DAVIS BASIC B-24 WING AIRFOIL (davis-corrected-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: DAVIS BASIC B-24 WING AIRFOIL (davis-corrected-il) Reynolds number: 1,000,000 Max Cl/Cd: 122.32 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-davis-corrected-il-1000000.txt Download as CSV file: xf-davis-corrected-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: DAVIS BASIC B-24 WING 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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0618 0.09629 0.09319 -0.0302 1.0000 0.0179
-18.750 -1.0829 0.08923 0.08603 -0.0341 1.0000 0.0180
-18.500 -1.1058 0.08201 0.07870 -0.0381 1.0000 0.0181
-18.250 -1.1260 0.07537 0.07194 -0.0417 1.0000 0.0180
-18.000 -1.1463 0.06876 0.06521 -0.0454 1.0000 0.0182
-17.750 -1.1635 0.06274 0.05907 -0.0487 1.0000 0.0182
-17.500 -1.1770 0.05730 0.05352 -0.0518 1.0000 0.0184
-17.250 -1.1890 0.05222 0.04832 -0.0546 1.0000 0.0185
-17.000 -1.1962 0.04789 0.04387 -0.0570 1.0000 0.0187
-16.750 -1.2016 0.04396 0.03983 -0.0590 1.0000 0.0188
-16.500 -1.2031 0.04067 0.03644 -0.0605 1.0000 0.0190
-16.250 -1.2030 0.03774 0.03341 -0.0616 1.0000 0.0192
-16.000 -1.2013 0.03516 0.03072 -0.0623 1.0000 0.0193
-15.750 -1.1952 0.03319 0.02866 -0.0626 1.0000 0.0195
-15.500 -1.2008 0.03034 0.02571 -0.0626 1.0000 0.0198
-15.250 -1.2013 0.02821 0.02350 -0.0620 1.0000 0.0201
-15.000 -1.1971 0.02662 0.02186 -0.0610 1.0000 0.0204
-14.750 -1.1900 0.02537 0.02056 -0.0598 1.0000 0.0207
-14.500 -1.1802 0.02438 0.01952 -0.0585 1.0000 0.0211
-14.250 -1.1708 0.02344 0.01852 -0.0569 1.0000 0.0215
-14.000 -1.1603 0.02262 0.01765 -0.0552 1.0000 0.0219
-13.750 -1.1494 0.02188 0.01685 -0.0534 1.0000 0.0222
-13.500 -1.1379 0.02121 0.01612 -0.0514 1.0000 0.0225
-13.250 -1.1246 0.02067 0.01552 -0.0494 1.0000 0.0228
-13.000 -1.1224 0.01972 0.01452 -0.0459 1.0000 0.0233
-12.750 -1.1156 0.01907 0.01384 -0.0426 1.0000 0.0238
-12.500 -1.1052 0.01858 0.01333 -0.0398 1.0000 0.0243
-12.250 -1.0908 0.01811 0.01283 -0.0376 1.0000 0.0248
-12.000 -1.0753 0.01766 0.01235 -0.0356 1.0000 0.0254
-11.750 -1.0584 0.01728 0.01194 -0.0337 1.0000 0.0260
-11.500 -1.0411 0.01692 0.01153 -0.0319 1.0000 0.0264
-11.250 -1.0288 0.01628 0.01087 -0.0293 1.0000 0.0274
-11.000 -1.0030 0.01574 0.01034 -0.0293 0.9896 0.0283
-10.750 -0.9600 0.01522 0.00979 -0.0328 0.9742 0.0294
-10.500 -0.9044 0.01468 0.00918 -0.0388 0.9495 0.0306
-10.250 -0.8678 0.01407 0.00846 -0.0410 0.8995 0.0322
-10.000 -0.8478 0.01389 0.00811 -0.0394 0.8551 0.0333
-9.750 -0.8271 0.01372 0.00780 -0.0380 0.8230 0.0344
-9.500 -0.8068 0.01346 0.00741 -0.0365 0.7970 0.0356
-9.250 -0.7861 0.01315 0.00703 -0.0352 0.7754 0.0372
-9.000 -0.7634 0.01294 0.00673 -0.0341 0.7561 0.0387
-8.750 -0.7398 0.01277 0.00646 -0.0332 0.7384 0.0400
