AVISTAR (avistar-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AVISTAR (avistar-il) Reynolds number: 1,000,000 Max Cl/Cd: 71.44 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-avistar-il-1000000-n5.txt Download as CSV file: xf-avistar-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AVISTAR
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -1.0117 0.08044 0.07788 -0.0462 1.0000 0.0174
-16.750 -1.0736 0.06588 0.06302 -0.0558 1.0000 0.0174
-16.500 -1.1020 0.05773 0.05466 -0.0612 1.0000 0.0174
-16.250 -1.1215 0.05143 0.04817 -0.0651 1.0000 0.0174
-16.000 -1.1341 0.04655 0.04313 -0.0677 1.0000 0.0175
-15.750 -1.1427 0.04256 0.03898 -0.0694 1.0000 0.0175
-15.500 -1.1491 0.03910 0.03538 -0.0705 1.0000 0.0176
-15.250 -1.1525 0.03624 0.03240 -0.0709 1.0000 0.0177
-15.000 -1.1523 0.03394 0.03000 -0.0708 1.0000 0.0178
-14.750 -1.1486 0.03215 0.02813 -0.0703 1.0000 0.0179
-14.500 -1.1443 0.03056 0.02644 -0.0693 1.0000 0.0179
-14.250 -1.1361 0.02939 0.02521 -0.0682 1.0000 0.0181
-14.000 -1.1275 0.02831 0.02407 -0.0669 1.0000 0.0182
-13.750 -1.1175 0.02742 0.02312 -0.0654 1.0000 0.0183
-13.500 -1.1069 0.02663 0.02227 -0.0636 1.0000 0.0184
-13.250 -1.0962 0.02589 0.02147 -0.0617 1.0000 0.0185
-13.000 -1.0855 0.02523 0.02077 -0.0595 1.0000 0.0186
-12.750 -1.0757 0.02454 0.02001 -0.0571 0.9995 0.0187
-12.500 -1.0533 0.02373 0.01913 -0.0572 0.9863 0.0189
-12.250 -1.0299 0.02291 0.01822 -0.0574 0.9679 0.0191
-12.000 -1.0093 0.02216 0.01736 -0.0568 0.9436 0.0192
-11.750 -0.9931 0.02151 0.01657 -0.0551 0.9205 0.0194
-11.500 -0.9758 0.02089 0.01581 -0.0536 0.9038 0.0196
-11.000 -0.9378 0.01966 0.01434 -0.0512 0.8816 0.0200
-10.750 -0.9178 0.01908 0.01364 -0.0502 0.8726 0.0201
-10.500 -0.8967 0.01851 0.01297 -0.0493 0.8652 0.0203
-10.250 -0.8751 0.01800 0.01236 -0.0484 0.8578 0.0204
-10.000 -0.8531 0.01752 0.01178 -0.0476 0.8506 0.0205
-9.750 -0.8321 0.01689 0.01108 -0.0467 0.8423 0.0208
-9.500 -0.8100 0.01643 0.01054 -0.0458 0.8338 0.0210
-9.250 -0.7865 0.01604 0.01011 -0.0452 0.8269 0.0212
-9.000 -0.7625 0.01571 0.00973 -0.0447 0.8194 0.0214
-8.750 -0.7379 0.01544 0.00941 -0.0442 0.8126 0.0216
-8.500 -0.7133 0.01513 0.00906 -0.0437 0.8056 0.0219
-8.250 -0.6886 0.01482 0.00870 -0.0432 0.7993 0.0221
-8.000 -0.6641 0.01448 0.00830 -0.0427 0.7949 0.0224
-7.750 -0.6393 0.01412 0.00790 -0.0423 0.7906 0.0227
-7.500 -0.6144 0.01377 0.00751 -0.0418 0.7855 0.0229
-7.250 -0.5896 0.01345 0.00712 -0.0413 0.7802 0.0232
-7.000 -0.5645 0.01313 0.00675 -0.0408 0.7754 0.0235
-6.750 -0.5390 0.01283 0.00641 -0.0404 0.7710 0.0237
-6.500 -0.5135 0.01255 0.00608 -0.0401 0.7660 0.0239
