FX 84-W-097 (fx84w097-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 84-W-097 (fx84w097-il) Reynolds number: 500,000 Max Cl/Cd: 96.19 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx84w097-il-500000-n5.txt Download as CSV file: xf-fx84w097-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 84-W-097
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.4962 0.10654 0.10426 -0.0110 1.0000 0.0085
-10.750 -0.4979 0.10150 0.09923 -0.0134 1.0000 0.0086
-9.750 -0.7241 0.03120 0.02800 -0.0570 0.9513 0.0083
-9.500 -0.7160 0.02760 0.02388 -0.0565 0.9276 0.0085
-9.250 -0.7057 0.02473 0.02058 -0.0555 0.9106 0.0087
-9.000 -0.6884 0.02322 0.01883 -0.0546 0.8975 0.0090
-8.500 -0.6456 0.02137 0.01665 -0.0535 0.8756 0.0096
-8.250 -0.6232 0.02042 0.01551 -0.0530 0.8662 0.0099
-7.750 -0.5777 0.01815 0.01276 -0.0520 0.8481 0.0107
-7.500 -0.5539 0.01716 0.01153 -0.0516 0.8401 0.0111
-7.250 -0.5293 0.01630 0.01046 -0.0512 0.8318 0.0115
-7.000 -0.5041 0.01560 0.00958 -0.0509 0.8242 0.0118
-6.750 -0.4795 0.01466 0.00851 -0.0505 0.8164 0.0125
-6.500 -0.4535 0.01414 0.00789 -0.0503 0.8090 0.0131
-6.250 -0.4271 0.01369 0.00733 -0.0501 0.8016 0.0138
-6.000 -0.4005 0.01326 0.00680 -0.0500 0.7944 0.0147
-5.750 -0.3738 0.01288 0.00631 -0.0498 0.7870 0.0157
-5.500 -0.3473 0.01238 0.00572 -0.0496 0.7800 0.0167
-5.250 -0.3206 0.01196 0.00524 -0.0495 0.7725 0.0180
-5.000 -0.2936 0.01163 0.00483 -0.0493 0.7654 0.0193
-4.750 -0.2664 0.01133 0.00445 -0.0492 0.7578 0.0207
-4.500 -0.2391 0.01102 0.00407 -0.0491 0.7508 0.0224
-4.250 -0.2119 0.01070 0.00372 -0.0490 0.7435 0.0249
-4.000 -0.1844 0.01047 0.00341 -0.0489 0.7367 0.0273
-3.750 -0.1568 0.01024 0.00312 -0.0489 0.7295 0.0296
-3.500 -0.1292 0.00999 0.00286 -0.0488 0.7229 0.0344
-3.250 -0.1014 0.00982 0.00264 -0.0488 0.7157 0.0386
-3.000 -0.0738 0.00961 0.00242 -0.0488 0.7091 0.0458
-2.750 -0.0459 0.00943 0.00224 -0.0488 0.7019 0.0547
-2.500 -0.0182 0.00928 0.00207 -0.0487 0.6952 0.0664
-2.250 0.0097 0.00910 0.00192 -0.0488 0.6877 0.0816
-2.000 0.0375 0.00895 0.00180 -0.0488 0.6807 0.1027
-1.750 0.0653 0.00877 0.00169 -0.0488 0.6731 0.1289
-1.500 0.0930 0.00859 0.00158 -0.0489 0.6661 0.1650
-1.250 0.1207 0.00837 0.00150 -0.0489 0.6585 0.2115
-1.000 0.1481 0.00813 0.00143 -0.0490 0.6515 0.2750
-0.750 0.1752 0.00780 0.00137 -0.0491 0.6441 0.3681
-0.500 0.2017 0.00740 0.00131 -0.0490 0.6374 0.4885
-0.250 0.2274 0.00694 0.00131 -0.0487 0.6302 0.6320
0.000 0.2523 0.00664 0.00134 -0.0480 0.6235 0.7421
0.250 0.2773 0.00649 0.00139 -0.0472 0.6162 0.8141
0.500 0.3025 0.00644 0.00142 -0.0463 0.6094 0.8586
0.750 0.3279 0.00642 0.00145 -0.0455 0.6018 0.8925
1.000 0.3537 0.00643 0.00148 -0.0448 0.5943 0.9239
1.250 0.3831 0.00645 0.00149 -0.0449 0.5858 0.9501
1.500 0.4221 0.00648 0.00149 -0.0472 0.5772 0.9793
1.750 0.4662 0.00652 0.00150 -0.0507 0.5680 0.9971
2.000 0.4958 0.00659 0.00153 -0.0511 0.5597 1.0000
2.250 0.5213 0.00668 0.00158 -0.0507 0.5518 1.0000
2.500 0.5474 0.00676 0.00163 -0.0504 0.5428 1.0000
2.750 0.5736 0.00687 0.00171 -0.0501 0.5326 1.0000
3.000 0.6000 0.00698 0.00178 -0.0498 0.5213 1.0000
3.250 0.6267 0.00710 0.00187 -0.0497 0.5110 1.0000
3.500 0.6536 0.00721 0.00198 -0.0495 0.5007 1.0000