-8.250 -0.6939 0.01221 0.00582 -0.0313 0.7082 0.0444
-8.000 -0.6699 0.01199 0.00553 -0.0305 0.6948 0.0466
-7.750 -0.6463 0.01173 0.00524 -0.0297 0.6818 0.0494
-7.500 -0.6212 0.01157 0.00502 -0.0290 0.6694 0.0517
-7.250 -0.5971 0.01130 0.00474 -0.0283 0.6587 0.0554
-6.750 -0.5472 0.01090 0.00428 -0.0270 0.6375 0.0632
-6.500 -0.5216 0.01076 0.00409 -0.0265 0.6274 0.0670
-6.250 -0.4966 0.01051 0.00386 -0.0258 0.6185 0.0732
-6.000 -0.4712 0.01035 0.00367 -0.0253 0.6095 0.0792
-5.750 -0.4452 0.01017 0.00349 -0.0248 0.6011 0.0857
-5.500 -0.4200 0.00999 0.00331 -0.0242 0.5921 0.0946
-5.250 -0.3940 0.00979 0.00314 -0.0238 0.5846 0.1041
-5.000 -0.3682 0.00964 0.00299 -0.0233 0.5767 0.1146
-4.750 -0.3422 0.00946 0.00284 -0.0228 0.5696 0.1268
-4.500 -0.3162 0.00929 0.00270 -0.0224 0.5621 0.1407
-4.250 -0.2904 0.00914 0.00257 -0.0219 0.5548 0.1564
-4.000 -0.2643 0.00895 0.00245 -0.0215 0.5483 0.1740
-3.750 -0.2384 0.00879 0.00233 -0.0210 0.5416 0.1940
-3.500 -0.2123 0.00864 0.00223 -0.0206 0.5355 0.2157
-3.250 -0.1861 0.00846 0.00213 -0.0202 0.5292 0.2396
-3.000 -0.1603 0.00832 0.00204 -0.0197 0.5225 0.2664
-2.750 -0.1342 0.00815 0.00196 -0.0193 0.5169 0.2938
-2.500 -0.1079 0.00800 0.00189 -0.0189 0.5113 0.3234
-2.250 -0.0822 0.00785 0.00183 -0.0184 0.5054 0.3553
-2.000 -0.0561 0.00771 0.00177 -0.0180 0.5001 0.3877
-1.750 -0.0300 0.00755 0.00172 -0.0175 0.4946 0.4219
-1.500 -0.0041 0.00744 0.00168 -0.0171 0.4890 0.4555
-1.250 0.0218 0.00733 0.00166 -0.0166 0.4838 0.4898
-1.000 0.0481 0.00720 0.00163 -0.0161 0.4793 0.5248
-0.750 0.0740 0.00709 0.00162 -0.0156 0.4741 0.5599
-0.500 0.0995 0.00702 0.00161 -0.0151 0.4686 0.5940
-0.250 0.1255 0.00692 0.00162 -0.0145 0.4643 0.6270
0.000 0.1513 0.00683 0.00162 -0.0140 0.4597 0.6603
0.250 0.1771 0.00677 0.00164 -0.0134 0.4550 0.6914
0.500 0.2024 0.00675 0.00167 -0.0127 0.4499 0.7214
0.750 0.2286 0.00667 0.00169 -0.0122 0.4463 0.7498
1.000 0.2547 0.00663 0.00172 -0.0117 0.4416 0.7776
1.250 0.2806 0.00663 0.00177 -0.0111 0.4369 0.8026
1.500 0.3064 0.00664 0.00183 -0.0105 0.4324 0.8270
1.750 0.3335 0.00662 0.00188 -0.0101 0.4290 0.8491
2.000 0.3605 0.00663 0.00194 -0.0097 0.4247 0.8697
2.250 0.3877 0.00668 0.00201 -0.0094 0.4201 0.8883
2.500 0.4155 0.00675 0.00210 -0.0092 0.4155 0.9052
2.750 0.4452 0.00679 0.00218 -0.0095 0.4122 0.9194
3.000 0.4756 0.00686 0.00226 -0.0098 0.4082 0.9318
3.250 0.5049 0.00696 0.00235 -0.0100 0.4039 0.9434
3.500 0.5389 0.00711 0.00248 -0.0113 0.3990 0.9509
3.750 0.5707 0.00719 0.00257 -0.0120 0.3957 0.9588
4.000 0.6070 0.00730 0.00269 -0.0137 0.3918 0.9630
4.250 0.6389 0.00744 0.00280 -0.0145 0.3876 0.9690
4.500 0.6742 0.00762 0.00294 -0.0161 0.3825 0.9719
4.750 0.7125 0.00772 0.00306 -0.0183 0.3793 0.9736