-6.250 -0.4887 0.01221 0.00570 -0.0395 0.7610 0.0242
-6.000 -0.4633 0.01192 0.00539 -0.0391 0.7564 0.0246
-5.750 -0.4370 0.01169 0.00516 -0.0388 0.7509 0.0249
-5.500 -0.4109 0.01148 0.00492 -0.0385 0.7446 0.0253
-5.250 -0.3848 0.01127 0.00468 -0.0382 0.7386 0.0256
-5.000 -0.3584 0.01106 0.00444 -0.0379 0.7324 0.0260
-4.750 -0.3322 0.01085 0.00421 -0.0376 0.7257 0.0264
-4.500 -0.3058 0.01066 0.00398 -0.0373 0.7193 0.0268
-4.250 -0.2792 0.01048 0.00376 -0.0370 0.7119 0.0271
-4.000 -0.2528 0.01032 0.00356 -0.0367 0.7039 0.0275
-3.750 -0.2262 0.01013 0.00335 -0.0364 0.6956 0.0278
-3.500 -0.2002 0.00996 0.00314 -0.0360 0.6855 0.0284
-3.250 -0.1734 0.00983 0.00299 -0.0358 0.6740 0.0290
-3.000 -0.1467 0.00973 0.00285 -0.0356 0.6620 0.0297
-2.750 -0.1201 0.00964 0.00271 -0.0353 0.6490 0.0303
-2.500 -0.0934 0.00955 0.00258 -0.0350 0.6356 0.0308
-2.250 -0.0667 0.00947 0.00246 -0.0348 0.6221 0.0314
-2.000 -0.0400 0.00940 0.00234 -0.0345 0.6086 0.0320
-1.750 -0.0137 0.00933 0.00222 -0.0342 0.5951 0.0329
-1.500 0.0130 0.00928 0.00214 -0.0339 0.5820 0.0338
-1.250 0.0399 0.00924 0.00207 -0.0337 0.5698 0.0349
-1.000 0.0668 0.00922 0.00200 -0.0335 0.5582 0.0361
-0.750 0.0935 0.00919 0.00194 -0.0332 0.5461 0.0373
-0.500 0.1202 0.00916 0.00188 -0.0330 0.5344 0.0388
-0.250 0.1469 0.00916 0.00184 -0.0327 0.5224 0.0405
0.000 0.1738 0.00915 0.00181 -0.0325 0.5120 0.0422
0.250 0.2007 0.00912 0.00178 -0.0323 0.5040 0.0454
0.500 0.2278 0.00910 0.00175 -0.0321 0.4965 0.0498
0.750 0.2544 0.00907 0.00173 -0.0318 0.4891 0.0607
1.000 0.2697 0.00802 0.00159 -0.0296 0.4836 0.3644
1.250 0.2932 0.00775 0.00159 -0.0288 0.4772 0.4551
1.500 0.3166 0.00751 0.00160 -0.0280 0.4713 0.5374
1.750 0.3395 0.00724 0.00164 -0.0269 0.4659 0.6328
2.000 0.3641 0.00717 0.00169 -0.0262 0.4588 0.6841
2.250 0.3895 0.00716 0.00174 -0.0257 0.4495 0.7140
2.750 0.4398 0.00716 0.00185 -0.0245 0.4257 0.7711
3.000 0.4640 0.00717 0.00193 -0.0237 0.4110 0.8045
3.250 0.4875 0.00714 0.00204 -0.0227 0.3928 0.8666
3.500 0.5156 0.00731 0.00215 -0.0228 0.3620 0.9032
3.750 0.5443 0.00787 0.00242 -0.0236 0.2926 0.9206
4.000 0.5877 0.00842 0.00275 -0.0277 0.2420 0.9326
4.250 0.6391 0.00919 0.00318 -0.0338 0.1743 0.9402
4.500 0.6834 0.01075 0.00413 -0.0388 0.0321 0.9485
4.750 0.7325 0.01109 0.00443 -0.0439 0.0273 0.9555
5.000 0.7762 0.01141 0.00473 -0.0476 0.0250 0.9635
5.250 0.7944 0.01176 0.00506 -0.0456 0.0237 0.9951
5.500 0.8306 0.01206 0.00533 -0.0477 0.0223 0.9978
5.750 0.8650 0.01232 0.00558 -0.0494 0.0213 0.9994
6.000 0.8944 0.01258 0.00582 -0.0500 0.0204 1.0000
6.250 0.9166 0.01285 0.00608 -0.0491 0.0197 1.0000
6.500 0.9382 0.01316 0.00637 -0.0480 0.0191 1.0000
