NACA 23024 (naca23024-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 23024 (naca23024-il) Reynolds number: 200,000 Max Cl/Cd: 41.34 at α=9.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca23024-il-200000.txt Download as CSV file: xf-naca23024-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0718 0.07630 0.06929 -0.0759 1.0000 0.1090
-19.500 -1.0636 0.07480 0.06785 -0.0755 1.0000 0.1112
-19.250 -1.0632 0.07237 0.06536 -0.0756 1.0000 0.1134
-19.000 -1.0689 0.06927 0.06212 -0.0758 1.0000 0.1156
-18.750 -1.0633 0.06755 0.06041 -0.0753 1.0000 0.1180
-18.500 -1.0565 0.06598 0.05890 -0.0748 1.0000 0.1206
-18.250 -1.0556 0.06375 0.05663 -0.0745 1.0000 0.1232
-18.000 -1.0624 0.06076 0.05347 -0.0744 1.0000 0.1259
-17.750 -1.0511 0.05976 0.05260 -0.0735 1.0000 0.1289
-17.500 -1.0484 0.05787 0.05071 -0.0729 1.0000 0.1319
-17.250 -1.0515 0.05544 0.04818 -0.0723 1.0000 0.1354
-17.000 -1.0462 0.05389 0.04669 -0.0714 1.0000 0.1388
-16.750 -1.0440 0.05211 0.04493 -0.0705 1.0000 0.1422
-16.500 -1.0461 0.04997 0.04270 -0.0695 1.0000 0.1461
-16.250 -1.0431 0.04836 0.04115 -0.0683 1.0000 0.1502
-16.000 -1.0429 0.04659 0.03940 -0.0670 1.0000 0.1543
-15.750 -1.0460 0.04460 0.03729 -0.0656 1.0000 0.1588
-15.500 -1.0431 0.04319 0.03601 -0.0640 1.0000 0.1633
-15.250 -1.0451 0.04149 0.03428 -0.0622 1.0000 0.1683
-15.000 -1.0459 0.03994 0.03270 -0.0603 1.0000 0.1732
-14.750 -1.0470 0.03851 0.03133 -0.0581 1.0000 0.1782
-14.500 -1.0506 0.03702 0.02975 -0.0557 1.0000 0.1838
-14.250 -1.0513 0.03579 0.02862 -0.0532 1.0000 0.1889
-14.000 -1.0553 0.03454 0.02736 -0.0502 1.0000 0.1945
-13.750 -1.0589 0.03340 0.02620 -0.0471 1.0000 0.2002
-13.500 -1.0632 0.03239 0.02525 -0.0437 1.0000 0.2054
-13.250 -1.0703 0.03141 0.02420 -0.0398 1.0000 0.2113
-13.000 -1.0749 0.03058 0.02343 -0.0359 1.0000 0.2166
-12.750 -1.0821 0.02982 0.02269 -0.0317 1.0000 0.2220
-12.500 -1.0919 0.02911 0.02188 -0.0269 1.0000 0.2277
-12.250 -1.0970 0.02850 0.02137 -0.0226 1.0000 0.2327
-12.000 -1.1056 0.02795 0.02082 -0.0178 1.0000 0.2379
-11.750 -1.1057 0.02742 0.02018 -0.0145 0.9987 0.2445
-11.500 -1.0759 0.02689 0.01975 -0.0162 0.9934 0.2532
-11.250 -1.0501 0.02633 0.01911 -0.0171 0.9872 0.2622
-11.000 -1.0217 0.02585 0.01871 -0.0183 0.9813 0.2708
-10.750 -0.9958 0.02539 0.01816 -0.0190 0.9752 0.2795
-10.500 -0.9688 0.02492 0.01776 -0.0195 0.9682 0.2877
-10.250 -0.9380 0.02453 0.01727 -0.0209 0.9639 0.2970
-10.000 -0.9169 0.02403 0.01688 -0.0201 0.9544 0.3043
-9.750 -0.8867 0.02364 0.01639 -0.0210 0.9495 0.3133
-9.500 -0.8643 0.02318 0.01602 -0.0203 0.9405 0.3206
-9.250 -0.8346 0.02277 0.01559 -0.0208 0.9347 0.3294
-9.000 -0.7957 0.02226 0.01509 -0.0231 0.9316 0.3384
-8.750 -0.7834 0.02196 0.01482 -0.0202 0.9197 0.3454
-8.500 -0.7538 0.02151 0.01424 -0.0205 0.9149 0.3541
-8.250 -0.7074 0.02090 0.01379 -0.0239 0.9129 0.3636
-8.000 -0.7008 0.02069 0.01352 -0.0197 0.8996 0.3705
-7.750 -0.6609 0.02008 0.01295 -0.0218 0.8960 0.3795
-7.500 -0.6191 0.01953 0.01242 -0.0243 0.8931 0.3891
-7.250 -0.6112 0.01932 0.01212 -0.0202 0.8805 0.3962
-7.000 -0.5640 0.01876 0.01169 -0.0237 0.8757 0.4056
