AVISTAR (avistar-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AVISTAR (avistar-il) Reynolds number: 500,000 Max Cl/Cd: 71.98 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-avistar-il-500000-n5.txt Download as CSV file: xf-avistar-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.750 -0.7819 0.05460 0.05129 -0.0673 1.0000 0.0206
-12.500 -0.8032 0.04934 0.04585 -0.0701 1.0000 0.0207
-12.250 -0.8191 0.04554 0.04189 -0.0708 1.0000 0.0207
-12.000 -0.8279 0.04299 0.03921 -0.0700 1.0000 0.0208
-11.750 -0.8362 0.04082 0.03691 -0.0680 1.0000 0.0209
-11.500 -0.8410 0.03930 0.03529 -0.0650 1.0000 0.0210
-11.250 -0.8427 0.03789 0.03378 -0.0621 0.9965 0.0210
-11.000 -0.8284 0.03614 0.03187 -0.0623 0.9805 0.0212
-10.750 -0.8126 0.03442 0.02998 -0.0623 0.9629 0.0214
-10.500 -0.7974 0.03270 0.02807 -0.0619 0.9456 0.0216
-10.250 -0.7843 0.03113 0.02630 -0.0607 0.9292 0.0218
-10.000 -0.7725 0.02950 0.02443 -0.0589 0.9147 0.0221
-9.750 -0.7602 0.02776 0.02243 -0.0571 0.9029 0.0225
-9.500 -0.7470 0.02588 0.02025 -0.0554 0.8928 0.0230
-9.250 -0.7317 0.02409 0.01814 -0.0538 0.8840 0.0235
-9.000 -0.7138 0.02277 0.01651 -0.0524 0.8746 0.0239
-8.750 -0.6932 0.02196 0.01561 -0.0515 0.8657 0.0242
-8.500 -0.6715 0.02141 0.01498 -0.0507 0.8565 0.0244
-8.250 -0.6490 0.02092 0.01441 -0.0500 0.8484 0.0246
-8.000 -0.6263 0.02035 0.01376 -0.0493 0.8400 0.0249
-7.750 -0.6034 0.01977 0.01307 -0.0486 0.8328 0.0252
-7.500 -0.5796 0.01916 0.01237 -0.0480 0.8266 0.0255
-7.250 -0.5559 0.01853 0.01165 -0.0474 0.8208 0.0259
-7.000 -0.5319 0.01791 0.01093 -0.0468 0.8158 0.0263
-6.750 -0.5075 0.01729 0.01022 -0.0463 0.8111 0.0267
-6.500 -0.4830 0.01673 0.00956 -0.0458 0.8057 0.0272
-6.250 -0.4581 0.01628 0.00900 -0.0453 0.8002 0.0276
-6.000 -0.4340 0.01573 0.00841 -0.0447 0.7951 0.0280
-5.750 -0.4090 0.01530 0.00798 -0.0443 0.7896 0.0284
-5.500 -0.3839 0.01493 0.00759 -0.0439 0.7841 0.0288
-5.250 -0.3589 0.01457 0.00718 -0.0434 0.7789 0.0291
-5.000 -0.3336 0.01421 0.00679 -0.0429 0.7738 0.0296
-4.750 -0.3083 0.01385 0.00640 -0.0425 0.7679 0.0301
-4.500 -0.2832 0.01351 0.00601 -0.0420 0.7617 0.0306
-4.250 -0.2580 0.01319 0.00564 -0.0414 0.7556 0.0312
-4.000 -0.2322 0.01292 0.00532 -0.0410 0.7486 0.0317
-3.750 -0.2076 0.01257 0.00496 -0.0404 0.7418 0.0324
-3.500 -0.1819 0.01231 0.00470 -0.0400 0.7352 0.0330
-3.250 -0.1562 0.01207 0.00444 -0.0396 0.7274 0.0337
-3.000 -0.1305 0.01185 0.00418 -0.0391 0.7201 0.0344
-2.750 -0.1045 0.01162 0.00394 -0.0387 0.7114 0.0351
-2.500 -0.0787 0.01144 0.00370 -0.0383 0.7025 0.0359
-2.250 -0.0525 0.01126 0.00349 -0.0379 0.6918 0.0366
-2.000 -0.0271 0.01105 0.00325 -0.0374 0.6809 0.0377
-1.750 -0.0011 0.01092 0.00309 -0.0370 0.6689 0.0390
-1.500 0.0252 0.01080 0.00293 -0.0366 0.6568 0.0403
-1.250 0.0514 0.01070 0.00278 -0.0363 0.6446 0.0415
-1.000 0.0772 0.01059 0.00263 -0.0358 0.6319 0.0430
-0.750 0.1034 0.01051 0.00251 -0.0354 0.6189 0.0449
-0.500 0.1297 0.01046 0.00242 -0.0351 0.6065 0.0472
-0.250 0.1557 0.01041 0.00233 -0.0347 0.5942 0.0506
0.250 0.2075 0.01030 0.00219 -0.0338 0.5690 0.0691
0.500 0.2199 0.00906 0.00201 -0.0313 0.5580 0.4048
0.750 0.2403 0.00870 0.00199 -0.0298 0.5459 0.5178
1.000 0.2592 0.00835 0.00205 -0.0279 0.5359 0.6404
1.250 0.2823 0.00829 0.00210 -0.0268 0.5266 0.6920
1.500 0.3069 0.00822 0.00215 -0.0260 0.5185 0.7309
1.750 0.3311 0.00817 0.00220 -0.0252 0.5104 0.7699
2.000 0.3567 0.00810 0.00227 -0.0246 0.5028 0.8094
2.250 0.3865 0.00804 0.00237 -0.0249 0.4950 0.8663
