NACA 23024 (naca23024-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 23024 (naca23024-il) Reynolds number: 500,000 Max Cl/Cd: 44.53 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca23024-il-500000.txt Download as CSV file: xf-naca23024-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 23024
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0645 0.07953 0.07408 -0.0660 1.0000 0.0831
-19.500 -1.0667 0.07672 0.07124 -0.0662 1.0000 0.0846
-19.250 -1.0701 0.07379 0.06831 -0.0664 1.0000 0.0861
-19.000 -1.0729 0.07091 0.06540 -0.0666 1.0000 0.0878
-18.750 -1.0728 0.06837 0.06281 -0.0666 1.0000 0.0896
-18.500 -1.0731 0.06586 0.06023 -0.0666 1.0000 0.0913
-18.250 -1.0798 0.06276 0.05713 -0.0665 1.0000 0.0932
-18.000 -1.0826 0.06009 0.05444 -0.0663 1.0000 0.0951
-17.750 -1.0838 0.05760 0.05191 -0.0659 1.0000 0.0973
-17.500 -1.0833 0.05537 0.04962 -0.0655 1.0000 0.0994
-17.250 -1.0902 0.05250 0.04675 -0.0649 1.0000 0.1017
-17.000 -1.0930 0.05006 0.04428 -0.0642 1.0000 0.1042
-16.750 -1.0910 0.04813 0.04229 -0.0634 1.0000 0.1068
-16.500 -1.0957 0.04567 0.03982 -0.0624 1.0000 0.1095
-16.250 -1.0992 0.04340 0.03754 -0.0613 1.0000 0.1125
-16.000 -1.0979 0.04163 0.03573 -0.0601 1.0000 0.1157
-15.750 -1.1014 0.03956 0.03364 -0.0586 1.0000 0.1185
-15.500 -1.1042 0.03763 0.03171 -0.0569 1.0000 0.1221
-15.250 -1.1027 0.03613 0.03018 -0.0551 1.0000 0.1259
-15.000 -1.1075 0.03430 0.02836 -0.0529 1.0000 0.1297
-14.750 -1.1092 0.03282 0.02687 -0.0506 1.0000 0.1337
-14.500 -1.1111 0.03146 0.02549 -0.0480 1.0000 0.1381
-14.250 -1.1162 0.03007 0.02411 -0.0450 1.0000 0.1422
-14.000 -1.1180 0.02902 0.02305 -0.0420 1.0000 0.1468
-13.750 -1.1252 0.02781 0.02184 -0.0383 1.0000 0.1513
-13.500 -1.0994 0.02674 0.02077 -0.0400 0.9977 0.1589
-13.250 -1.0776 0.02547 0.01954 -0.0413 0.9947 0.1666
-13.000 -1.0521 0.02452 0.01861 -0.0428 0.9921 0.1748
-12.750 -1.0289 0.02354 0.01764 -0.0436 0.9887 0.1831
-12.500 -1.0063 0.02254 0.01668 -0.0443 0.9849 0.1907
-12.250 -0.9776 0.02183 0.01596 -0.0456 0.9820 0.1988
-12.000 -0.9503 0.02097 0.01515 -0.0470 0.9796 0.2078
-11.750 -0.9223 0.02028 0.01447 -0.0481 0.9768 0.2156
-11.500 -0.9026 0.01950 0.01372 -0.0476 0.9706 0.2235
-11.250 -0.8729 0.01889 0.01310 -0.0488 0.9673 0.2308
-11.000 -0.8428 0.01822 0.01248 -0.0501 0.9649 0.2396
-10.750 -0.8214 0.01767 0.01191 -0.0494 0.9581 0.2461
-10.500 -0.7955 0.01702 0.01131 -0.0497 0.9533 0.2542
-10.250 -0.7623 0.01653 0.01080 -0.0511 0.9505 0.2616
-10.000 -0.7395 0.01590 0.01022 -0.0507 0.9445 0.2688
-9.750 -0.7140 0.01544 0.00975 -0.0505 0.9382 0.2761
-9.500 -0.6830 0.01486 0.00920 -0.0515 0.9341 0.2836
-9.250 -0.6474 0.01437 0.00871 -0.0534 0.9305 0.2916
-9.000 -0.6204 0.01400 0.00832 -0.0534 0.9210 0.2983
-8.750 -0.5809 0.01350 0.00787 -0.0560 0.9157 0.3070
-8.500 -0.5403 0.01320 0.00752 -0.0587 0.9083 0.3146
