S1012 (s1012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1012 (s1012-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.3 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1012-il-1000000-n5.txt Download as CSV file: xf-s1012-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1012
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
------ -------- --------- --------- -------- -------- --------
-19.500 -1.1248 0.11570 0.11290 -0.0109 1.0000 0.0101
-19.250 -1.2051 0.09626 0.09320 -0.0224 1.0000 0.0099
-19.000 -1.2727 0.07950 0.07615 -0.0325 1.0000 0.0098
-18.750 -1.3142 0.06812 0.06455 -0.0394 1.0000 0.0097
-18.500 -1.3339 0.06118 0.05744 -0.0434 1.0000 0.0097
-18.250 -1.3506 0.05528 0.05138 -0.0464 1.0000 0.0097
-18.000 -1.3595 0.05096 0.04694 -0.0481 1.0000 0.0098
-17.750 -1.3680 0.04704 0.04288 -0.0493 1.0000 0.0099
-17.500 -1.3719 0.04395 0.03969 -0.0497 1.0000 0.0099
-17.250 -1.3783 0.04087 0.03649 -0.0497 1.0000 0.0102
-17.000 -1.3807 0.03835 0.03388 -0.0493 1.0000 0.0103
-16.750 -1.3817 0.03611 0.03155 -0.0486 1.0000 0.0105
-16.500 -1.3797 0.03422 0.02957 -0.0478 1.0000 0.0106
-16.250 -1.3762 0.03252 0.02780 -0.0468 1.0000 0.0109
-16.000 -1.3713 0.03100 0.02620 -0.0457 1.0000 0.0111
-15.750 -1.3651 0.02962 0.02474 -0.0445 1.0000 0.0113
-15.500 -1.3572 0.02840 0.02346 -0.0432 1.0000 0.0116
-15.250 -1.3488 0.02724 0.02224 -0.0419 1.0000 0.0119
-15.000 -1.3391 0.02620 0.02112 -0.0406 1.0000 0.0122
-14.750 -1.3285 0.02524 0.02009 -0.0393 1.0000 0.0124
-14.500 -1.3171 0.02435 0.01913 -0.0379 1.0000 0.0126
-14.250 -1.3058 0.02347 0.01819 -0.0365 1.0000 0.0127
-14.000 -1.2951 0.02255 0.01721 -0.0349 1.0000 0.0132
-13.750 -1.2830 0.02172 0.01634 -0.0334 1.0000 0.0136
-13.500 -1.2696 0.02099 0.01557 -0.0319 1.0000 0.0140
-13.000 -1.2240 0.01962 0.01407 -0.0325 0.9444 0.0152
-12.750 -1.2091 0.01915 0.01345 -0.0308 0.9137 0.0156
-12.500 -1.1953 0.01869 0.01288 -0.0289 0.8981 0.0159
-12.250 -1.1814 0.01814 0.01226 -0.0270 0.8876 0.0166
-12.000 -1.1666 0.01766 0.01170 -0.0252 0.8793 0.0173
-11.750 -1.1506 0.01719 0.01119 -0.0235 0.8726 0.0181
-11.500 -1.1342 0.01678 0.01071 -0.0218 0.8663 0.0188
-11.250 -1.1169 0.01641 0.01028 -0.0202 0.8614 0.0195
-11.000 -1.0994 0.01600 0.00983 -0.0186 0.8568 0.0204
-10.750 -1.0802 0.01559 0.00939 -0.0174 0.8528 0.0215
-10.500 -1.0597 0.01523 0.00899 -0.0163 0.8494 0.0227
-10.250 -1.0382 0.01489 0.00860 -0.0154 0.8466 0.0237
-10.000 -1.0167 0.01451 0.00821 -0.0146 0.8438 0.0252
-9.750 -0.9947 0.01415 0.00784 -0.0137 0.8411 0.0269
-9.500 -0.9721 0.01384 0.00750 -0.0130 0.8385 0.0285
-9.250 -0.9491 0.01354 0.00716 -0.0123 0.8361 0.0299
-9.000 -0.9263 0.01321 0.00683 -0.0116 0.8339 0.0320
-8.750 -0.9028 0.01293 0.00653 -0.0110 0.8319 0.0339
-8.500 -0.8785 0.01267 0.00624 -0.0105 0.8302 0.0354
-8.250 -0.8546 0.01236 0.00594 -0.0100 0.8283 0.0381
