NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 63(2)-215 MOD B (n63215b-il) Reynolds number: 1,000,000 Max Cl/Cd: 86.28 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-n63215b-il-1000000.txt Download as CSV file: xf-n63215b-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(2)-215 MOD B
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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0885 0.10678 0.10342 -0.0223 1.0000 0.0114
-19.500 -1.1019 0.10042 0.09696 -0.0259 1.0000 0.0115
-19.250 -1.1157 0.09425 0.09068 -0.0292 1.0000 0.0115
-19.000 -1.1343 0.08746 0.08376 -0.0329 1.0000 0.0115
-18.750 -1.1452 0.08209 0.07830 -0.0356 1.0000 0.0116
-18.500 -1.1568 0.07674 0.07284 -0.0383 1.0000 0.0117
-18.250 -1.1679 0.07163 0.06762 -0.0407 1.0000 0.0116
-18.000 -1.1789 0.06672 0.06261 -0.0429 1.0000 0.0118
-17.750 -1.1833 0.06281 0.05862 -0.0446 1.0000 0.0119
-17.500 -1.1908 0.05862 0.05434 -0.0463 1.0000 0.0119
-17.250 -1.1955 0.05489 0.05053 -0.0477 1.0000 0.0122
-17.000 -1.1971 0.05167 0.04722 -0.0487 1.0000 0.0122
-16.750 -1.1966 0.04878 0.04427 -0.0496 1.0000 0.0123
-16.500 -1.1948 0.04612 0.04155 -0.0503 1.0000 0.0125
-16.250 -1.1921 0.04364 0.03901 -0.0508 1.0000 0.0126
-16.000 -1.1861 0.04161 0.03694 -0.0511 1.0000 0.0128
-15.750 -1.1839 0.03924 0.03449 -0.0514 1.0000 0.0129
-15.500 -1.1792 0.03718 0.03236 -0.0515 1.0000 0.0130
-15.250 -1.1697 0.03562 0.03077 -0.0514 1.0000 0.0133
-15.000 -1.1645 0.03369 0.02877 -0.0513 1.0000 0.0134
-14.750 -1.1563 0.03209 0.02712 -0.0511 1.0000 0.0136
-14.500 -1.1446 0.03083 0.02581 -0.0508 1.0000 0.0139
-14.250 -1.1370 0.02924 0.02415 -0.0504 1.0000 0.0141
-14.000 -1.1289 0.02777 0.02262 -0.0499 1.0000 0.0141
-13.750 -1.1197 0.02641 0.02121 -0.0492 1.0000 0.0143
-13.500 -1.1150 0.02478 0.01954 -0.0484 1.0000 0.0148
-13.250 -1.1054 0.02356 0.01829 -0.0475 1.0000 0.0151
-13.000 -1.0945 0.02250 0.01721 -0.0465 1.0000 0.0154
-12.750 -1.0816 0.02163 0.01631 -0.0455 1.0000 0.0158
-12.500 -1.0688 0.02080 0.01545 -0.0444 1.0000 0.0162
-12.250 -1.0553 0.02007 0.01469 -0.0433 1.0000 0.0166
-12.000 -1.0429 0.01934 0.01392 -0.0418 1.0000 0.0170
-11.750 -1.0313 0.01867 0.01322 -0.0401 1.0000 0.0173
-11.500 -1.0244 0.01796 0.01248 -0.0376 1.0000 0.0177
-11.250 -1.0152 0.01729 0.01181 -0.0352 1.0000 0.0185
-11.000 -0.9978 0.01686 0.01138 -0.0338 1.0000 0.0192
-10.750 -0.9617 0.01641 0.01093 -0.0360 0.9801 0.0202
-10.500 -0.9216 0.01604 0.01052 -0.0388 0.9614 0.0211
-10.250 -0.8967 0.01537 0.00978 -0.0390 0.9345 0.0222
-10.000 -0.8768 0.01506 0.00940 -0.0378 0.9150 0.0230
-9.750 -0.8548 0.01485 0.00915 -0.0368 0.9004 0.0240
-9.500 -0.8337 0.01453 0.00876 -0.0357 0.8875 0.0246
-9.250 -0.8106 0.01429 0.00846 -0.0349 0.8759 0.0253
-9.000 -0.7895 0.01385 0.00796 -0.0339 0.8652 0.0261
-8.750 -0.7673 0.01347 0.00755 -0.0331 0.8555 0.0273
-8.500 -0.7432 0.01318 0.00723 -0.0325 0.8463 0.0281
