NACA 0010-34 a=0.8 c(li)=0.2 (naca001034a08cli02-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0010-34 a=0.8 c(li)=0.2 (naca001034a08cli02-il) Reynolds number: 1,000,000 Max Cl/Cd: 93.58 at α=2.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca001034a08cli02-il-1000000.txt Download as CSV file: xf-naca001034a08cli02-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0010-34 a=0.8 c(li)=0.2
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
------ -------- --------- --------- -------- -------- --------
-9.500 -0.5151 0.08454 0.08297 -0.0388 1.0000 0.0076
-9.250 -0.5209 0.07915 0.07760 -0.0422 1.0000 0.0076
-9.000 -0.5366 0.07293 0.07142 -0.0473 1.0000 0.0074
-8.750 -0.4733 0.05542 0.05397 -0.0523 0.9984 0.0084
-8.500 -0.4919 0.04899 0.04743 -0.0577 0.9955 0.0081
-8.250 -0.4981 0.04337 0.04167 -0.0600 0.9916 0.0082
-8.000 -0.4939 0.03818 0.03632 -0.0614 0.9883 0.0085
-7.750 -0.4791 0.03430 0.03226 -0.0625 0.9863 0.0088
-7.500 -0.4664 0.02973 0.02746 -0.0635 0.9846 0.0089
-7.250 -0.4523 0.02528 0.02277 -0.0643 0.9831 0.0090
-7.000 -0.4422 0.02161 0.01885 -0.0632 0.9784 0.0090
-6.750 -0.4282 0.01815 0.01511 -0.0625 0.9746 0.0090
-6.500 -0.4121 0.01493 0.01158 -0.0617 0.9715 0.0090
-6.250 -0.3964 0.01225 0.00860 -0.0604 0.9678 0.0091
-6.000 -0.4112 0.01780 0.01323 -0.0572 0.9692 0.0070
-5.750 -0.3900 0.01579 0.01096 -0.0556 0.9649 0.0074
-5.500 -0.3648 0.01464 0.00965 -0.0550 0.9615 0.0080
-5.250 -0.3389 0.01360 0.00849 -0.0546 0.9587 0.0084
-5.000 -0.3132 0.01270 0.00749 -0.0542 0.9560 0.0086
-4.500 -0.2680 0.01079 0.00538 -0.0522 0.9477 0.0096
-4.250 -0.2461 0.00980 0.00429 -0.0510 0.9441 0.0102
-4.000 -0.2219 0.00927 0.00369 -0.0503 0.9404 0.0115
-3.750 -0.1967 0.00894 0.00332 -0.0498 0.9362 0.0131
-3.500 -0.1709 0.00863 0.00295 -0.0495 0.9323 0.0144
-3.250 -0.1448 0.00831 0.00254 -0.0491 0.9289 0.0167
-3.000 -0.1192 0.00800 0.00219 -0.0487 0.9244 0.0232
-2.750 -0.0968 0.00722 0.00184 -0.0479 0.9195 0.1474
-2.500 -0.0768 0.00620 0.00156 -0.0469 0.9151 0.3671
-2.250 -0.0549 0.00557 0.00143 -0.0461 0.9097 0.5101
-2.000 -0.0320 0.00510 0.00132 -0.0452 0.9046 0.6243
-1.750 -0.0078 0.00483 0.00128 -0.0445 0.8997 0.7030
-1.500 0.0165 0.00463 0.00126 -0.0437 0.8939 0.7639
-1.250 0.0431 0.00454 0.00121 -0.0434 0.8891 0.7908
-1.000 0.0700 0.00448 0.00118 -0.0432 0.8836 0.8076
-0.750 0.0970 0.00442 0.00114 -0.0431 0.8780 0.8237
-0.500 0.1241 0.00437 0.00111 -0.0429 0.8727 0.8418
-0.250 0.1508 0.00431 0.00110 -0.0427 0.8662 0.8603
0.000 0.1778 0.00428 0.00109 -0.0425 0.8603 0.8776
0.250 0.2046 0.00425 0.00111 -0.0422 0.8530 0.8944
0.500 0.2316 0.00425 0.00112 -0.0420 0.8461 0.9103
0.750 0.2586 0.00425 0.00115 -0.0418 0.8374 0.9248
1.000 0.2859 0.00428 0.00118 -0.0417 0.8282 0.9372
1.250 0.3137 0.00432 0.00122 -0.0416 0.8171 0.9477
1.500 0.3414 0.00438 0.00126 -0.0416 0.8049 0.9573
1.750 0.3704 0.00445 0.00131 -0.0418 0.7928 0.9651
2.000 0.4007 0.00453 0.00137 -0.0424 0.7790 0.9713
2.250 0.4324 0.00467 0.00145 -0.0434 0.7497 0.9763
2.500 0.4604 0.00492 0.00153 -0.0434 0.7021 0.9825
2.750 0.4938 0.00533 0.00165 -0.0450 0.6272 0.9847
3.000 0.5249 0.00592 0.00183 -0.0462 0.5288 0.9876
3.250 0.5538 0.00664 0.00210 -0.0470 0.4144 0.9911
3.500 0.5792 0.00774 0.00249 -0.0474 0.2498 0.9946
3.750 0.6052 0.00922 0.00308 -0.0482 0.0484 0.9968
4.000 0.6383 0.00971 0.00346 -0.0497 0.0205 0.9987
4.250 0.6685 0.01024 0.00407 -0.0504 0.0147 1.0000
4.500 0.6891 0.01046 0.00433 -0.0491 0.0137 1.0000
4.750 0.7088 0.01079 0.00469 -0.0476 0.0123 1.0000
5.000 0.7281 0.01114 0.00508 -0.0460 0.0108 1.0000
5.250 0.7395 0.01221 0.00627 -0.0427 0.0089 1.0000
5.500 0.7572 0.01272 0.00683 -0.0408 0.0085 1.0000
5.750 0.7756 0.01320 0.00736 -0.0390 0.0081 1.0000
6.000 0.7935 0.01377 0.00801 -0.0371 0.0077 1.0000
6.250 0.8118 0.01438 0.00867 -0.0353 0.0071 1.0000
6.500 0.8307 0.01498 0.00932 -0.0336 0.0065 1.0000
6.750 0.8496 0.01565 0.01004 -0.0321 0.0060 1.0000
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Polar data table (+)
Polar graphs
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