-8.000 -0.8303 0.01209 0.00567 -0.0095 0.8262 0.0406
-7.750 -0.8054 0.01186 0.00542 -0.0090 0.8243 0.0425
-7.500 -0.7807 0.01161 0.00516 -0.0086 0.8224 0.0451
-7.250 -0.7559 0.01136 0.00492 -0.0082 0.8208 0.0480
-7.000 -0.7306 0.01115 0.00470 -0.0078 0.8193 0.0507
-6.750 -0.7054 0.01092 0.00447 -0.0074 0.8178 0.0544
-6.500 -0.6801 0.01070 0.00426 -0.0070 0.8163 0.0585
-6.250 -0.6539 0.01052 0.00407 -0.0068 0.8151 0.0614
-6.000 -0.6283 0.01028 0.00387 -0.0065 0.8139 0.0663
-5.750 -0.6021 0.01009 0.00370 -0.0063 0.8126 0.0704
-5.500 -0.5759 0.00990 0.00352 -0.0060 0.8112 0.0754
-5.250 -0.5497 0.00971 0.00336 -0.0058 0.8098 0.0808
-5.000 -0.5230 0.00955 0.00321 -0.0056 0.8083 0.0856
-4.750 -0.4968 0.00935 0.00305 -0.0054 0.8069 0.0932
-4.500 -0.4700 0.00920 0.00291 -0.0052 0.8056 0.0991
-4.250 -0.4436 0.00902 0.00277 -0.0050 0.8044 0.1081
-4.000 -0.4168 0.00886 0.00264 -0.0049 0.8032 0.1167
-3.750 -0.3899 0.00872 0.00253 -0.0047 0.8021 0.1252
-3.500 -0.3632 0.00856 0.00242 -0.0046 0.8008 0.1369
-3.250 -0.3363 0.00839 0.00231 -0.0045 0.7996 0.1507
-3.000 -0.3093 0.00822 0.00221 -0.0044 0.7984 0.1650
-2.750 -0.2824 0.00804 0.00211 -0.0042 0.7972 0.1840
-2.500 -0.2556 0.00785 0.00202 -0.0041 0.7959 0.2054
-2.250 -0.2290 0.00765 0.00193 -0.0039 0.7943 0.2316
-2.000 -0.2026 0.00741 0.00184 -0.0037 0.7926 0.2659
-1.750 -0.1764 0.00718 0.00174 -0.0035 0.7903 0.3018
-1.500 -0.1512 0.00690 0.00161 -0.0030 0.7840 0.3501
-1.250 -0.1264 0.00652 0.00144 -0.0025 0.7724 0.4100
-1.000 -0.1021 0.00612 0.00128 -0.0019 0.7604 0.4816
-0.750 -0.0780 0.00572 0.00113 -0.0012 0.7527 0.5580
-0.500 -0.0538 0.00531 0.00104 -0.0006 0.7451 0.6405
-0.250 -0.0282 0.00512 0.00106 -0.0001 0.7362 0.7047
0.000 0.0000 0.00510 0.00107 0.0000 0.7249 0.7246
0.250 0.0281 0.00512 0.00106 0.0001 0.7045 0.7364
0.500 0.0539 0.00530 0.00104 0.0006 0.6417 0.7451
0.750 0.0780 0.00572 0.00113 0.0012 0.5584 0.7528
1.000 0.1021 0.00612 0.00128 0.0019 0.4818 0.7605
1.250 0.1263 0.00653 0.00144 0.0025 0.4090 0.7724
1.500 0.1511 0.00690 0.00161 0.0031 0.3497 0.7840
1.750 0.1764 0.00718 0.00174 0.0035 0.3019 0.7903
2.000 0.2027 0.00741 0.00184 0.0037 0.2665 0.7926
2.250 0.2289 0.00765 0.00193 0.0040 0.2315 0.7943
2.500 0.2556 0.00785 0.00202 0.0041 0.2055 0.7959
2.750 0.2824 0.00804 0.00212 0.0042 0.1833 0.7972
3.000 0.3093 0.00822 0.00221 0.0044 0.1647 0.7984
3.250 0.3363 0.00839 0.00231 0.0045 0.1505 0.7996
3.500 0.3631 0.00856 0.00242 0.0046 0.1366 0.8008
3.750 0.3898 0.00872 0.00253 0.0047 0.1252 0.8021
4.000 0.4168 0.00886 0.00264 0.0049 0.1167 0.8032
4.250 0.4436 0.00902 0.00277 0.0050 0.1081 0.8044
4.500 0.4700 0.00920 0.00291 0.0052 0.0991 0.8056
4.750 0.4968 0.00935 0.00305 0.0054 0.0933 0.8069
5.000 0.5230 0.00955 0.00321 0.0056 0.0855 0.8083
5.250 0.5497 0.00971 0.00336 0.0058 0.0808 0.8098
