WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Reynolds number: 1,000,000 Max Cl/Cd: 86.79 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx77w343-il-1000000.txt Download as CSV file: xf-fx77w343-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 77-W-343 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0997 0.09446 0.08748 -0.0141 0.4731 0.0206
-19.500 -1.0944 0.09180 0.08476 -0.0148 0.4700 0.0207
-19.250 -1.0885 0.08924 0.08213 -0.0154 0.4667 0.0208
-19.000 -1.0812 0.08686 0.07970 -0.0159 0.4652 0.0209
-18.750 -1.0752 0.08431 0.07710 -0.0164 0.4638 0.0210
-18.500 -1.0665 0.08213 0.07488 -0.0169 0.4623 0.0211
-18.250 -1.0579 0.07993 0.07263 -0.0173 0.4607 0.0212
-18.000 -1.0504 0.07762 0.07025 -0.0177 0.4590 0.0213
-17.750 -1.0402 0.07565 0.06824 -0.0180 0.4573 0.0214
-17.500 -1.0298 0.07371 0.06625 -0.0183 0.4555 0.0216
-17.250 -1.0202 0.07165 0.06414 -0.0186 0.4535 0.0218
-17.000 -1.0098 0.06971 0.06216 -0.0188 0.4513 0.0220
-16.750 -0.9982 0.06791 0.06032 -0.0191 0.4490 0.0223
-16.500 -0.9875 0.06602 0.05839 -0.0193 0.4467 0.0226
-16.250 -0.9763 0.06422 0.05658 -0.0194 0.4461 0.0230
-16.000 -0.9641 0.06255 0.05490 -0.0195 0.4455 0.0234
-15.750 -0.9524 0.06082 0.05316 -0.0196 0.4447 0.0238
-15.500 -0.9403 0.05914 0.05147 -0.0197 0.4438 0.0243
-15.250 -0.9260 0.05769 0.05002 -0.0198 0.4428 0.0247
-15.000 -0.9109 0.05634 0.04872 -0.0199 0.4417 0.0278
-14.750 -0.8952 0.05504 0.04740 -0.0200 0.4405 0.0300
-14.500 -0.8804 0.05365 0.04598 -0.0201 0.4393 0.0309
-14.250 -0.8644 0.05238 0.04468 -0.0202 0.4381 0.0315
-14.000 -0.8476 0.05123 0.04350 -0.0203 0.4367 0.0320
-13.750 -0.8316 0.05000 0.04225 -0.0203 0.4353 0.0325
-13.500 -0.8155 0.04878 0.04100 -0.0204 0.4337 0.0331
-13.250 -0.7994 0.04754 0.03973 -0.0205 0.4319 0.0338
-13.000 -0.7819 0.04648 0.03864 -0.0205 0.4298 0.0344
-12.750 -0.7636 0.04550 0.03764 -0.0207 0.4277 0.0349
-12.500 -0.7456 0.04449 0.03660 -0.0207 0.4271 0.0353
-12.250 -0.7277 0.04345 0.03554 -0.0208 0.4267 0.0356
-12.000 -0.7115 0.04230 0.03438 -0.0207 0.4263 0.0360
-11.750 -0.6959 0.04115 0.03322 -0.0206 0.4259 0.0364
-11.500 -0.6795 0.04007 0.03214 -0.0204 0.4254 0.0369
-11.250 -0.6628 0.03903 0.03109 -0.0203 0.4248 0.0374
-11.000 -0.6464 0.03798 0.03002 -0.0201 0.4243 0.0378
-10.750 -0.6300 0.03693 0.02896 -0.0200 0.4236 0.0383
-10.500 -0.6121 0.03603 0.02805 -0.0199 0.4230 0.0387
-10.250 -0.5937 0.03518 0.02718 -0.0198 0.4223 0.0391
-10.000 -0.5753 0.03434 0.02633 -0.0196 0.4217 0.0394
-9.750 -0.5571 0.03352 0.02549 -0.0194 0.4210 0.0397
-9.500 -0.5420 0.03255 0.02451 -0.0190 0.4204 0.0401