-8.250 -0.5026 0.01278 0.00714 -0.0611 0.8980 0.3232
-8.000 -0.4486 0.01249 0.00681 -0.0666 0.8905 0.3323
-7.750 -0.4175 0.01222 0.00655 -0.0675 0.8763 0.3403
-7.500 -0.3765 0.01198 0.00629 -0.0703 0.8646 0.3490
-7.250 -0.3479 0.01182 0.00607 -0.0706 0.8487 0.3564
-7.000 -0.3253 0.01162 0.00587 -0.0696 0.8321 0.3640
-6.750 -0.2988 0.01151 0.00567 -0.0694 0.8162 0.3715
-6.500 -0.2796 0.01138 0.00549 -0.0676 0.7994 0.3783
-6.250 -0.2637 0.01124 0.00534 -0.0652 0.7831 0.3856
-6.000 -0.2444 0.01119 0.00519 -0.0633 0.7672 0.3928
-5.750 -0.2279 0.01109 0.00505 -0.0610 0.7515 0.3996
-5.500 -0.2140 0.01099 0.00494 -0.0580 0.7371 0.4070
-5.250 -0.1969 0.01096 0.00482 -0.0557 0.7227 0.4141
-5.000 -0.1831 0.01088 0.00472 -0.0527 0.7086 0.4214
-4.750 -0.1691 0.01081 0.00464 -0.0498 0.6954 0.4292
-4.500 -0.1542 0.01079 0.00455 -0.0470 0.6821 0.4365
-4.250 -0.1405 0.01072 0.00447 -0.0440 0.6700 0.4439
-4.000 -0.1279 0.01067 0.00441 -0.0407 0.6569 0.4520
-3.750 -0.1131 0.01067 0.00435 -0.0378 0.6451 0.4596
-3.500 -0.1006 0.01060 0.00429 -0.0345 0.6331 0.4674
-3.250 -0.0885 0.01058 0.00424 -0.0311 0.6215 0.4758
-3.000 -0.0759 0.01059 0.00420 -0.0277 0.6095 0.4836
-2.750 -0.0649 0.01054 0.00416 -0.0241 0.5984 0.4921
-2.500 -0.0535 0.01053 0.00414 -0.0205 0.5869 0.5008
-2.250 -0.0421 0.01056 0.00411 -0.0169 0.5763 0.5090
-2.000 -0.0324 0.01051 0.00411 -0.0129 0.5657 0.5179
-1.750 -0.0234 0.01056 0.00409 -0.0088 0.5554 0.5265
-1.500 -0.0142 0.01053 0.00409 -0.0047 0.5467 0.5350
-1.250 -0.0115 0.01052 0.00409 0.0007 0.5367 0.5443
-1.000 -0.0032 0.01057 0.00408 0.0050 0.5281 0.5530
-0.750 0.0061 0.01051 0.00408 0.0090 0.5193 0.5628
-0.500 0.0158 0.01054 0.00408 0.0130 0.5102 0.5727
-0.250 0.0279 0.01053 0.00410 0.0164 0.5020 0.5826
0.000 0.0389 0.01053 0.00411 0.0201 0.4925 0.5934
0.250 0.0506 0.01059 0.00413 0.0236 0.4839 0.6035
0.500 0.0637 0.01056 0.00417 0.0268 0.4759 0.6146
1.000 0.0879 0.01064 0.00426 0.0336 0.4589 0.6374
1.250 0.1022 0.01067 0.00430 0.0365 0.4509 0.6486
1.500 0.1149 0.01071 0.00436 0.0397 0.4426 0.6609
1.750 0.1287 0.01077 0.00443 0.0427 0.4352 0.6733
2.000 0.1427 0.01079 0.00451 0.0456 0.4266 0.6864
2.500 0.1716 0.01091 0.00468 0.0513 0.4114 0.7135
2.750 0.1853 0.01098 0.00477 0.0542 0.4030 0.7271
3.000 0.1990 0.01109 0.00490 0.0571 0.3953 0.7422
3.250 0.2170 0.01113 0.00501 0.0591 0.3879 0.7568
3.500 0.2310 0.01124 0.00514 0.0619 0.3801 0.7729
3.750 0.2491 0.01135 0.00531 0.0638 0.3727 0.7893
4.000 0.2693 0.01146 0.00547 0.0653 0.3642 0.8058
4.250 0.2859 0.01165 0.00565 0.0674 0.3561 0.8223
4.500 0.3112 0.01176 0.00584 0.0678 0.3488 0.8388
4.750 0.3412 0.01197 0.00607 0.0670 0.3399 0.8535
5.000 0.3666 0.01218 0.00630 0.0672 0.3317 0.8694
5.250 0.4132 0.01246 0.00659 0.0629 0.3219 0.8807
5.500 0.4490 0.01276 0.00688 0.0608 0.3132 0.8932