2.500 0.4246 0.00808 0.00246 -0.0271 0.4883 0.9084
2.750 0.4780 0.00820 0.00257 -0.0330 0.4742 0.9292
3.000 0.5263 0.00838 0.00269 -0.0378 0.4567 0.9374
3.250 0.5736 0.00857 0.00282 -0.0423 0.4394 0.9434
3.500 0.6166 0.00882 0.00298 -0.0458 0.4183 0.9498
3.750 0.6579 0.00914 0.00316 -0.0490 0.3843 0.9568
4.000 0.6932 0.00984 0.00349 -0.0512 0.3095 0.9667
4.500 0.7456 0.01154 0.00450 -0.0518 0.1883 0.9981
4.750 0.7609 0.01329 0.00552 -0.0506 0.0385 1.0000
5.000 0.7817 0.01359 0.00580 -0.0494 0.0332 1.0000
5.250 0.8027 0.01390 0.00608 -0.0482 0.0305 1.0000
5.500 0.8241 0.01418 0.00637 -0.0470 0.0288 1.0000
5.750 0.8449 0.01450 0.00668 -0.0458 0.0273 1.0000
6.000 0.8650 0.01487 0.00705 -0.0445 0.0262 1.0000
6.250 0.8857 0.01521 0.00740 -0.0432 0.0254 1.0000
6.500 0.9058 0.01557 0.00776 -0.0419 0.0245 1.0000
6.750 0.9254 0.01595 0.00815 -0.0405 0.0237 1.0000
7.000 0.9442 0.01638 0.00859 -0.0390 0.0230 1.0000
7.250 0.9614 0.01689 0.00910 -0.0373 0.0223 1.0000
7.500 0.9796 0.01733 0.00955 -0.0357 0.0219 1.0000
7.750 0.9968 0.01781 0.01006 -0.0340 0.0215 1.0000
8.000 1.0130 0.01832 0.01060 -0.0321 0.0210 1.0000
8.250 1.0269 0.01885 0.01116 -0.0298 0.0206 1.0000
8.500 1.0372 0.01940 0.01173 -0.0269 0.0203 1.0000
8.750 1.0473 0.01999 0.01235 -0.0241 0.0200 1.0000
9.000 1.0577 0.02066 0.01305 -0.0216 0.0197 1.0000
9.250 1.0679 0.02141 0.01384 -0.0192 0.0195 1.0000
9.500 1.0772 0.02230 0.01475 -0.0169 0.0192 1.0000
9.750 1.0849 0.02335 0.01584 -0.0146 0.0190 1.0000
10.000 1.0932 0.02445 0.01699 -0.0125 0.0188 1.0000
10.250 1.1034 0.02550 0.01809 -0.0108 0.0187 1.0000
10.500 1.1128 0.02666 0.01930 -0.0092 0.0185 1.0000
10.750 1.1218 0.02790 0.02060 -0.0077 0.0183 1.0000
11.000 1.1306 0.02920 0.02197 -0.0062 0.0181 1.0000
11.250 1.1392 0.03058 0.02340 -0.0049 0.0179 1.0000
11.500 1.1476 0.03201 0.02489 -0.0037 0.0176 1.0000
11.750 1.1559 0.03350 0.02643 -0.0026 0.0174 1.0000
12.000 1.1638 0.03507 0.02806 -0.0016 0.0172 1.0000
12.250 1.1708 0.03674 0.02979 -0.0007 0.0170 1.0000
12.500 1.1777 0.03848 0.03158 0.0002 0.0169 1.0000
12.750 1.1841 0.04030 0.03346 0.0010 0.0167 1.0000
13.000 1.1901 0.04218 0.03539 0.0017 0.0166 1.0000
13.250 1.1961 0.04411 0.03738 0.0023 0.0164 1.0000
13.500 1.2017 0.04611 0.03943 0.0029 0.0163 1.0000
13.750 1.2072 0.04817 0.04154 0.0034 0.0162 1.0000
14.000 1.2123 0.05030 0.04372 0.0038 0.0161 1.0000
14.250 1.2171 0.05249 0.04596 0.0042 0.0160 1.0000
14.500 1.2219 0.05469 0.04821 0.0046 0.0159 1.0000
14.750 1.2263 0.05693 0.05049 0.0051 0.0157 1.0000
15.000 1.2318 0.05915 0.05280 0.0053 0.0157 1.0000
15.250 1.2369 0.06145 0.05519 0.0055 0.0156 1.0000
15.500 1.2418 0.06381 0.05764 0.0056 0.0155 1.0000
15.750 1.2463 0.06623 0.06015 0.0057 0.0154 1.0000
16.000 1.2503 0.06875 0.06276 0.0057 0.0153 1.0000
16.250 1.2537 0.07134 0.06545 0.0056 0.0152 1.0000
16.500 1.2565 0.07405 0.06827 0.0055 0.0151 1.0000
16.750 1.2588 0.07688 0.07121 0.0053 0.0150 1.0000
17.000 1.2600 0.07990 0.07434 0.0049 0.0149 1.0000
17.250 1.2606 0.08305 0.07761 0.0044 0.0148 1.0000
17.500 1.2600 0.08642 0.08108 0.0037 0.0146 1.0000
17.750 1.2587 0.08994 0.08472 0.0029 0.0145 1.0000
18.000 1.2569 0.09361 0.08850 0.0019 0.0144 1.0000
18.250 1.2540 0.09749 0.09250 0.0007 0.0143 1.0000
18.500 1.2504 0.10152 0.09665 -0.0006 0.0142 1.0000
18.750 1.2457 0.10578 0.10103 -0.0021 0.0141 1.0000
19.000 1.2399 0.11030 0.10569 -0.0038 0.0140 1.0000
19.250 1.2331 0.11511 0.11062 -0.0058 0.0139 1.0000
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