LOCKHEED L-188 TIP AIRFOIL (l188tip-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: LOCKHEED L-188 TIP AIRFOIL (l188tip-il) Reynolds number: 100,000 Max Cl/Cd: 53.19 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-l188tip-il-100000-n5.txt Download as CSV file: xf-l188tip-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: LOCKHEED L-188 TIP 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.000 -0.4530 0.09439 0.08913 -0.0490 1.0000 0.0373
-9.750 -0.4679 0.09039 0.08520 -0.0490 1.0000 0.0372
-9.500 -0.4868 0.08616 0.08105 -0.0490 1.0000 0.0371
-9.250 -0.5111 0.08148 0.07647 -0.0492 1.0000 0.0368
-9.000 -0.5572 0.07464 0.06971 -0.0507 1.0000 0.0356
-8.750 -0.6076 0.06363 0.05843 -0.0549 0.9960 0.0346
-8.500 -0.6032 0.05873 0.05330 -0.0581 0.9905 0.0352
-8.250 -0.5981 0.05308 0.04727 -0.0611 0.9851 0.0357
-8.000 -0.5917 0.04780 0.04153 -0.0625 0.9797 0.0361
-7.750 -0.5789 0.04324 0.03645 -0.0637 0.9748 0.0367
-7.500 -0.5589 0.03916 0.03177 -0.0651 0.9715 0.0377
-7.250 -0.5434 0.03587 0.02780 -0.0646 0.9662 0.0395
-7.000 -0.5194 0.03387 0.02550 -0.0652 0.9623 0.0411
-6.750 -0.4908 0.03232 0.02374 -0.0663 0.9594 0.0426
-6.500 -0.4603 0.03052 0.02162 -0.0676 0.9572 0.0443
-6.250 -0.4394 0.02908 0.01982 -0.0667 0.9518 0.0465
-6.000 -0.4118 0.02789 0.01848 -0.0672 0.9480 0.0490
-5.750 -0.3810 0.02691 0.01740 -0.0683 0.9451 0.0518
-5.500 -0.3478 0.02580 0.01605 -0.0695 0.9428 0.0551
-5.250 -0.3245 0.02500 0.01522 -0.0690 0.9378 0.0584
-5.000 -0.2974 0.02431 0.01448 -0.0692 0.9334 0.0623
-4.750 -0.2662 0.02352 0.01358 -0.0701 0.9302 0.0672
-4.500 -0.2330 0.02286 0.01295 -0.0715 0.9277 0.0734
-4.250 -0.2077 0.02229 0.01233 -0.0712 0.9230 0.0796
-4.000 -0.1824 0.02183 0.01188 -0.0710 0.9177 0.0878
-3.750 -0.1513 0.02128 0.01135 -0.0719 0.9142 0.0986
-3.500 -0.1176 0.02076 0.01087 -0.0733 0.9117 0.1140
-3.250 -0.0937 0.02040 0.01055 -0.0728 0.9062 0.1328
-3.000 -0.0678 0.01996 0.01025 -0.0728 0.9009 0.1619
-2.750 -0.0366 0.01935 0.00992 -0.0738 0.8976 0.2204
-2.500 -0.0058 0.01836 0.00962 -0.0750 0.8951 0.3690
-2.250 0.0105 0.01780 0.00984 -0.0728 0.8882 0.5604
-2.000 0.0355 0.01766 0.00994 -0.0717 0.8834 0.6567
-1.750 0.0650 0.01756 0.00992 -0.0714 0.8802 0.7166
-1.500 0.0882 0.01757 0.00996 -0.0701 0.8747 0.7587
-1.250 0.1109 0.01757 0.00999 -0.0686 0.8686 0.7947
-1.000 0.1395 0.01745 0.00993 -0.0680 0.8651 0.8348
-0.750 0.1739 0.01735 0.00993 -0.0680 0.8629 0.8912
-0.500 0.2148 0.01751 0.01011 -0.0702 0.8581 0.9377
-0.250 0.2564 0.01756 0.01009 -0.0732 0.8536 0.9591
0.000 0.3006 0.01752 0.00997 -0.0768 0.8504 0.9760
0.250 0.3462 0.01744 0.00982 -0.0806 0.8480 0.9919
0.500 0.3682 0.01756 0.00989 -0.0802 0.8397 1.0000
0.750 0.3928 0.01753 0.00979 -0.0798 0.8342 1.0000
1.250 0.4371 0.01769 0.00986 -0.0781 0.8207 1.0000
1.500 0.4681 0.01762 0.00976 -0.0787 0.8168 1.0000
1.750 0.4866 0.01785 0.00998 -0.0771 0.8082 1.0000
2.000 0.5157 0.01784 0.00995 -0.0773 0.8032 1.0000
2.250 0.5434 0.01786 0.00997 -0.0773 0.7978 1.0000