5.750 0.4976 0.01311 0.00724 0.0561 0.3035 0.9012
6.000 0.5292 0.01350 0.00760 0.0549 0.2957 0.9127
6.250 0.5752 0.01392 0.00802 0.0507 0.2872 0.9175
6.500 0.6103 0.01450 0.00854 0.0486 0.2790 0.9240
6.750 0.6384 0.01486 0.00893 0.0482 0.2730 0.9323
7.000 0.6730 0.01544 0.00947 0.0462 0.2659 0.9356
7.250 0.7020 0.01602 0.01003 0.0454 0.2601 0.9404
7.500 0.7218 0.01648 0.01050 0.0465 0.2549 0.9489
7.750 0.7533 0.01712 0.01109 0.0450 0.2491 0.9515
8.000 0.7832 0.01773 0.01168 0.0437 0.2436 0.9550
8.250 0.8015 0.01824 0.01221 0.0449 0.2396 0.9637
8.500 0.8342 0.01886 0.01281 0.0430 0.2344 0.9657
8.750 0.8629 0.01960 0.01349 0.0416 0.2293 0.9684
9.000 0.8937 0.02007 0.01401 0.0402 0.2249 0.9721
9.250 0.9149 0.02076 0.01470 0.0404 0.2210 0.9784
9.500 0.9450 0.02147 0.01537 0.0385 0.2166 0.9802
9.750 0.9758 0.02211 0.01601 0.0366 0.2127 0.9824
10.000 1.0064 0.02267 0.01661 0.0349 0.2090 0.9853
10.250 1.0326 0.02342 0.01736 0.0337 0.2050 0.9890
10.500 1.0558 0.02436 0.01825 0.0327 0.2008 0.9922
10.750 1.0864 0.02496 0.01889 0.0306 0.1975 0.9946
11.000 1.1161 0.02562 0.01959 0.0287 0.1941 0.9973
11.250 1.1440 0.02644 0.02041 0.0268 0.1904 0.9996
11.500 1.1475 0.02735 0.02130 0.0290 0.1878 1.0000
11.750 1.1482 0.02815 0.02210 0.0320 0.1853 1.0000
12.000 1.1518 0.02890 0.02291 0.0345 0.1831 1.0000
12.250 1.1564 0.02971 0.02376 0.0368 0.1808 1.0000
12.500 1.1591 0.03073 0.02478 0.0390 0.1781 1.0000
12.750 1.1617 0.03184 0.02589 0.0412 0.1757 1.0000
13.000 1.1638 0.03307 0.02710 0.0432 0.1730 1.0000
13.250 1.1709 0.03407 0.02817 0.0447 0.1710 1.0000
13.500 1.1769 0.03521 0.02936 0.0461 0.1687 1.0000
13.750 1.1819 0.03647 0.03063 0.0475 0.1662 1.0000
14.000 1.1846 0.03794 0.03210 0.0489 0.1637 1.0000
14.250 1.1875 0.03942 0.03356 0.0503 0.1611 1.0000
14.500 1.1936 0.04081 0.03503 0.0512 0.1591 1.0000
14.750 1.1990 0.04226 0.03654 0.0521 0.1567 1.0000
15.000 1.2025 0.04392 0.03822 0.0529 0.1542 1.0000
15.250 1.2048 0.04568 0.03997 0.0538 0.1520 1.0000
15.500 1.2070 0.04746 0.04175 0.0546 0.1496 1.0000
15.750 1.2118 0.04918 0.04356 0.0551 0.1476 1.0000
16.000 1.2148 0.05108 0.04551 0.0555 0.1452 1.0000
16.250 1.2170 0.05307 0.04753 0.0559 0.1430 1.0000
16.500 1.2176 0.05521 0.04966 0.0563 0.1408 1.0000
16.750 1.2193 0.05728 0.05175 0.0566 0.1385 1.0000
17.000 1.2212 0.05949 0.05405 0.0567 0.1364 1.0000
17.250 1.2225 0.06175 0.05637 0.0567 0.1342 1.0000
17.500 1.2220 0.06420 0.05884 0.0567 0.1320 1.0000
17.750 1.2228 0.06644 0.06105 0.0567 0.1299 1.0000
18.000 1.2222 0.06902 0.06370 0.0565 0.1279 1.0000
18.250 1.2226 0.07153 0.06629 0.0563 0.1260 1.0000
18.500 1.2204 0.07436 0.06918 0.0558 0.1238 1.0000
18.750 1.2201 0.07691 0.07173 0.0555 0.1219 1.0000
19.000 1.2203 0.07935 0.07414 0.0553 0.1198 1.0000
19.250 1.2174 0.08239 0.07729 0.0546 0.1180 1.0000
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