-8.250 -0.7186 0.01292 0.00693 -0.0319 0.8383 0.0290
-8.000 -0.6932 0.01267 0.00664 -0.0315 0.8304 0.0298
-7.750 -0.6676 0.01247 0.00638 -0.0310 0.8233 0.0304
-7.500 -0.6436 0.01201 0.00590 -0.0305 0.8160 0.0318
-7.250 -0.6182 0.01173 0.00559 -0.0301 0.8091 0.0331
-7.000 -0.5916 0.01149 0.00534 -0.0298 0.8025 0.0345
-6.750 -0.5649 0.01128 0.00509 -0.0296 0.7956 0.0357
-6.500 -0.5388 0.01098 0.00476 -0.0292 0.7891 0.0376
-6.250 -0.5121 0.01069 0.00447 -0.0290 0.7821 0.0400
-6.000 -0.4852 0.01049 0.00423 -0.0288 0.7755 0.0423
-5.750 -0.4581 0.01018 0.00395 -0.0286 0.7694 0.0479
-5.500 -0.4313 0.00988 0.00369 -0.0284 0.7622 0.0593
-5.250 -0.4050 0.00949 0.00341 -0.0282 0.7539 0.0834
-5.000 -0.3788 0.00907 0.00313 -0.0280 0.7446 0.1182
-4.750 -0.3522 0.00863 0.00286 -0.0279 0.7362 0.1592
-4.500 -0.3261 0.00809 0.00257 -0.0279 0.7281 0.2198
-4.250 -0.2995 0.00753 0.00228 -0.0279 0.7206 0.2907
-4.000 -0.2723 0.00706 0.00207 -0.0280 0.7142 0.3599
-3.750 -0.2441 0.00680 0.00194 -0.0280 0.7080 0.4030
-3.500 -0.2151 0.00663 0.00186 -0.0282 0.7006 0.4330
-3.250 -0.1861 0.00654 0.00178 -0.0282 0.6935 0.4550
-3.000 -0.1567 0.00646 0.00174 -0.0284 0.6864 0.4746
-2.750 -0.1275 0.00641 0.00168 -0.0284 0.6777 0.4909
-2.500 -0.0980 0.00635 0.00164 -0.0285 0.6682 0.5039
-2.250 -0.0688 0.00632 0.00161 -0.0286 0.6591 0.5179
-2.000 -0.0392 0.00627 0.00159 -0.0287 0.6505 0.5321
-1.750 -0.0098 0.00629 0.00156 -0.0288 0.6409 0.5429
-1.500 0.0195 0.00628 0.00155 -0.0289 0.6300 0.5548
-1.250 0.0489 0.00627 0.00155 -0.0290 0.6196 0.5653
-1.000 0.0784 0.00631 0.00154 -0.0291 0.6081 0.5736
-0.750 0.1076 0.00632 0.00153 -0.0292 0.5941 0.5805
-0.500 0.1368 0.00636 0.00152 -0.0293 0.5774 0.5875
-0.250 0.1657 0.00643 0.00152 -0.0293 0.5534 0.5937
0.000 0.1936 0.00661 0.00155 -0.0292 0.5058 0.5998
0.250 0.2170 0.00738 0.00174 -0.0287 0.3615 0.6059
0.500 0.2448 0.00762 0.00186 -0.0286 0.3325 0.6118
0.750 0.2732 0.00778 0.00195 -0.0287 0.3103 0.6185
1.250 0.3301 0.00807 0.00211 -0.0288 0.2738 0.6312
1.500 0.3587 0.00821 0.00219 -0.0288 0.2594 0.6375
1.750 0.3873 0.00834 0.00227 -0.0289 0.2465 0.6433
2.000 0.4156 0.00847 0.00236 -0.0289 0.2346 0.6494
2.250 0.4441 0.00862 0.00246 -0.0289 0.2234 0.6557
2.500 0.4726 0.00873 0.00256 -0.0290 0.2148 0.6619
2.750 0.5007 0.00888 0.00268 -0.0290 0.2056 0.6688
3.000 0.5293 0.00899 0.00278 -0.0290 0.1991 0.6754
3.250 0.5572 0.00915 0.00291 -0.0290 0.1903 0.6819
3.500 0.5856 0.00927 0.00302 -0.0290 0.1841 0.6885
3.750 0.6136 0.00942 0.00315 -0.0290 0.1770 0.6948
4.000 0.6415 0.00957 0.00329 -0.0290 0.1710 0.7019
4.250 0.6696 0.00971 0.00342 -0.0290 0.1659 0.7089
4.500 0.6970 0.00990 0.00359 -0.0289 0.1593 0.7160
4.750 0.7249 0.01004 0.00374 -0.0288 0.1550 0.7228
5.000 0.7525 0.01019 0.00389 -0.0288 0.1503 0.7292
5.250 0.7796 0.01039 0.00408 -0.0286 0.1451 0.7360
