FX 84-W-218 (fx84w218-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: FX 84-W-218 (fx84w218-il) Reynolds number: 200,000 Max Cl/Cd: 49.38 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w218-il-200000-n5.txt Download as CSV file: xf-fx84w218-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-218
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.6949 0.10571 0.10060 -0.0752 1.0000 0.0508
-18.750 -0.7232 0.09734 0.09203 -0.0801 1.0000 0.0516
-18.500 -0.7435 0.09054 0.08504 -0.0842 1.0000 0.0523
-18.250 -0.7623 0.08415 0.07845 -0.0879 1.0000 0.0531
-18.000 -0.7682 0.07995 0.07417 -0.0903 1.0000 0.0538
-17.750 -0.7678 0.07678 0.07099 -0.0921 1.0000 0.0544
-17.500 -0.7693 0.07339 0.06757 -0.0940 1.0000 0.0551
-17.250 -0.7693 0.06976 0.06387 -0.0966 0.9762 0.0559
-17.000 -0.7628 0.06588 0.05985 -0.1009 0.9592 0.0569
-16.750 -0.7562 0.06209 0.05588 -0.1049 0.9474 0.0580
-16.500 -0.7498 0.05866 0.05225 -0.1082 0.9359 0.0590
-16.250 -0.7414 0.05614 0.04968 -0.1103 0.9245 0.0599
-16.000 -0.7353 0.05367 0.04714 -0.1119 0.9141 0.0608
-15.750 -0.7311 0.05132 0.04469 -0.1130 0.9040 0.0618
-15.500 -0.7272 0.04909 0.04235 -0.1138 0.8954 0.0629
-15.250 -0.7232 0.04702 0.04014 -0.1142 0.8871 0.0641
-15.000 -0.7185 0.04512 0.03810 -0.1144 0.8799 0.0652
-14.750 -0.7138 0.04333 0.03630 -0.1145 0.8722 0.0662
-14.500 -0.7089 0.04166 0.03455 -0.1144 0.8650 0.0672
-14.250 -0.7032 0.04009 0.03289 -0.1142 0.8587 0.0686
-14.000 -0.6965 0.03860 0.03131 -0.1140 0.8521 0.0700
-13.750 -0.6893 0.03723 0.02979 -0.1135 0.8459 0.0715
-13.500 -0.6832 0.03587 0.02840 -0.1129 0.8405 0.0727
-13.250 -0.6757 0.03457 0.02707 -0.1124 0.8341 0.0741
-13.000 -0.6675 0.03339 0.02582 -0.1118 0.8281 0.0757
-12.750 -0.6580 0.03232 0.02463 -0.1110 0.8231 0.0775
-12.500 -0.6487 0.03125 0.02349 -0.1102 0.8181 0.0792
-12.250 -0.6398 0.03019 0.02242 -0.1094 0.8122 0.0808
-12.000 -0.6295 0.02925 0.02142 -0.1085 0.8067 0.0829
-11.750 -0.6181 0.02839 0.02046 -0.1075 0.8020 0.0850
-11.500 -0.6070 0.02753 0.01954 -0.1065 0.7974 0.0870
-11.250 -0.5962 0.02668 0.01869 -0.1055 0.7920 0.0892
-11.000 -0.5837 0.02593 0.01789 -0.1044 0.7868 0.0918
-10.750 -0.5700 0.02526 0.01712 -0.1033 0.7822 0.0944
-10.500 -0.5592 0.02451 0.01634 -0.1019 0.7780 0.0969
-10.250 -0.5455 0.02387 0.01569 -0.1009 0.7730 0.0999
-9.750 -0.5182 0.02266 0.01441 -0.0983 0.7635 0.1061
-9.500 -0.5040 0.02211 0.01380 -0.0970 0.7594 0.1098
-9.250 -0.4886 0.02162 0.01325 -0.0957 0.7551 0.1135
-9.000 -0.4750 0.02109 0.01275 -0.0942 0.7501 0.1173
-8.750 -0.4592 0.02065 0.01226 -0.0929 0.7456 0.1218
-8.500 -0.4451 0.02017 0.01177 -0.0913 0.7414 0.1261
-8.250 -0.4304 0.01976 0.01131 -0.0896 0.7377 0.1310
-8.000 -0.4155 0.01944 0.01097 -0.0879 0.7332 0.1361