-9.250 -0.5283 0.03150 0.02345 -0.0185 0.4198 0.0408
-9.000 -0.5125 0.03060 0.02254 -0.0180 0.4192 0.0413
-8.750 -0.4969 0.02969 0.02163 -0.0175 0.4185 0.0419
-8.500 -0.4816 0.02877 0.02070 -0.0170 0.4180 0.0424
-8.250 -0.4668 0.02784 0.01975 -0.0164 0.4174 0.0430
-8.000 -0.4509 0.02699 0.01889 -0.0158 0.4168 0.0435
-7.750 -0.4359 0.02611 0.01799 -0.0151 0.4163 0.0442
-7.500 -0.4254 0.02508 0.01696 -0.0138 0.4157 0.0453
-7.250 -0.4280 0.02403 0.01590 -0.0104 0.4153 0.0462
-7.000 -0.4124 0.02316 0.01505 -0.0101 0.4147 0.0478
-6.750 -0.3925 0.02227 0.01423 -0.0107 0.4140 0.0574
-6.500 -0.3653 0.02177 0.01372 -0.0118 0.4133 0.0614
-6.250 -0.3372 0.02122 0.01316 -0.0133 0.4125 0.0633
-6.000 -0.3071 0.02078 0.01271 -0.0150 0.4116 0.0652
-5.750 -0.2758 0.02045 0.01236 -0.0168 0.4107 0.0667
-5.500 -0.2437 0.02007 0.01199 -0.0190 0.4094 0.0682
-5.250 -0.2103 0.01965 0.01157 -0.0212 0.4088 0.0700
-5.000 -0.1760 0.01925 0.01117 -0.0235 0.4085 0.0718
-4.750 -0.1418 0.01887 0.01081 -0.0258 0.4082 0.0750
-4.500 -0.1074 0.01839 0.01043 -0.0282 0.4078 0.0888
-4.250 -0.0732 0.01813 0.01020 -0.0301 0.4074 0.1017
-4.000 -0.0388 0.01788 0.00997 -0.0321 0.4069 0.1073
-3.750 -0.0033 0.01739 0.00963 -0.0348 0.4063 0.1351
-3.500 0.0317 0.01713 0.00941 -0.0369 0.4056 0.1514
-3.250 0.0685 0.01658 0.00906 -0.0399 0.4049 0.1953
-3.000 0.1057 0.01604 0.00872 -0.0429 0.4042 0.2412
-2.750 0.1438 0.01545 0.00837 -0.0461 0.4035 0.2951
-2.500 0.1822 0.01487 0.00803 -0.0494 0.4027 0.3568
-2.250 0.2210 0.01429 0.00771 -0.0527 0.4020 0.4230
-2.000 0.2564 0.01415 0.00764 -0.0548 0.4014 0.4462
-1.750 0.2924 0.01396 0.00756 -0.0570 0.4008 0.4748
-1.500 0.3274 0.01389 0.00753 -0.0588 0.4002 0.4960
-1.250 0.3623 0.01384 0.00753 -0.0607 0.3996 0.5088
-1.000 0.3976 0.01374 0.00756 -0.0627 0.3990 0.5358
-0.750 0.4318 0.01379 0.00761 -0.0642 0.3984 0.5554
-0.500 0.4660 0.01383 0.00770 -0.0659 0.3978 0.5665
-0.250 0.4998 0.01391 0.00776 -0.0674 0.3972 0.5734
0.000 0.5336 0.01401 0.00788 -0.0689 0.3965 0.5800
0.250 0.5671 0.01415 0.00804 -0.0703 0.3958 0.5860
0.500 0.6005 0.01431 0.00819 -0.0718 0.3949 0.5909
0.750 0.6336 0.01452 0.00839 -0.0732 0.3939 0.5952
1.000 0.6663 0.01480 0.00868 -0.0745 0.3928 0.5993
1.250 0.6986 0.01520 0.00907 -0.0758 0.3914 0.6036
1.500 0.7320 0.01530 0.00916 -0.0773 0.3911 0.6082
1.750 0.7654 0.01540 0.00924 -0.0787 0.3908 0.6109
2.000 0.7984 0.01548 0.00935 -0.0801 0.3904 0.6134
2.250 0.8313 0.01558 0.00947 -0.0815 0.3899 0.6154
2.500 0.8642 0.01568 0.00958 -0.0829 0.3893 0.6173
2.750 0.8970 0.01578 0.00970 -0.0842 0.3886 0.6193
3.000 0.9296 0.01591 0.00984 -0.0856 0.3879 0.6216
