AVISTAR (avistar-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AVISTAR (avistar-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.61 at α=3.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-avistar-il-1000000.txt Download as CSV file: xf-avistar-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.750 -0.5908 0.07348 0.07153 -0.0543 1.0000 0.0238
-11.500 -0.5998 0.06825 0.06630 -0.0588 1.0000 0.0236
-11.250 -0.6239 0.06103 0.05899 -0.0653 1.0000 0.0234
-11.000 -0.6497 0.05544 0.05328 -0.0689 1.0000 0.0232
-10.750 -0.6785 0.05095 0.04864 -0.0690 1.0000 0.0230
-10.500 -0.7102 0.04634 0.04381 -0.0664 0.9925 0.0229
-10.250 -0.7480 0.03735 0.03418 -0.0638 0.9527 0.0228
-10.000 -0.7829 0.02919 0.02509 -0.0571 0.9207 0.0236
-9.750 -0.7812 0.02617 0.02155 -0.0538 0.9044 0.0240
-9.500 -0.7686 0.02412 0.01929 -0.0521 0.8926 0.0243
-9.250 -0.7481 0.02345 0.01854 -0.0512 0.8833 0.0245
-9.000 -0.7273 0.02284 0.01783 -0.0503 0.8743 0.0247
-8.750 -0.7051 0.02234 0.01727 -0.0496 0.8666 0.0250
-8.500 -0.6828 0.02177 0.01662 -0.0489 0.8590 0.0252
-8.250 -0.6604 0.02118 0.01593 -0.0481 0.8527 0.0255
-8.000 -0.6378 0.02028 0.01493 -0.0475 0.8478 0.0259
-7.750 -0.6151 0.01932 0.01383 -0.0467 0.8423 0.0263
-7.500 -0.5920 0.01840 0.01276 -0.0460 0.8368 0.0267
-7.250 -0.5680 0.01762 0.01184 -0.0454 0.8318 0.0271
-7.000 -0.5429 0.01718 0.01130 -0.0449 0.8270 0.0275
-6.750 -0.5191 0.01605 0.01006 -0.0444 0.8221 0.0280
-6.500 -0.4946 0.01529 0.00925 -0.0440 0.8173 0.0283
-6.250 -0.4691 0.01486 0.00880 -0.0436 0.8128 0.0287
-6.000 -0.4432 0.01443 0.00836 -0.0433 0.8082 0.0290
-5.750 -0.4175 0.01405 0.00794 -0.0430 0.8031 0.0294
-5.500 -0.3918 0.01367 0.00751 -0.0426 0.7978 0.0299
-5.250 -0.3659 0.01326 0.00707 -0.0422 0.7930 0.0304
-5.000 -0.3399 0.01288 0.00665 -0.0419 0.7880 0.0309
-4.750 -0.3135 0.01262 0.00635 -0.0416 0.7828 0.0314
-4.500 -0.2871 0.01240 0.00606 -0.0413 0.7774 0.0317
-4.250 -0.2635 0.01166 0.00533 -0.0405 0.7726 0.0323
-4.000 -0.2387 0.01124 0.00491 -0.0399 0.7669 0.0328
-3.750 -0.2130 0.01097 0.00462 -0.0395 0.7610 0.0333
-3.500 -0.1868 0.01073 0.00437 -0.0391 0.7551 0.0340
-3.250 -0.1606 0.01048 0.00411 -0.0388 0.7483 0.0346
-3.000 -0.1345 0.01027 0.00386 -0.0384 0.7413 0.0353
-2.750 -0.1078 0.01007 0.00365 -0.0381 0.7345 0.0360
-2.500 -0.0805 0.00997 0.00352 -0.0379 0.7266 0.0365
-2.250 -0.0566 0.00955 0.00307 -0.0371 0.7189 0.0376
-2.000 -0.0302 0.00936 0.00287 -0.0368 0.7098 0.0385
-1.750 -0.0036 0.00922 0.00270 -0.0364 0.7005 0.0395
-1.500 0.0231 0.00910 0.00255 -0.0361 0.6895 0.0406
-1.250 0.0501 0.00900 0.00242 -0.0359 0.6777 0.0416
-1.000 0.0758 0.00884 0.00221 -0.0354 0.6645 0.0432
-0.750 0.1021 0.00876 0.00209 -0.0350 0.6489 0.0451
-0.500 0.1285 0.00873 0.00199 -0.0347 0.6313 0.0470
-0.250 0.1545 0.00868 0.00188 -0.0342 0.6125 0.0495
0.000 0.1805 0.00866 0.00181 -0.0338 0.5951 0.0531
0.250 0.2066 0.00864 0.00174 -0.0334 0.5794 0.0596
0.500 0.2195 0.00745 0.00154 -0.0308 0.5671 0.3829
0.750 0.2361 0.00677 0.00151 -0.0286 0.5558 0.5832
1.000 0.2570 0.00656 0.00157 -0.0271 0.5447 0.6836
1.250 0.2812 0.00647 0.00160 -0.0262 0.5358 0.7291
1.500 0.3057 0.00645 0.00164 -0.0254 0.5267 0.7635
1.750 0.3303 0.00635 0.00168 -0.0246 0.5195 0.8043
2.000 0.3545 0.00626 0.00177 -0.0236 0.5118 0.8645
2.250 0.3837 0.00625 0.00182 -0.0238 0.5029 0.9047
2.500 0.4319 0.00632 0.00189 -0.0285 0.4903 0.9311
2.750 0.5004 0.00642 0.00198 -0.0380 0.4763 0.9434