2.500 0.5665 0.01798 0.01011 -0.0764 0.7896 1.0000
2.750 0.6022 0.01766 0.00981 -0.0774 0.7850 1.0000
3.000 0.6252 0.01754 0.00970 -0.0761 0.7724 1.0000
3.250 0.6529 0.01718 0.00935 -0.0753 0.7585 1.0000
3.500 0.6812 0.01682 0.00900 -0.0746 0.7435 1.0000
3.750 0.7085 0.01660 0.00880 -0.0739 0.7286 1.0000
4.000 0.7356 0.01646 0.00866 -0.0733 0.7130 1.0000
4.250 0.7625 0.01634 0.00858 -0.0726 0.6958 1.0000
4.500 0.7902 0.01622 0.00846 -0.0720 0.6765 1.0000
4.750 0.8136 0.01626 0.00850 -0.0708 0.6534 1.0000
5.000 0.8386 0.01627 0.00849 -0.0698 0.6263 1.0000
5.250 0.8609 0.01639 0.00855 -0.0684 0.5917 1.0000
5.500 0.8824 0.01659 0.00861 -0.0668 0.5453 1.0000
5.750 0.9004 0.01700 0.00874 -0.0646 0.4784 1.0000
6.000 0.9113 0.01784 0.00905 -0.0614 0.3932 1.0000
6.250 0.9195 0.01891 0.00966 -0.0582 0.3227 1.0000
6.500 0.9294 0.01995 0.01037 -0.0554 0.2691 1.0000
6.750 0.9411 0.02091 0.01111 -0.0530 0.2293 1.0000
7.000 0.9531 0.02181 0.01183 -0.0506 0.1988 1.0000
7.250 0.9659 0.02268 0.01257 -0.0484 0.1752 1.0000
7.500 0.9789 0.02357 0.01335 -0.0462 0.1567 1.0000
7.750 0.9929 0.02444 0.01416 -0.0443 0.1414 1.0000
8.000 1.0069 0.02534 0.01503 -0.0425 0.1288 1.0000
8.250 1.0217 0.02621 0.01591 -0.0407 0.1179 1.0000
8.500 1.0358 0.02716 0.01685 -0.0390 0.1091 1.0000
8.750 1.0492 0.02817 0.01783 -0.0372 0.1015 1.0000
9.000 1.0641 0.02912 0.01887 -0.0356 0.0944 1.0000
9.250 1.0773 0.03020 0.01993 -0.0339 0.0888 1.0000
9.500 1.0920 0.03125 0.02105 -0.0324 0.0834 1.0000
9.750 1.1061 0.03232 0.02217 -0.0309 0.0785 1.0000
10.000 1.1191 0.03357 0.02341 -0.0293 0.0748 1.0000
10.250 1.1347 0.03468 0.02467 -0.0280 0.0705 1.0000
10.500 1.1481 0.03587 0.02590 -0.0266 0.0671 1.0000
10.750 1.1612 0.03724 0.02726 -0.0252 0.0643 1.0000
11.000 1.1767 0.03852 0.02877 -0.0239 0.0612 1.0000
11.250 1.1898 0.03985 0.03020 -0.0226 0.0583 1.0000
11.500 1.2015 0.04124 0.03161 -0.0213 0.0561 1.0000
11.750 1.2151 0.04285 0.03331 -0.0201 0.0541 1.0000
12.000 1.2274 0.04451 0.03522 -0.0187 0.0519 1.0000
12.250 1.2375 0.04617 0.03706 -0.0173 0.0499 1.0000
12.500 1.2459 0.04782 0.03879 -0.0160 0.0483 1.0000
12.750 1.2553 0.04954 0.04053 -0.0148 0.0469 1.0000
13.000 1.2627 0.05179 0.04300 -0.0134 0.0457 1.0000
13.250 1.2657 0.05429 0.04583 -0.0118 0.0444 1.0000
13.500 1.2664 0.05688 0.04867 -0.0104 0.0432 1.0000
13.750 1.2658 0.05947 0.05149 -0.0091 0.0421 1.0000
14.000 1.2644 0.06209 0.05428 -0.0080 0.0411 1.0000
14.250 1.2633 0.06470 0.05701 -0.0072 0.0403 1.0000
14.500 1.2631 0.06736 0.05975 -0.0065 0.0396 1.0000
14.750 1.2573 0.07086 0.06342 -0.0059 0.0390 1.0000
15.000 1.2409 0.07561 0.06851 -0.0058 0.0387 1.0000
15.250 1.2216 0.08095 0.07417 -0.0064 0.0384 1.0000
15.500 1.1993 0.08705 0.08057 -0.0079 0.0382 1.0000
15.750 1.1740 0.09414 0.08795 -0.0105 0.0381 1.0000
16.000 1.1448 0.10257 0.09666 -0.0145 0.0381 1.0000
16.250 1.1105 0.11306 0.10740 -0.0206 0.0382 1.0000
16.500 1.0656 0.12762 0.12218 -0.0302 0.0386 1.0000
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