6.750 0.9600 0.01345 0.00666 -0.0469 0.0187 1.0000
7.000 0.9816 0.01374 0.00696 -0.0459 0.0183 1.0000
7.250 1.0029 0.01405 0.00727 -0.0448 0.0180 1.0000
7.500 1.0238 0.01437 0.00759 -0.0436 0.0176 1.0000
7.750 1.0444 0.01471 0.00794 -0.0424 0.0173 1.0000
8.000 1.0645 0.01506 0.00830 -0.0411 0.0169 1.0000
8.250 1.0841 0.01544 0.00868 -0.0398 0.0167 1.0000
8.500 1.1029 0.01585 0.00910 -0.0383 0.0164 1.0000
8.750 1.1207 0.01632 0.00958 -0.0367 0.0161 1.0000
9.000 1.1365 0.01686 0.01014 -0.0348 0.0158 1.0000
9.250 1.1504 0.01735 0.01065 -0.0325 0.0157 1.0000
9.500 1.1618 0.01781 0.01115 -0.0297 0.0156 1.0000
9.750 1.1736 0.01832 0.01170 -0.0272 0.0154 1.0000
10.000 1.1862 0.01888 0.01229 -0.0250 0.0153 1.0000
10.250 1.1991 0.01949 0.01294 -0.0229 0.0151 1.0000
10.500 1.2123 0.02015 0.01363 -0.0211 0.0149 1.0000
10.750 1.2250 0.02087 0.01439 -0.0193 0.0147 1.0000
11.000 1.2372 0.02169 0.01524 -0.0176 0.0146 1.0000
11.250 1.2490 0.02258 0.01617 -0.0159 0.0144 1.0000
11.500 1.2606 0.02352 0.01716 -0.0144 0.0143 1.0000
11.750 1.2719 0.02453 0.01821 -0.0130 0.0141 1.0000
12.000 1.2827 0.02562 0.01934 -0.0116 0.0140 1.0000
12.250 1.2928 0.02680 0.02057 -0.0103 0.0139 1.0000
12.500 1.3026 0.02805 0.02186 -0.0091 0.0138 1.0000
12.750 1.3116 0.02940 0.02326 -0.0079 0.0137 1.0000
13.000 1.3197 0.03087 0.02477 -0.0068 0.0136 1.0000
13.250 1.3272 0.03245 0.02640 -0.0058 0.0135 1.0000
13.500 1.3331 0.03420 0.02821 -0.0048 0.0134 1.0000
13.750 1.3378 0.03611 0.03017 -0.0038 0.0133 1.0000
14.000 1.3411 0.03822 0.03234 -0.0030 0.0132 1.0000
14.250 1.3420 0.04062 0.03481 -0.0022 0.0131 1.0000
14.500 1.3417 0.04321 0.03747 -0.0016 0.0130 1.0000
14.750 1.3424 0.04581 0.04016 -0.0011 0.0129 1.0000
15.000 1.3458 0.04822 0.04263 -0.0009 0.0129 1.0000
15.250 1.3486 0.05075 0.04523 -0.0008 0.0128 1.0000
15.500 1.3510 0.05338 0.04794 -0.0007 0.0128 1.0000
15.750 1.3523 0.05619 0.05083 -0.0008 0.0127 1.0000
16.000 1.3537 0.05905 0.05376 -0.0009 0.0127 1.0000
16.250 1.3547 0.06200 0.05679 -0.0012 0.0126 1.0000
16.500 1.3548 0.06506 0.05993 -0.0014 0.0126 1.0000
16.750 1.3553 0.06814 0.06308 -0.0018 0.0125 1.0000
17.000 1.3551 0.07132 0.06634 -0.0022 0.0125 1.0000
17.250 1.3543 0.07463 0.06972 -0.0028 0.0124 1.0000
17.750 1.3526 0.08128 0.07653 -0.0039 0.0123 1.0000
18.000 1.3514 0.08475 0.08009 -0.0047 0.0123 1.0000
18.250 1.3502 0.08824 0.08365 -0.0055 0.0122 1.0000
18.500 1.3488 0.09177 0.08726 -0.0063 0.0121 1.0000
18.750 1.3466 0.09545 0.09102 -0.0073 0.0120 1.0000
19.000 1.3451 0.09906 0.09470 -0.0083 0.0119 1.0000
19.250 1.3423 0.10291 0.09863 -0.0094 0.0119 1.0000
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