5.000 0.7493 0.00783 0.00318 -0.0202 0.3755 0.9758
5.250 0.7840 0.00797 0.00331 -0.0217 0.3713 0.9788
5.500 0.8149 0.00818 0.00347 -0.0224 0.3663 0.9828
5.750 0.8528 0.00825 0.00358 -0.0245 0.3633 0.9841
6.000 0.8898 0.00835 0.00369 -0.0265 0.3589 0.9857
6.250 0.9249 0.00853 0.00381 -0.0282 0.3505 0.9878
6.500 0.9601 0.00860 0.00390 -0.0298 0.3421 0.9901
6.750 0.9925 0.00880 0.00405 -0.0310 0.3334 0.9928
7.000 1.0283 0.00889 0.00415 -0.0328 0.3273 0.9943
7.250 1.0637 0.00905 0.00429 -0.0346 0.3195 0.9960
7.500 1.0990 0.00916 0.00441 -0.0363 0.3131 0.9978
7.750 1.1335 0.00934 0.00457 -0.0380 0.3047 0.9994
8.000 1.1608 0.00949 0.00472 -0.0381 0.2974 1.0000
8.250 1.1801 0.00969 0.00490 -0.0366 0.2891 1.0000
8.500 1.1998 0.00987 0.00508 -0.0352 0.2806 1.0000
8.750 1.2178 0.01014 0.00531 -0.0335 0.2702 1.0000
9.000 1.2350 0.01044 0.00556 -0.0317 0.2568 1.0000
9.250 1.2510 0.01080 0.00586 -0.0297 0.2414 1.0000
9.500 1.2650 0.01125 0.00622 -0.0273 0.2210 1.0000
9.750 1.2743 0.01189 0.00672 -0.0243 0.1950 1.0000
10.000 1.2792 0.01271 0.00736 -0.0206 0.1645 1.0000
10.250 1.2801 0.01364 0.00811 -0.0163 0.1349 1.0000
10.500 1.2825 0.01447 0.00882 -0.0123 0.1153 1.0000
10.750 1.2819 0.01516 0.00944 -0.0076 0.1016 1.0000
11.000 1.2811 0.01588 0.01012 -0.0032 0.0904 1.0000
11.250 1.2833 0.01672 0.01092 0.0002 0.0810 1.0000
11.500 1.2868 0.01768 0.01186 0.0030 0.0732 1.0000
11.750 1.2931 0.01866 0.01285 0.0051 0.0671 1.0000
12.000 1.2982 0.01987 0.01406 0.0069 0.0615 1.0000
12.250 1.3023 0.02133 0.01552 0.0083 0.0564 1.0000
12.500 1.3096 0.02271 0.01694 0.0093 0.0528 1.0000
12.750 1.3129 0.02453 0.01876 0.0101 0.0491 1.0000
13.000 1.3198 0.02616 0.02044 0.0107 0.0465 1.0000
13.250 1.3227 0.02822 0.02253 0.0111 0.0439 1.0000
13.500 1.3261 0.03031 0.02466 0.0114 0.0417 1.0000
13.750 1.3297 0.03242 0.02682 0.0117 0.0399 1.0000
14.000 1.3298 0.03490 0.02934 0.0118 0.0381 1.0000
14.250 1.3291 0.03751 0.03200 0.0119 0.0366 1.0000
14.500 1.3311 0.03986 0.03442 0.0120 0.0354 1.0000
14.750 1.3300 0.04256 0.03716 0.0120 0.0341 1.0000
15.000 1.3265 0.04554 0.04019 0.0119 0.0330 1.0000
15.250 1.3215 0.04878 0.04349 0.0116 0.0319 1.0000
15.500 1.3221 0.05150 0.04628 0.0114 0.0311 1.0000
15.750 1.3213 0.05441 0.04925 0.0110 0.0302 1.0000
16.000 1.3181 0.05763 0.05252 0.0105 0.0293 1.0000
16.250 1.3143 0.06097 0.05591 0.0100 0.0285 1.0000
16.500 1.3070 0.06480 0.05980 0.0093 0.0277 1.0000
16.750 1.3067 0.06782 0.06289 0.0087 0.0271 1.0000
17.000 1.3064 0.07087 0.06600 0.0081 0.0264 1.0000
17.250 1.3035 0.07429 0.06948 0.0074 0.0258 1.0000
17.500 1.3006 0.07771 0.07294 0.0066 0.0251 1.0000
17.750 1.2948 0.08154 0.07682 0.0057 0.0245 1.0000
18.000 1.2856 0.08590 0.08125 0.0046 0.0238 1.0000
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