3.750 0.6805 0.00734 0.00209 -0.0494 0.4892 1.0000
4.000 0.7073 0.00749 0.00221 -0.0492 0.4772 1.0000
4.250 0.7341 0.00764 0.00234 -0.0491 0.4636 1.0000
4.500 0.7599 0.00790 0.00251 -0.0489 0.4356 1.0000
4.750 0.7849 0.00827 0.00270 -0.0485 0.3952 1.0000
5.000 0.8100 0.00863 0.00293 -0.0483 0.3601 1.0000
5.250 0.8349 0.00903 0.00319 -0.0480 0.3254 1.0000
5.500 0.8586 0.00957 0.00354 -0.0476 0.2792 1.0000
5.750 0.8813 0.01025 0.00396 -0.0471 0.2251 1.0000
6.250 0.9239 0.01187 0.00501 -0.0459 0.1146 1.0000
6.500 0.9454 0.01262 0.00556 -0.0452 0.0765 1.0000
6.750 0.9679 0.01322 0.00606 -0.0447 0.0542 1.0000
7.000 0.9907 0.01376 0.00653 -0.0442 0.0411 1.0000
7.250 1.0137 0.01426 0.00701 -0.0436 0.0326 1.0000
7.500 1.0367 0.01474 0.00749 -0.0431 0.0267 1.0000
7.750 1.0590 0.01527 0.00803 -0.0425 0.0223 1.0000
8.000 1.0814 0.01575 0.00855 -0.0419 0.0197 1.0000
8.250 1.1021 0.01636 0.00917 -0.0410 0.0171 1.0000
8.500 1.1235 0.01690 0.00977 -0.0403 0.0156 1.0000
8.750 1.1440 0.01747 0.01039 -0.0395 0.0143 1.0000
9.000 1.1631 0.01813 0.01109 -0.0385 0.0130 1.0000
9.250 1.1803 0.01890 0.01191 -0.0372 0.0119 1.0000
9.500 1.1979 0.01957 0.01266 -0.0360 0.0113 1.0000
9.750 1.2139 0.02030 0.01346 -0.0346 0.0107 1.0000
10.000 1.2270 0.02105 0.01428 -0.0328 0.0103 1.0000
10.250 1.2376 0.02186 0.01516 -0.0307 0.0098 1.0000
10.500 1.2471 0.02279 0.01616 -0.0286 0.0095 1.0000
10.750 1.2552 0.02388 0.01732 -0.0267 0.0091 1.0000
11.000 1.2596 0.02532 0.01884 -0.0246 0.0087 1.0000
11.250 1.2680 0.02655 0.02017 -0.0231 0.0084 1.0000
11.500 1.2751 0.02797 0.02169 -0.0216 0.0082 1.0000
11.750 1.2852 0.02919 0.02300 -0.0206 0.0079 1.0000
12.000 1.2932 0.03065 0.02456 -0.0195 0.0076 1.0000
12.250 1.2989 0.03236 0.02637 -0.0184 0.0074 1.0000
12.500 1.3055 0.03406 0.02817 -0.0176 0.0072 1.0000
12.750 1.3103 0.03598 0.03018 -0.0168 0.0070 1.0000
13.000 1.3149 0.03799 0.03231 -0.0162 0.0068 1.0000
13.250 1.3197 0.04004 0.03445 -0.0157 0.0066 1.0000
13.500 1.3226 0.04236 0.03687 -0.0154 0.0065 1.0000
13.750 1.3242 0.04490 0.03951 -0.0152 0.0063 1.0000
14.000 1.3240 0.04772 0.04245 -0.0152 0.0062 1.0000
14.250 1.3212 0.05096 0.04580 -0.0154 0.0061 1.0000
14.500 1.3157 0.05463 0.04960 -0.0157 0.0060 1.0000
14.750 1.3104 0.05844 0.05354 -0.0163 0.0059 1.0000
15.000 1.3103 0.06175 0.05700 -0.0171 0.0059 1.0000
15.250 1.3069 0.06564 0.06104 -0.0182 0.0058 1.0000
15.500 1.3023 0.06989 0.06544 -0.0196 0.0057 1.0000
15.750 1.2969 0.07439 0.07010 -0.0212 0.0056 1.0000
16.000 1.2907 0.07920 0.07507 -0.0231 0.0056 1.0000
16.250 1.2819 0.08464 0.08067 -0.0254 0.0055 1.0000
16.500 1.2732 0.09026 0.08645 -0.0281 0.0055 1.0000
16.750 1.2624 0.09648 0.09283 -0.0311 0.0054 1.0000
17.000 1.2506 0.10312 0.09964 -0.0345 0.0054 1.0000
17.250 1.2373 0.11034 0.10703 -0.0385 0.0053 1.0000
17.500 1.2236 0.11779 0.11463 -0.0426 0.0053 1.0000
17.750 1.2086 0.12592 0.12292 -0.0473 0.0053 1.0000
18.000 1.1918 0.13471 0.13187 -0.0525 0.0053 1.0000
18.250 1.1738 0.14420 0.14153 -0.0582 0.0053 1.0000
18.500 1.1542 0.15451 0.15198 -0.0645 0.0054 1.0000
18.750 1.1280 0.16733 0.16497 -0.0724 0.0054 1.0000
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