5.500 0.5759 0.00990 0.00352 0.0060 0.0753 0.8112
5.750 0.6021 0.01009 0.00370 0.0063 0.0705 0.8126
6.000 0.6283 0.01028 0.00387 0.0065 0.0663 0.8139
6.250 0.6539 0.01052 0.00407 0.0068 0.0613 0.8151
6.500 0.6801 0.01070 0.00427 0.0070 0.0586 0.8163
6.750 0.7054 0.01092 0.00447 0.0074 0.0545 0.8177
7.000 0.7306 0.01115 0.00470 0.0078 0.0507 0.8193
7.250 0.7559 0.01136 0.00492 0.0082 0.0480 0.8208
7.500 0.7807 0.01161 0.00516 0.0086 0.0451 0.8224
7.750 0.8054 0.01186 0.00542 0.0090 0.0425 0.8242
8.000 0.8303 0.01209 0.00567 0.0095 0.0406 0.8262
8.250 0.8546 0.01237 0.00594 0.0100 0.0379 0.8283
8.500 0.8785 0.01267 0.00625 0.0105 0.0354 0.8302
8.750 0.9028 0.01293 0.00652 0.0110 0.0340 0.8319
9.000 0.9263 0.01321 0.00682 0.0116 0.0320 0.8339
9.250 0.9491 0.01354 0.00716 0.0123 0.0298 0.8361
9.500 0.9721 0.01384 0.00750 0.0130 0.0285 0.8385
9.750 0.9948 0.01415 0.00784 0.0137 0.0270 0.8411
10.000 1.0167 0.01451 0.00820 0.0146 0.0253 0.8438
10.250 1.0383 0.01489 0.00860 0.0154 0.0238 0.8466
10.500 1.0598 0.01522 0.00898 0.0163 0.0227 0.8494
10.750 1.0803 0.01559 0.00939 0.0174 0.0215 0.8528
11.000 1.0995 0.01600 0.00982 0.0186 0.0204 0.8568
11.250 1.1169 0.01641 0.01028 0.0202 0.0195 0.8614
11.500 1.1342 0.01678 0.01071 0.0218 0.0189 0.8663
11.750 1.1507 0.01719 0.01119 0.0235 0.0182 0.8725
12.000 1.1668 0.01764 0.01170 0.0251 0.0174 0.8792
12.250 1.1816 0.01814 0.01225 0.0270 0.0166 0.8876
12.500 1.1954 0.01869 0.01288 0.0289 0.0159 0.8981
12.750 1.2093 0.01915 0.01345 0.0308 0.0156 0.9138
13.000 1.2243 0.01962 0.01406 0.0325 0.0153 0.9449
13.500 1.2698 0.02100 0.01558 0.0319 0.0140 1.0000
13.750 1.2832 0.02172 0.01635 0.0334 0.0138 1.0000
14.000 1.2957 0.02252 0.01718 0.0348 0.0133 1.0000
14.250 1.3068 0.02342 0.01813 0.0364 0.0129 1.0000
14.500 1.3179 0.02431 0.01909 0.0378 0.0126 1.0000
14.750 1.3291 0.02522 0.02008 0.0392 0.0124 1.0000
15.000 1.3395 0.02620 0.02112 0.0406 0.0121 1.0000
15.250 1.3489 0.02726 0.02226 0.0419 0.0119 1.0000
15.500 1.3582 0.02835 0.02341 0.0431 0.0116 1.0000
15.750 1.3652 0.02963 0.02477 0.0444 0.0115 1.0000
16.000 1.3716 0.03101 0.02622 0.0456 0.0112 1.0000
16.250 1.3770 0.03250 0.02777 0.0467 0.0109 1.0000
16.500 1.3807 0.03418 0.02953 0.0477 0.0107 1.0000
16.750 1.3828 0.03606 0.03150 0.0485 0.0105 1.0000
17.000 1.3820 0.03829 0.03381 0.0492 0.0102 1.0000
17.250 1.3794 0.04081 0.03644 0.0496 0.0101 1.0000
17.500 1.3744 0.04376 0.03949 0.0496 0.0099 1.0000
17.750 1.3701 0.04686 0.04270 0.0492 0.0099 1.0000
18.000 1.3632 0.05057 0.04654 0.0482 0.0098 1.0000
18.250 1.3529 0.05506 0.05116 0.0464 0.0098 1.0000
18.500 1.3385 0.06059 0.05684 0.0436 0.0097 1.0000
18.750 1.3147 0.06819 0.06462 0.0392 0.0097 1.0000
19.000 1.2777 0.07874 0.07538 0.0328 0.0097 1.0000
19.250 1.2087 0.09577 0.09270 0.0225 0.0099 1.0000
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