LWK 80-100 (lwk80100-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: LWK 80-100 (lwk80100-il) Reynolds number: 1,000,000 Max Cl/Cd: 60.48 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-lwk80100-il-1000000.txt Download as CSV file: xf-lwk80100-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: LWK 80-100
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.9745 0.06924 0.06738 -0.0168 1.0000 0.0060
-13.500 -0.9899 0.06141 0.05942 -0.0230 1.0000 0.0060
-13.250 -1.0389 0.05044 0.04813 -0.0290 1.0000 0.0059
-13.000 -1.0376 0.04790 0.04551 -0.0298 1.0000 0.0059
-12.750 -1.0779 0.04075 0.03800 -0.0299 1.0000 0.0058
-12.500 -1.0628 0.04024 0.03747 -0.0297 1.0000 0.0062
-12.250 -1.0802 0.03634 0.03331 -0.0280 1.0000 0.0062
-12.000 -1.0849 0.03393 0.03070 -0.0260 1.0000 0.0063
-11.750 -1.0869 0.03184 0.02842 -0.0235 1.0000 0.0064
-11.500 -1.0820 0.03042 0.02686 -0.0212 1.0000 0.0065
-11.250 -1.0699 0.02940 0.02572 -0.0196 1.0000 0.0068
-11.000 -1.0600 0.02781 0.02396 -0.0178 1.0000 0.0069
-10.750 -1.0505 0.02596 0.02190 -0.0159 1.0000 0.0070
-10.500 -1.0284 0.02588 0.02176 -0.0153 1.0000 0.0072
-10.250 -1.0281 0.02222 0.01769 -0.0122 1.0000 0.0075
-10.000 -1.0126 0.02083 0.01614 -0.0107 1.0000 0.0075
-9.750 -0.9990 0.01911 0.01424 -0.0089 1.0000 0.0078
-9.500 -0.9807 0.01814 0.01316 -0.0077 1.0000 0.0081
-9.250 -0.9614 0.01729 0.01223 -0.0066 1.0000 0.0083
-9.000 -0.9406 0.01665 0.01154 -0.0057 1.0000 0.0088
-8.750 -0.9254 0.01608 0.01092 -0.0034 0.9943 0.0092
-8.500 -0.8885 0.01518 0.00992 -0.0061 0.9748 0.0097
-8.250 -0.8471 0.01452 0.00917 -0.0096 0.9644 0.0102
-8.000 -0.8036 0.01396 0.00853 -0.0136 0.9564 0.0107
-7.750 -0.7648 0.01254 0.00693 -0.0169 0.9441 0.0120
-7.500 -0.7268 0.01203 0.00635 -0.0196 0.9318 0.0131
-7.250 -0.6955 0.01161 0.00585 -0.0208 0.9192 0.0142
-7.000 -0.6676 0.01137 0.00554 -0.0210 0.9087 0.0156
-6.750 -0.6447 0.01083 0.00492 -0.0203 0.8991 0.0197
-6.500 -0.6200 0.01064 0.00469 -0.0198 0.8917 0.0216
-6.250 -0.5970 0.01026 0.00428 -0.0190 0.8853 0.0264
-6.000 -0.5726 0.01006 0.00406 -0.0185 0.8797 0.0297
-5.750 -0.5487 0.00979 0.00376 -0.0177 0.8742 0.0341
-5.500 -0.5244 0.00956 0.00351 -0.0172 0.8693 0.0394
-5.250 -0.5001 0.00935 0.00329 -0.0165 0.8647 0.0446
-5.000 -0.4758 0.00914 0.00309 -0.0159 0.8604 0.0529
-4.750 -0.4514 0.00891 0.00289 -0.0154 0.8564 0.0650
-4.500 -0.4273 0.00867 0.00270 -0.0147 0.8525 0.0791
-4.250 -0.4038 0.00839 0.00250 -0.0140 0.8484 0.1016
-4.000 -0.3802 0.00811 0.00232 -0.0132 0.8447 0.1316
-3.750 -0.3572 0.00779 0.00215 -0.0124 0.8412 0.1758
-3.500 -0.3367 0.00730 0.00195 -0.0112 0.8376 0.2485
-3.250 -0.3165 0.00681 0.00176 -0.0099 0.8338 0.3300
-3.000 -0.2979 0.00624 0.00156 -0.0082 0.8303 0.4350
-2.750 -0.2816 0.00561 0.00138 -0.0061 0.8267 0.5598
-2.500 -0.2617 0.00528 0.00132 -0.0044 0.8234 0.6407
-2.250 -0.2377 0.00516 0.00132 -0.0035 0.8201 0.6814
-2.000 -0.2118 0.00512 0.00130 -0.0031 0.8170 0.7007
-1.750 -0.1853 0.00512 0.00129 -0.0027 0.8142 0.7161
-1.500 -0.1587 0.00512 0.00130 -0.0024 0.8112 0.7294