3.000 0.5589 0.00659 0.00212 -0.0450 0.4639 0.9521
3.250 0.6027 0.00679 0.00226 -0.0486 0.4497 0.9580
3.500 0.6415 0.00700 0.00241 -0.0511 0.4343 0.9632
3.750 0.6768 0.00723 0.00255 -0.0528 0.4113 0.9699
4.000 0.7008 0.00767 0.00279 -0.0522 0.3689 0.9891
4.250 0.7271 0.00880 0.00333 -0.0527 0.2582 0.9952
4.500 0.7489 0.01105 0.00452 -0.0532 0.0423 0.9986
4.750 0.7843 0.01141 0.00482 -0.0551 0.0335 1.0000
5.000 0.8047 0.01170 0.00508 -0.0538 0.0306 1.0000
5.250 0.8266 0.01193 0.00531 -0.0527 0.0292 1.0000
5.500 0.8485 0.01220 0.00556 -0.0516 0.0278 1.0000
5.750 0.8691 0.01258 0.00594 -0.0503 0.0263 1.0000
6.000 0.8913 0.01285 0.00622 -0.0493 0.0256 1.0000
6.250 0.9130 0.01315 0.00652 -0.0482 0.0249 1.0000
6.500 0.9344 0.01348 0.00684 -0.0471 0.0242 1.0000
6.750 0.9551 0.01383 0.00720 -0.0458 0.0236 1.0000
7.000 0.9744 0.01427 0.00765 -0.0444 0.0230 1.0000
7.250 0.9901 0.01493 0.00834 -0.0423 0.0224 1.0000
7.500 1.0097 0.01531 0.00874 -0.0409 0.0222 1.0000
7.750 1.0285 0.01573 0.00919 -0.0394 0.0219 1.0000
8.000 1.0463 0.01620 0.00967 -0.0377 0.0216 1.0000
8.250 1.0632 0.01671 0.01020 -0.0359 0.0213 1.0000
8.500 1.0788 0.01725 0.01077 -0.0339 0.0210 1.0000
8.750 1.0919 0.01777 0.01131 -0.0315 0.0206 1.0000
9.000 1.1015 0.01829 0.01186 -0.0284 0.0203 1.0000
9.250 1.1116 0.01888 0.01247 -0.0256 0.0200 1.0000
9.500 1.1216 0.01958 0.01319 -0.0230 0.0198 1.0000
9.750 1.1305 0.02042 0.01407 -0.0205 0.0195 1.0000
10.000 1.1374 0.02147 0.01515 -0.0180 0.0193 1.0000
10.250 1.1396 0.02292 0.01665 -0.0151 0.0191 1.0000
10.500 1.1418 0.02451 0.01829 -0.0125 0.0189 1.0000
10.750 1.1537 0.02551 0.01934 -0.0111 0.0188 1.0000
11.000 1.1645 0.02662 0.02049 -0.0096 0.0187 1.0000
11.250 1.1750 0.02781 0.02173 -0.0082 0.0186 1.0000
11.500 1.1850 0.02907 0.02303 -0.0069 0.0184 1.0000
11.750 1.1947 0.03038 0.02438 -0.0056 0.0183 1.0000
12.000 1.2040 0.03175 0.02581 -0.0044 0.0182 1.0000
12.250 1.2132 0.03318 0.02728 -0.0032 0.0180 1.0000
12.500 1.2224 0.03461 0.02876 -0.0021 0.0179 1.0000
12.750 1.2315 0.03608 0.03028 -0.0010 0.0178 1.0000
13.000 1.2408 0.03757 0.03182 0.0001 0.0177 1.0000
13.250 1.2501 0.03908 0.03338 0.0010 0.0175 1.0000
13.500 1.2593 0.04060 0.03495 0.0020 0.0174 1.0000
13.750 1.2684 0.04215 0.03655 0.0029 0.0173 1.0000
14.000 1.2772 0.04375 0.03820 0.0036 0.0171 1.0000
14.250 1.2854 0.04542 0.03991 0.0042 0.0169 1.0000
14.500 1.2934 0.04712 0.04166 0.0048 0.0168 1.0000
14.750 1.3003 0.04898 0.04357 0.0053 0.0166 1.0000
15.000 1.3073 0.05086 0.04550 0.0057 0.0165 1.0000
15.250 1.3141 0.05280 0.04749 0.0062 0.0164 1.0000
15.500 1.3206 0.05478 0.04952 0.0066 0.0163 1.0000
15.750 1.3270 0.05677 0.05157 0.0071 0.0162 1.0000
16.000 1.3339 0.05874 0.05359 0.0077 0.0161 1.0000
16.250 1.3422 0.06060 0.05550 0.0087 0.0159 1.0000
16.500 1.3506 0.06286 0.05789 0.0106 0.0157 1.0000
16.750 1.3472 0.06596 0.06112 0.0103 0.0157 1.0000
17.000 1.3444 0.06916 0.06445 0.0100 0.0157 1.0000
17.250 1.3411 0.07255 0.06796 0.0096 0.0156 1.0000
17.500 1.3369 0.07614 0.07169 0.0090 0.0156 1.0000
17.750 1.3308 0.08005 0.07574 0.0083 0.0155 1.0000
18.000 1.3233 0.08429 0.08011 0.0073 0.0155 1.0000
18.250 1.3138 0.08891 0.08489 0.0061 0.0155 1.0000
18.500 1.3025 0.09393 0.09006 0.0045 0.0154 1.0000
18.750 1.2891 0.09938 0.09566 0.0026 0.0154 1.0000
19.000 1.2740 0.10528 0.10173 0.0003 0.0154 1.0000
19.250 1.2570 0.11169 0.10830 -0.0025 0.0154 1.0000
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