WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX L V-152 AIRFOIL (fxlv152-il) Reynolds number: 100,000 Max Cl/Cd: 42.63 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxlv152-il-100000.txt Download as CSV file: xf-fxlv152-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX L V-152 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.750 -0.9849 0.09139 0.08606 -0.0114 1.0005 0.0443
-14.500 -1.0087 0.08463 0.07910 -0.0148 1.0005 0.0441
-14.250 -1.0325 0.07832 0.07255 -0.0176 1.0005 0.0441
-14.000 -1.0552 0.07254 0.06648 -0.0197 1.0005 0.0441
-13.750 -1.0776 0.06716 0.06077 -0.0211 1.0005 0.0443
-13.500 -1.0663 0.06495 0.05866 -0.0209 1.0005 0.0461
-13.250 -1.0773 0.06100 0.05447 -0.0214 1.0005 0.0472
-13.000 -1.0943 0.05671 0.04980 -0.0216 1.0005 0.0483
-12.750 -1.0937 0.05408 0.04709 -0.0213 1.0005 0.0507
-12.500 -1.1003 0.05118 0.04392 -0.0206 1.0005 0.0532
-12.250 -1.0965 0.04903 0.04173 -0.0199 1.0005 0.0566
-12.000 -1.1060 0.04630 0.03854 -0.0180 1.0005 0.0594
-11.750 -1.0919 0.04464 0.03695 -0.0174 1.0005 0.0637
-11.500 -1.0846 0.04283 0.03499 -0.0163 1.0005 0.0678
-11.250 -1.0766 0.04091 0.03273 -0.0151 1.0005 0.0718
-11.000 -1.0542 0.03914 0.03103 -0.0150 1.0005 0.0754
-10.750 -1.0400 0.03740 0.02904 -0.0141 1.0005 0.0797
-10.500 -1.0199 0.03607 0.02776 -0.0138 1.0005 0.0844
-10.250 -0.9987 0.03445 0.02608 -0.0135 1.0005 0.0889
-10.000 -0.9791 0.03305 0.02455 -0.0129 1.0005 0.0944
-9.750 -0.9585 0.03174 0.02334 -0.0126 1.0005 0.1011
-9.500 -0.9393 0.03045 0.02208 -0.0121 1.0005 0.1092
-9.250 -0.9203 0.02917 0.02084 -0.0115 1.0005 0.1189
-9.000 -0.9012 0.02792 0.01963 -0.0110 1.0005 0.1303
-8.750 -0.8816 0.02663 0.01841 -0.0105 1.0005 0.1432
-8.500 -0.8621 0.02531 0.01720 -0.0099 1.0005 0.1579
-8.250 -0.8436 0.02402 0.01603 -0.0093 1.0005 0.1757
-8.000 -0.8258 0.02276 0.01499 -0.0087 1.0005 0.1962
-7.750 -0.8091 0.02150 0.01399 -0.0081 1.0005 0.2232
-7.500 -0.7948 0.02025 0.01311 -0.0073 1.0005 0.2583
-7.250 -0.7876 0.01922 0.01242 -0.0055 1.0005 0.3031
-7.000 -0.7939 0.01860 0.01214 -0.0015 1.0005 0.3423
-6.750 -0.7587 0.01817 0.01221 -0.0039 0.9869 0.4334
-6.500 -0.7141 0.01880 0.01293 -0.0068 0.9761 0.4919
-6.250 -0.6700 0.01980 0.01383 -0.0092 0.9656 0.5269
-6.000 -0.6254 0.02071 0.01461 -0.0115 0.9556 0.5516
-5.750 -0.5868 0.02151 0.01531 -0.0125 0.9437 0.5688
-5.500 -0.5500 0.02235 0.01604 -0.0130 0.9330 0.5842
-5.250 -0.5177 0.02308 0.01667 -0.0127 0.9225 0.5994
-5.000 -0.4914 0.02354 0.01700 -0.0121 0.9116 0.6148
-4.750 -0.4584 0.02456 0.01799 -0.0108 0.9039 0.6231
-4.500 -0.4344 0.02466 0.01799 -0.0102 0.8945 0.6359
-4.250 -0.4057 0.02519 0.01845 -0.0092 0.8873 0.6450
-4.000 -0.3811 0.02537 0.01855 -0.0083 0.8793 0.6559
-3.750 -0.3583 0.02539 0.01845 -0.0075 0.8714 0.6689
-3.500 -0.3302 0.02593 0.01896 -0.0059 0.8652 0.6756
-3.250 -0.3089 0.02575 0.01869 -0.0056 0.8574 0.6885
-3.000 -0.2804 0.02621 0.01913 -0.0041 0.8520 0.6944
-2.750 -0.2595 0.02584 0.01863 -0.0043 0.8455 0.7054
-2.500 -0.2334 0.02588 0.01866 -0.0036 0.8387 0.7103
-2.250 -0.2087 0.02579 0.01851 -0.0030 0.8329 0.7165
-2.000 -0.1874 0.02536 0.01799 -0.0036 0.8265 0.7253
-1.750 -0.1612 0.02543 0.01805 -0.0031 0.8205 0.7299
-1.500 -0.1372 0.02532 0.01788 -0.0027 0.8152 0.7370
-1.250 -0.1147 0.02512 0.01764 -0.0028 0.8089 0.7447
-1.000 -0.0897 0.02529 0.01783 -0.0021 0.8025 0.7509