5.500 0.8069 0.01057 0.00426 -0.0285 0.1414 0.7424
5.750 0.8344 0.01071 0.00443 -0.0285 0.1384 0.7491
6.000 0.8616 0.01090 0.00461 -0.0283 0.1346 0.7559
6.250 0.8879 0.01112 0.00483 -0.0281 0.1300 0.7628
6.500 0.9146 0.01133 0.00506 -0.0279 0.1267 0.7705
6.750 0.9416 0.01147 0.00524 -0.0278 0.1243 0.7778
7.000 0.9680 0.01167 0.00544 -0.0275 0.1208 0.7857
7.250 0.9935 0.01193 0.00569 -0.0272 0.1159 0.7933
7.500 1.0193 0.01215 0.00593 -0.0269 0.1122 0.8012
7.750 1.0456 0.01233 0.00613 -0.0267 0.1092 0.8088
8.000 1.0709 0.01256 0.00637 -0.0263 0.1059 0.8168
8.250 1.0951 0.01288 0.00667 -0.0258 0.1009 0.8250
8.500 1.1201 0.01310 0.00694 -0.0254 0.0987 0.8339
8.750 1.1449 0.01331 0.00719 -0.0250 0.0970 0.8431
9.000 1.1691 0.01355 0.00747 -0.0244 0.0949 0.8536
9.250 1.1922 0.01382 0.00776 -0.0237 0.0927 0.8646
9.500 1.2143 0.01413 0.00809 -0.0229 0.0897 0.8769
9.750 1.2348 0.01448 0.00849 -0.0217 0.0868 0.8912
10.000 1.2559 0.01468 0.00877 -0.0206 0.0860 0.9084
10.500 1.2930 0.01506 0.00932 -0.0174 0.0830 1.0000
10.750 1.3150 0.01544 0.00969 -0.0168 0.0813 1.0000
11.000 1.3352 0.01585 0.01009 -0.0159 0.0793 1.0000
11.250 1.3516 0.01633 0.01056 -0.0144 0.0768 1.0000
11.500 1.3672 0.01682 0.01106 -0.0127 0.0749 1.0000
11.750 1.3856 0.01717 0.01145 -0.0116 0.0743 1.0000
12.000 1.4035 0.01756 0.01189 -0.0104 0.0735 1.0000
12.250 1.4207 0.01801 0.01236 -0.0091 0.0724 1.0000
12.500 1.4371 0.01851 0.01289 -0.0079 0.0710 1.0000
12.750 1.4528 0.01907 0.01345 -0.0067 0.0693 1.0000
13.000 1.4673 0.01971 0.01411 -0.0055 0.0678 1.0000
13.250 1.4808 0.02044 0.01486 -0.0042 0.0664 1.0000
13.500 1.4922 0.02132 0.01577 -0.0028 0.0646 1.0000
13.750 1.5083 0.02194 0.01642 -0.0019 0.0634 1.0000
14.000 1.5233 0.02264 0.01716 -0.0010 0.0626 1.0000
14.250 1.5373 0.02342 0.01799 0.0000 0.0616 1.0000
14.500 1.5508 0.02426 0.01884 0.0009 0.0599 1.0000
14.750 1.5627 0.02524 0.01983 0.0018 0.0584 1.0000
15.000 1.5731 0.02635 0.02095 0.0027 0.0564 1.0000
15.250 1.5834 0.02750 0.02215 0.0036 0.0560 1.0000
15.500 1.5944 0.02862 0.02329 0.0043 0.0533 1.0000
15.750 1.6044 0.02985 0.02458 0.0050 0.0529 1.0000
16.000 1.6140 0.03114 0.02591 0.0056 0.0516 1.0000
16.250 1.6217 0.03263 0.02743 0.0062 0.0500 1.0000
16.500 1.6286 0.03422 0.02907 0.0067 0.0493 1.0000
16.750 1.6320 0.03617 0.03103 0.0071 0.0470 1.0000
17.000 1.6382 0.03794 0.03287 0.0074 0.0469 1.0000
17.250 1.6399 0.04018 0.03517 0.0076 0.0456 1.0000
17.500 1.6476 0.04189 0.03696 0.0076 0.0448 1.0000
17.750 1.6518 0.04404 0.03918 0.0075 0.0444 1.0000
18.000 1.6549 0.04638 0.04161 0.0072 0.0436 1.0000
18.250 1.6558 0.04904 0.04433 0.0068 0.0425 1.0000
18.500 1.6510 0.05246 0.04779 0.0060 0.0403 1.0000
18.750 1.6413 0.05667 0.05205 0.0047 0.0378 1.0000
19.000 1.6377 0.06027 0.05575 0.0035 0.0374 1.0000
19.250 1.6291 0.06469 0.06026 0.0017 0.0357 1.0000
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