-7.750 -0.4021 0.01913 0.01068 -0.0859 0.7285 0.1416
-7.500 -0.3855 0.01886 0.01038 -0.0843 0.7242 0.1477
-7.250 -0.3691 0.01852 0.01005 -0.0827 0.7203 0.1543
-7.000 -0.3497 0.01824 0.00970 -0.0815 0.7168 0.1617
-6.750 -0.3315 0.01795 0.00945 -0.0802 0.7125 0.1695
-6.500 -0.3119 0.01770 0.00922 -0.0791 0.7079 0.1780
-6.250 -0.2916 0.01744 0.00897 -0.0781 0.7037 0.1876
-6.000 -0.2714 0.01716 0.00869 -0.0770 0.6998 0.1974
-5.750 -0.2493 0.01691 0.00840 -0.0761 0.6964 0.2082
-5.500 -0.2284 0.01667 0.00821 -0.0752 0.6923 0.2201
-5.250 -0.2074 0.01645 0.00805 -0.0743 0.6879 0.2324
-5.000 -0.1853 0.01623 0.00785 -0.0734 0.6836 0.2455
-4.500 -0.1396 0.01575 0.00739 -0.0720 0.6764 0.2763
-4.250 -0.1173 0.01554 0.00725 -0.0712 0.6725 0.2935
-4.000 -0.0953 0.01536 0.00715 -0.0704 0.6681 0.3120
-3.750 -0.0725 0.01516 0.00702 -0.0697 0.6639 0.3321
-3.500 -0.0491 0.01495 0.00687 -0.0690 0.6599 0.3541
-3.250 -0.0247 0.01474 0.00669 -0.0685 0.6565 0.3778
-3.000 -0.0010 0.01459 0.00661 -0.0679 0.6527 0.4020
-2.750 0.0217 0.01446 0.00660 -0.0671 0.6482 0.4265
-2.500 0.0455 0.01433 0.00655 -0.0665 0.6439 0.4514
-2.250 0.0703 0.01420 0.00648 -0.0659 0.6399 0.4759
-2.000 0.0966 0.01409 0.00639 -0.0656 0.6365 0.4999
-1.750 0.1215 0.01404 0.00641 -0.0651 0.6326 0.5224
-1.500 0.1456 0.01403 0.00648 -0.0645 0.6279 0.5431
-1.250 0.1708 0.01400 0.00651 -0.0640 0.6234 0.5624
-1.000 0.1972 0.01398 0.00649 -0.0637 0.6195 0.5808
-0.750 0.2250 0.01396 0.00645 -0.0636 0.6162 0.5981
-0.500 0.2496 0.01402 0.00655 -0.0630 0.6118 0.6139
-0.250 0.2741 0.01407 0.00666 -0.0624 0.6069 0.6279
0.000 0.2999 0.01411 0.00669 -0.0620 0.6026 0.6418
0.250 0.3269 0.01413 0.00672 -0.0617 0.5989 0.6548
0.500 0.3546 0.01418 0.00673 -0.0616 0.5953 0.6671
0.750 0.3776 0.01429 0.00690 -0.0608 0.5903 0.6791
1.000 0.4020 0.01437 0.00701 -0.0602 0.5855 0.6898
1.250 0.4278 0.01444 0.00707 -0.0598 0.5815 0.7014
1.500 0.4553 0.01449 0.00709 -0.0596 0.5778 0.7118
1.750 0.4791 0.01461 0.00724 -0.0589 0.5733 0.7221
2.000 0.5018 0.01473 0.00739 -0.0580 0.5683 0.7314
2.250 0.5258 0.01483 0.00751 -0.0573 0.5638 0.7398
2.500 0.5524 0.01490 0.00753 -0.0571 0.5598 0.7494
2.750 0.5774 0.01500 0.00763 -0.0565 0.5557 0.7567
3.000 0.5973 0.01516 0.00785 -0.0552 0.5505 0.7649
3.250 0.6200 0.01528 0.00795 -0.0545 0.5456 0.7737
3.500 0.6441 0.01537 0.00805 -0.0537 0.5413 0.7799
3.750 0.6693 0.01547 0.00812 -0.0532 0.5373 0.7873
4.000 0.6870 0.01565 0.00834 -0.0517 0.5319 0.7960
4.250 0.7057 0.01579 0.00854 -0.0501 0.5268 0.8023
4.500 0.7284 0.01590 0.00862 -0.0492 0.5222 0.8097
4.750 0.7516 0.01602 0.00871 -0.0485 0.5178 0.8177
5.000 0.7613 0.01621 0.00899 -0.0454 0.5124 0.8247
5.250 0.7767 0.01637 0.00918 -0.0434 0.5071 0.8328
5.500 0.7983 0.01650 0.00927 -0.0424 0.5025 0.8405