-1.250 -0.1320 0.00512 0.00129 -0.0021 0.8078 0.7393
-1.000 -0.1052 0.00510 0.00130 -0.0018 0.8043 0.7477
-0.750 -0.0789 0.00512 0.00131 -0.0013 0.8003 0.7592
-0.500 -0.0525 0.00515 0.00132 -0.0009 0.7952 0.7679
-0.250 -0.0264 0.00512 0.00132 -0.0004 0.7887 0.7756
0.000 -0.0001 0.00516 0.00132 0.0000 0.7823 0.7829
0.250 0.0263 0.00512 0.00132 0.0005 0.7750 0.7889
0.500 0.0527 0.00515 0.00132 0.0009 0.7682 0.7949
0.750 0.0789 0.00512 0.00130 0.0014 0.7588 0.8000
1.000 0.1052 0.00510 0.00129 0.0018 0.7474 0.8043
1.250 0.1320 0.00512 0.00129 0.0021 0.7390 0.8078
1.500 0.1588 0.00512 0.00130 0.0024 0.7292 0.8112
1.750 0.1851 0.00512 0.00128 0.0028 0.7142 0.8142
2.000 0.2117 0.00513 0.00129 0.0031 0.6999 0.8171
2.250 0.2378 0.00516 0.00131 0.0035 0.6821 0.8201
2.500 0.2628 0.00524 0.00133 0.0042 0.6515 0.8234
2.750 0.2818 0.00561 0.00138 0.0061 0.5604 0.8267
3.000 0.2972 0.00629 0.00157 0.0084 0.4252 0.8303
3.250 0.3164 0.00682 0.00176 0.0099 0.3290 0.8338
3.500 0.3365 0.00732 0.00196 0.0112 0.2449 0.8375
3.750 0.3573 0.00779 0.00215 0.0125 0.1758 0.8412
4.000 0.3802 0.00811 0.00232 0.0132 0.1313 0.8447
4.250 0.4039 0.00839 0.00250 0.0140 0.1025 0.8484
4.500 0.4275 0.00866 0.00270 0.0147 0.0811 0.8525
4.750 0.4515 0.00890 0.00288 0.0154 0.0654 0.8564
5.000 0.4759 0.00912 0.00308 0.0159 0.0534 0.8604
5.250 0.5006 0.00931 0.00326 0.0165 0.0464 0.8647
5.500 0.5246 0.00955 0.00350 0.0172 0.0397 0.8694
5.750 0.5488 0.00979 0.00374 0.0177 0.0334 0.8742
6.000 0.5730 0.01002 0.00402 0.0184 0.0295 0.8796
6.250 0.5971 0.01025 0.00424 0.0190 0.0256 0.8853
6.500 0.6209 0.01056 0.00460 0.0197 0.0209 0.8915
7.000 0.6683 0.01130 0.00545 0.0209 0.0148 0.9085
7.250 0.6955 0.01161 0.00584 0.0208 0.0139 0.9192
7.500 0.7270 0.01202 0.00632 0.0196 0.0124 0.9319
7.750 0.7638 0.01283 0.00723 0.0170 0.0112 0.9449
8.000 0.8035 0.01405 0.00863 0.0136 0.0105 0.9566
8.250 0.8464 0.01474 0.00943 0.0097 0.0101 0.9647
8.500 0.8877 0.01542 0.01019 0.0062 0.0093 0.9754
8.750 0.9249 0.01626 0.01112 0.0035 0.0089 0.9953
9.000 0.9399 0.01676 0.01164 0.0058 0.0085 1.0000
9.250 0.9596 0.01756 0.01252 0.0069 0.0083 1.0000
9.500 0.9785 0.01847 0.01351 0.0081 0.0080 1.0000
9.750 0.9964 0.01954 0.01471 0.0094 0.0078 1.0000
10.000 1.0107 0.02114 0.01648 0.0110 0.0075 1.0000
10.250 1.0201 0.02354 0.01915 0.0132 0.0074 1.0000
10.500 1.0275 0.02606 0.02196 0.0155 0.0073 1.0000
10.750 1.0347 0.02830 0.02446 0.0176 0.0071 1.0000
11.000 1.0545 0.02857 0.02479 0.0184 0.0070 1.0000
11.250 1.0594 0.03077 0.02722 0.0206 0.0069 1.0000
11.500 1.0573 0.03303 0.02971 0.0237 0.0068 1.0000
11.750 1.0638 0.03421 0.03101 0.0256 0.0067 1.0000
12.000 1.0759 0.03486 0.03172 0.0267 0.0064 1.0000
12.250 1.0748 0.03692 0.03393 0.0283 0.0062 1.0000
12.500 1.0522 0.04144 0.03874 0.0299 0.0064 1.0000
12.750 1.0487 0.04413 0.04156 0.0302 0.0060 1.0000
13.000 1.0322 0.04868 0.04632 0.0295 0.0060 1.0000
13.250 1.0058 0.05532 0.05318 0.0268 0.0059 1.0000
13.750 0.9615 0.07279 0.07100 0.0138 0.0062 1.0000
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