 0.00968 0.00183 -0.0194 0.5195 0.1987
-1.250 0.1491 0.00971 0.00180 -0.0193 0.5073 0.2039
-1.000 0.1766 0.00972 0.00179 -0.0192 0.4952 0.2082
-0.750 0.2039 0.00974 0.00178 -0.0190 0.4829 0.2132
-0.500 0.2311 0.00978 0.00178 -0.0189 0.4705 0.2188
-0.250 0.2584 0.00984 0.00180 -0.0188 0.4599 0.2233
0.000 0.2856 0.00985 0.00182 -0.0187 0.4508 0.2297
0.250 0.3128 0.00989 0.00185 -0.0186 0.4430 0.2375
0.500 0.3400 0.00989 0.00188 -0.0186 0.4359 0.2473
0.750 0.3670 0.00992 0.00193 -0.0185 0.4290 0.2588
1.000 0.3936 0.00986 0.00198 -0.0184 0.4220 0.2894
1.250 0.4102 0.00895 0.00199 -0.0166 0.4133 0.5942
1.500 0.4253 0.00817 0.00214 -0.0136 0.4057 0.8725
1.750 0.4680 0.00829 0.00234 -0.0168 0.3952 0.9195
2.000 0.5120 0.00843 0.00250 -0.0204 0.3854 0.9378
2.250 0.5488 0.00860 0.00264 -0.0225 0.3731 0.9500
2.750 0.6093 0.00930 0.00298 -0.0242 0.2851 0.9705
3.000 0.6395 0.00991 0.00332 -0.0252 0.2383 0.9778
3.250 0.6704 0.01022 0.00357 -0.0262 0.2262 0.9845
3.500 0.7080 0.01045 0.00379 -0.0287 0.2193 0.9885
3.750 0.7421 0.01070 0.00401 -0.0304 0.2134 0.9923
4.000 0.7752 0.01094 0.00424 -0.0320 0.2075 0.9948
4.250 0.8098 0.01111 0.00443 -0.0338 0.2039 0.9969
4.500 0.8450 0.01131 0.00465 -0.0359 0.2001 0.9992
4.750 0.8725 0.01157 0.00489 -0.0363 0.1943 1.0000
5.000 0.8958 0.01176 0.00509 -0.0357 0.1882 1.0000
5.250 0.9188 0.01197 0.00531 -0.0351 0.1820 1.0000
5.500 0.9412 0.01224 0.00556 -0.0344 0.1759 1.0000
5.750 0.9644 0.01242 0.00577 -0.0338 0.1701 1.0000
6.000 0.9865 0.01269 0.00601 -0.0331 0.1610 1.0000
6.250 1.0081 0.01300 0.00627 -0.0324 0.1449 1.0000
6.500 1.0227 0.01387 0.00681 -0.0307 0.0918 1.0000
6.750 1.0408 0.01442 0.00730 -0.0294 0.0793 1.0000
7.000 1.0592 0.01491 0.00778 -0.0282 0.0714 1.0000
7.250 1.0786 0.01531 0.00820 -0.0271 0.0641 1.0000
7.500 1.0952 0.01590 0.00873 -0.0257 0.0490 1.0000
7.750 1.1076 0.01675 0.00942 -0.0236 0.0306 1.0000
8.000 1.1234 0.01733 0.01000 -0.0220 0.0261 1.0000
8.250 1.1384 0.01793 0.01063 -0.0204 0.0230 1.0000
8.500 1.1541 0.01845 0.01119 -0.0188 0.0213 1.0000
8.750 1.1681 0.01905 0.01183 -0.0171 0.0197 1.0000
9.000 1.1798 0.01977 0.01258 -0.0150 0.0182 1.0000
9.250 1.1912 0.02033 0.01320 -0.0129 0.0174 1.0000
9.500 1.2018 0.02100 0.01393 -0.0108 0.0164 1.0000
9.750 1.2122 0.02179 0.01476 -0.0090 0.0156 1.0000
10.000 1.2216 0.02275 0.01577 -0.0074 0.0148 1.0000
10.250 1.2309 0.02381 0.01689 -0.0059 0.0142 1.0000
10.500 1.2416 0.02485 0.01801 -0.0048 0.0137 1.0000
10.750 1.2515 0.02601 0.01924 -0.0038 0.0132 1.0000
11.000 1.2608 0.02728 0.02057 -0.0029 0.0127 1.0000
11.250 1.2691 0.02868 0.02205 -0.0022 0.0122 1.0000
11.500 1.2753 0.03033 0.02375 -0.0014 0.0118 1.0000
11.750 1.2789 0.03229 0.02579 -0.0008 0.0114 1.0000
12.000 1.2855 0.03406 0.02766 -0.0004 0.0111 1.0000
12.250 1.2904 0.03607 0.02976 -0.0001 0.0108 1.0000
12.500 1.2942 0.03829 0.03207 -0.0001 0.0105 1.0000
12.750 1.2968 0.04070 0.03458 -0.0001 0.0103 1.0000
13.000 1.2986 0.04330 0.03727 -0.0004 0.0100 1.0000
13.250 1.2992 0.04608 0.04014 -0.0007 0.0098 1.0000
13.500 1.2985 0.04906 0.04322 -0.0011 0.0097 1.0000
13.750 1.2963 0.05227 0.04652 -0.0017 0.0095 1.0000
14.000 1.2927 0.05576 0.05010 -0.0024 0.0093 1.0000
14.250 1.2872 0.05960 0.05403 -0.0033 0.0092 1.0000
14.500 1.2797 0.06381 0.05834 -0.0043 0.0091 1.0000
14.750 1.2744 0.06782 0.06245 -0.0054 0.0089 1.0000
15.000 1.2694 0.07186 0.06660 -0.0066 0.0088 1.0000
15.250 1.2636 0.07609 0.07095 -0.0079 0.0087 1.0000
15.500 1.2572 0.08050 0.07546 -0.0093 0.0086 1.0000
15.750 1.2502 0.08503 0.08010 -0.0108 0.0085 1.0000
16.000 1.2427 0.08973 0.08490 -0.0124 0.0083 1.0000
16.250 1.2351 0.09453 0.08981 -0.0141 0.0082 1.0000
16.500 1.2270 0.09946 0.09485 -0.0158 0.0081 1.0000
16.750 1.2187 0.10450 0.09998 -0.0177 0.0080 1.0000
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