3.250 0.9622 0.01606 0.00999 -0.0869 0.3872 0.6241
3.500 0.9947 0.01620 0.01012 -0.0883 0.3864 0.6262
3.750 1.0273 0.01632 0.01025 -0.0897 0.3856 0.6275
4.000 1.0597 0.01645 0.01036 -0.0910 0.3847 0.6285
4.250 1.0921 0.01653 0.01044 -0.0924 0.3838 0.6297
4.500 1.1243 0.01654 0.01047 -0.0938 0.3829 0.6326
4.750 1.1560 0.01666 0.01060 -0.0951 0.3819 0.6347
5.000 1.1874 0.01680 0.01077 -0.0963 0.3810 0.6367
5.250 1.2186 0.01696 0.01094 -0.0974 0.3800 0.6386
5.500 1.2496 0.01712 0.01111 -0.0986 0.3789 0.6402
5.750 1.2802 0.01733 0.01130 -0.0998 0.3774 0.6419
6.000 1.3101 0.01763 0.01158 -0.1008 0.3754 0.6434
6.250 1.3401 0.01791 0.01187 -0.1019 0.3739 0.6447
6.500 1.3713 0.01796 0.01194 -0.1032 0.3734 0.6457
6.750 1.4022 0.01803 0.01203 -0.1045 0.3727 0.6465
7.000 1.4330 0.01809 0.01211 -0.1057 0.3717 0.6473
7.250 1.4636 0.01816 0.01221 -0.1069 0.3705 0.6479
7.500 1.4939 0.01825 0.01230 -0.1081 0.3689 0.6484
7.750 1.5238 0.01836 0.01242 -0.1092 0.3673 0.6489
8.000 1.5541 0.01835 0.01242 -0.1105 0.3658 0.6510
8.250 1.5830 0.01848 0.01256 -0.1115 0.3646 0.6523
8.500 1.6109 0.01865 0.01275 -0.1123 0.3633 0.6534
8.750 1.6376 0.01887 0.01298 -0.1130 0.3620 0.6543
9.000 1.6628 0.01916 0.01328 -0.1134 0.3605 0.6553
9.250 1.6856 0.01954 0.01367 -0.1135 0.3589 0.6561
9.500 1.7072 0.01996 0.01411 -0.1134 0.3574 0.6570
9.750 1.7301 0.02029 0.01449 -0.1135 0.3566 0.6579
10.000 1.7441 0.02077 0.01503 -0.1120 0.3557 0.6588
10.250 1.7547 0.02150 0.01582 -0.1103 0.3544 0.6596
10.500 1.7698 0.02231 0.01669 -0.1096 0.3529 0.6605
10.750 1.7849 0.02325 0.01766 -0.1093 0.3511 0.6613
11.000 1.7995 0.02431 0.01876 -0.1091 0.3492 0.6622
11.250 1.8128 0.02553 0.02002 -0.1090 0.3472 0.6631
11.500 1.8229 0.02707 0.02158 -0.1088 0.3449 0.6640
11.750 1.8274 0.02909 0.02362 -0.1084 0.3424 0.6648
12.000 1.8370 0.03075 0.02534 -0.1083 0.3407 0.6656
12.250 1.8444 0.03260 0.02724 -0.1081 0.3389 0.6664
12.500 1.8475 0.03483 0.02952 -0.1078 0.3369 0.6670
12.750 1.8456 0.03749 0.03223 -0.1072 0.3347 0.6675
13.000 1.8327 0.04113 0.03593 -0.1062 0.3322 0.6678
13.250 1.8056 0.04608 0.04093 -0.1046 0.3290 0.6681
13.500 1.7839 0.05068 0.04560 -0.1034 0.3263 0.6683
13.750 1.7660 0.05514 0.05017 -0.1026 0.3244 0.6685
14.000 1.7352 0.06096 0.05610 -0.1015 0.3218 0.6687
14.250 1.6988 0.06741 0.06263 -0.1003 0.3187 0.6688
14.500 1.6622 0.07394 0.06922 -0.0992 0.3151 0.6689
14.750 1.6632 0.07658 0.07185 -0.0992 0.3124 0.6691
15.000 1.6392 0.08202 0.07739 -0.0988 0.3101 0.6693
15.250 1.5526 0.09451 0.09010 -0.0970 0.3044 0.6692
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