-0.750 -0.0675 0.02516 0.01764 -0.0018 0.7974 0.7613
-0.500 -0.0422 0.02539 0.01790 -0.0008 0.7927 0.7673
-0.250 -0.0197 0.02544 0.01797 -0.0011 0.7859 0.7750
0.000 0.0043 0.02528 0.01778 -0.0011 0.7802 0.7806
0.250 0.0297 0.02529 0.01779 -0.0004 0.7757 0.7850
0.500 0.0517 0.02544 0.01798 -0.0008 0.7673 0.7916
0.750 0.0760 0.02520 0.01769 -0.0001 0.7604 0.7980
1.000 0.0985 0.02529 0.01783 0.0006 0.7509 0.8027
1.250 0.1231 0.02521 0.01776 0.0011 0.7438 0.8083
1.500 0.1484 0.02515 0.01767 0.0011 0.7390 0.8148
1.750 0.1693 0.02556 0.01820 0.0011 0.7303 0.8200
2.000 0.1944 0.02557 0.01825 0.0017 0.7246 0.8263
2.250 0.2180 0.02573 0.01843 0.0015 0.7177 0.8331
2.500 0.2404 0.02595 0.01875 0.0020 0.7092 0.8382
2.750 0.2671 0.02583 0.01865 0.0028 0.7042 0.8445
3.000 0.2871 0.02625 0.01918 0.0027 0.6937 0.8519
3.250 0.3141 0.02594 0.01891 0.0041 0.6868 0.8576
3.500 0.3358 0.02605 0.01910 0.0047 0.6749 0.8648
3.750 0.3650 0.02539 0.01847 0.0061 0.6675 0.8708
4.000 0.3866 0.02552 0.01872 0.0069 0.6545 0.8779
4.250 0.4158 0.02491 0.01813 0.0081 0.6482 0.8861
4.500 0.4386 0.02494 0.01831 0.0089 0.6343 0.8939
4.750 0.4648 0.02447 0.01791 0.0100 0.6236 0.9035
5.000 0.4963 0.02372 0.01723 0.0108 0.6123 0.9110
5.250 0.5224 0.02324 0.01686 0.0116 0.5978 0.9215
5.500 0.5574 0.02236 0.01607 0.0117 0.5835 0.9304
5.750 0.5950 0.02130 0.01502 0.0116 0.5704 0.9407
6.000 0.6354 0.02048 0.01429 0.0103 0.5524 0.9510
6.250 0.6764 0.01983 0.01388 0.0080 0.5249 0.9622
6.500 0.7191 0.01882 0.01294 0.0060 0.4899 0.9736
6.750 0.7637 0.01824 0.01227 0.0030 0.4287 0.9838
7.000 0.8006 0.01878 0.01225 0.0003 0.3346 0.9984
7.250 0.7960 0.01946 0.01262 0.0040 0.2948 0.9995
7.500 0.7984 0.02035 0.01322 0.0066 0.2559 0.9995
7.750 0.8111 0.02156 0.01406 0.0077 0.2223 0.9995
8.000 0.8272 0.02278 0.01505 0.0084 0.1956 0.9995
8.250 0.8440 0.02400 0.01606 0.0091 0.1753 0.9995
8.500 0.8616 0.02532 0.01717 0.0099 0.1581 0.9995
8.750 0.8806 0.02664 0.01835 0.0105 0.1436 0.9995
9.000 0.8999 0.02791 0.01953 0.0111 0.1309 0.9995
9.250 0.9188 0.02913 0.02072 0.0117 0.1196 0.9995
9.500 0.9368 0.03035 0.02194 0.0124 0.1098 0.9995
9.750 0.9546 0.03162 0.02324 0.0131 0.1014 0.9995
10.000 0.9736 0.03297 0.02461 0.0137 0.0945 0.9995
10.250 0.9964 0.03438 0.02588 0.0139 0.0893 0.9995
10.500 1.0143 0.03591 0.02764 0.0147 0.0846 0.9995
10.750 1.0335 0.03741 0.02914 0.0151 0.0802 0.9995
11.000 1.0496 0.03889 0.03074 0.0159 0.0759 0.9995
11.250 1.0665 0.04087 0.03286 0.0165 0.0725 0.9995
11.500 1.0816 0.04255 0.03462 0.0172 0.0686 0.9995
11.750 1.0839 0.04446 0.03679 0.0189 0.0648 0.9995
12.000 1.0960 0.04613 0.03844 0.0197 0.0607 0.9995
12.250 1.0904 0.04857 0.04123 0.0214 0.0577 0.9995
12.500 1.0925 0.05080 0.04356 0.0222 0.0545 0.9995
12.750 1.0884 0.05338 0.04635 0.0230 0.0517 0.9995
13.000 1.0861 0.05616 0.04925 0.0235 0.0495 0.9995
13.250 1.0696 0.06022 0.05368 0.0235 0.0483 0.9995
13.500 1.0681 0.06310 0.05665 0.0235 0.0465 0.9995
13.750 1.0667 0.06635 0.05997 0.0234 0.0453 0.9995
14.000 1.0442 0.07159 0.06553 0.0222 0.0451 0.9995
14.250 1.0210 0.07725 0.07147 0.0203 0.0450 0.9995
14.500 0.9967 0.08341 0.07787 0.0177 0.0451 0.9995
14.750 0.9722 0.09005 0.08471 0.0146 0.0453 0.9995
15.000 0.9479 0.09718 0.09201 0.0108 0.0455 0.9995
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