5.750 0.8138 0.01673 0.00954 -0.0404 0.4977 0.8478
6.000 0.8250 0.01705 0.00992 -0.0379 0.4918 0.8572
6.250 0.8410 0.01727 0.01015 -0.0361 0.4865 0.8651
6.750 0.8702 0.01782 0.01077 -0.0322 0.4756 0.8836
7.000 0.8832 0.01814 0.01111 -0.0301 0.4696 0.8941
7.250 0.9027 0.01833 0.01128 -0.0290 0.4645 0.9036
7.750 0.9295 0.01917 0.01224 -0.0255 0.4522 0.9297
8.000 0.9538 0.01946 0.01252 -0.0255 0.4467 0.9424
8.250 0.9782 0.01998 0.01309 -0.0262 0.4403 0.9579
8.500 1.0064 0.02052 0.01368 -0.0278 0.4332 0.9776
8.750 1.0305 0.02087 0.01397 -0.0282 0.4271 1.0000
9.000 1.0412 0.02157 0.01471 -0.0268 0.4207 1.0000
9.250 1.0541 0.02222 0.01536 -0.0256 0.4140 1.0000
9.750 1.0803 0.02360 0.01672 -0.0233 0.4009 1.0000
10.000 1.0933 0.02431 0.01742 -0.0222 0.3941 1.0000
10.250 1.1067 0.02504 0.01812 -0.0211 0.3876 1.0000
10.500 1.1154 0.02603 0.01915 -0.0198 0.3801 1.0000
10.750 1.1290 0.02677 0.01984 -0.0188 0.3734 1.0000
11.000 1.1375 0.02785 0.02097 -0.0175 0.3663 1.0000
11.250 1.1473 0.02886 0.02197 -0.0163 0.3587 1.0000
11.500 1.1574 0.02989 0.02298 -0.0152 0.3516 1.0000
11.750 1.1642 0.03117 0.02429 -0.0140 0.3431 1.0000
12.000 1.1741 0.03226 0.02534 -0.0130 0.3357 1.0000
12.250 1.1797 0.03373 0.02686 -0.0119 0.3272 1.0000
12.500 1.1877 0.03500 0.02807 -0.0109 0.3191 1.0000
12.750 1.1929 0.03661 0.02974 -0.0099 0.3104 1.0000
13.000 1.1993 0.03808 0.03116 -0.0089 0.3023 1.0000
13.250 1.2043 0.03980 0.03293 -0.0081 0.2936 1.0000
13.500 1.2096 0.04146 0.03453 -0.0073 0.2855 1.0000
13.750 1.2151 0.04323 0.03636 -0.0066 0.2774 1.0000
14.000 1.2188 0.04512 0.03820 -0.0059 0.2691 1.0000
14.250 1.2241 0.04699 0.04012 -0.0053 0.2613 1.0000
14.500 1.2271 0.04903 0.04214 -0.0047 0.2533 1.0000
14.750 1.2318 0.05105 0.04419 -0.0043 0.2456 1.0000
15.000 1.2343 0.05324 0.04636 -0.0039 0.2379 1.0000
15.250 1.2383 0.05539 0.04855 -0.0036 0.2304 1.0000
15.500 1.2402 0.05776 0.05091 -0.0034 0.2229 1.0000
15.750 1.2439 0.06001 0.05319 -0.0032 0.2160 1.0000
16.000 1.2454 0.06253 0.05571 -0.0031 0.2088 1.0000
16.250 1.2483 0.06494 0.05814 -0.0031 0.2021 1.0000
16.500 1.2497 0.06757 0.06079 -0.0031 0.1952 1.0000
16.750 1.2515 0.07015 0.06338 -0.0032 0.1890 1.0000
17.000 1.2529 0.07289 0.06618 -0.0035 0.1823 1.0000
17.250 1.2535 0.07570 0.06897 -0.0037 0.1763 1.0000
17.500 1.2550 0.07852 0.07185 -0.0041 0.1699 1.0000
17.750 1.2543 0.08156 0.07488 -0.0046 0.1640 1.0000
18.000 1.2557 0.08448 0.07787 -0.0051 0.1580 1.0000
18.250 1.2548 0.08765 0.08104 -0.0057 0.1522 1.0000
18.500 1.2558 0.09067 0.08412 -0.0064 0.1469 1.0000
18.750 1.2547 0.09395 0.08742 -0.0072 0.1412 1.0000
19.000 1.2543 0.09718 0.09068 -0.0080 0.1362 1.0000
19.250 1.2540 0.10044 0.09399 -0.0089 0.1310 1.0000
|
Polar data table (+)
Polar graphs
<< Back to FX 84-W-218 (fx84w218-il)