-6.750 -0.5207 0.01824 0.01108 -0.0266 0.8711 0.4157
-6.500 -0.4563 0.01758 0.01054 -0.0336 0.8680 0.4262
-6.250 -0.4532 0.01749 0.01041 -0.0284 0.8523 0.4333
-6.000 -0.4017 0.01695 0.00987 -0.0329 0.8459 0.4433
-5.750 -0.3844 0.01681 0.00975 -0.0305 0.8325 0.4512
-5.500 -0.3565 0.01654 0.00934 -0.0303 0.8221 0.4606
-5.250 -0.3256 0.01627 0.00920 -0.0306 0.8096 0.4690
-5.000 -0.2973 0.01606 0.00891 -0.0304 0.7983 0.4787
-4.750 -0.2800 0.01591 0.00875 -0.0280 0.7847 0.4870
-4.500 -0.2457 0.01571 0.00854 -0.0289 0.7737 0.4965
-4.250 -0.2414 0.01569 0.00844 -0.0239 0.7596 0.5051
-4.000 -0.2001 0.01546 0.00823 -0.0263 0.7486 0.5148
-3.750 -0.1936 0.01545 0.00821 -0.0217 0.7347 0.5235
-3.500 -0.1626 0.01531 0.00799 -0.0221 0.7237 0.5336
-3.250 -0.1518 0.01528 0.00803 -0.0183 0.7101 0.5421
-3.000 -0.1310 0.01525 0.00782 -0.0166 0.6993 0.5526
-2.750 -0.1131 0.01517 0.00788 -0.0143 0.6862 0.5614
-2.500 -0.0897 0.01515 0.00775 -0.0131 0.6752 0.5721
-2.250 -0.0782 0.01510 0.00776 -0.0095 0.6626 0.5813
-2.000 -0.0526 0.01509 0.00769 -0.0087 0.6516 0.5918
-1.750 -0.0457 0.01508 0.00767 -0.0042 0.6399 0.6021
-1.500 -0.0179 0.01504 0.00765 -0.0038 0.6285 0.6123
-1.250 -0.0099 0.01506 0.00763 0.0004 0.6175 0.6233
-1.000 0.0157 0.01502 0.00763 0.0012 0.6060 0.6334
-0.750 0.0296 0.01505 0.00763 0.0043 0.5956 0.6450
-0.500 0.0483 0.01503 0.00764 0.0064 0.5846 0.6556
-0.250 0.0689 0.01509 0.00765 0.0082 0.5746 0.6675
0.000 0.0818 0.01506 0.00768 0.0115 0.5639 0.6786
0.250 0.1093 0.01516 0.00770 0.0119 0.5540 0.6907
0.500 0.1177 0.01514 0.00776 0.0160 0.5441 0.7026
0.750 0.1405 0.01521 0.00783 0.0173 0.5343 0.7146
1.000 0.1570 0.01526 0.00789 0.0198 0.5249 0.7272
1.250 0.1751 0.01532 0.00800 0.0221 0.5148 0.7394
1.500 0.1998 0.01544 0.00806 0.0230 0.5055 0.7520
1.750 0.2130 0.01550 0.00821 0.0262 0.4957 0.7648
2.000 0.2405 0.01566 0.00831 0.0265 0.4862 0.7771
2.250 0.2532 0.01576 0.00848 0.0298 0.4772 0.7908
2.500 0.2804 0.01593 0.00867 0.0301 0.4672 0.8023
2.750 0.2972 0.01610 0.00879 0.0325 0.4588 0.8165
3.000 0.3270 0.01634 0.00911 0.0323 0.4481 0.8268
3.250 0.3521 0.01659 0.00924 0.0330 0.4393 0.8401
3.500 0.3828 0.01691 0.00966 0.0325 0.4287 0.8496
3.750 0.4283 0.01740 0.01002 0.0291 0.4180 0.8580
4.000 0.4425 0.01760 0.01031 0.0319 0.4091 0.8706
4.250 0.4988 0.01822 0.01080 0.0262 0.3975 0.8745
4.500 0.5328 0.01868 0.01132 0.0249 0.3871 0.8816
4.750 0.5526 0.01898 0.01155 0.0265 0.3788 0.8927
5.000 0.5972 0.01963 0.01220 0.0232 0.3682 0.8956
5.250 0.6368 0.02022 0.01272 0.0209 0.3587 0.8994
5.500 0.6637 0.02073 0.01321 0.0210 0.3503 0.9073
5.750 0.6879 0.02114 0.01363 0.0215 0.3420 0.9148
6.000 0.7304 0.02179 0.01416 0.0185 0.3333 0.9178
6.250 0.7587 0.02227 0.01469 0.0181 0.3253 0.9245
6.500 0.7830 0.02270 0.01504 0.0185 0.3186 0.9331
6.750 0.8206 0.02327 0.01562 0.0161 0.3109 0.9369
7.000 0.8466 0.02372 0.01608 0.0160 0.3042 0.9449
7.250 0.8823 0.02427 0.01646 0.0141 0.2975 0.9504
7.500 0.9121 0.02472 0.01702 0.0129 0.2910 0.9558
7.750 0.9347 0.02518 0.01749 0.0132 0.2854 0.9645
8.000 0.9778 0.02569 0.01785 0.0097 0.2789 0.9675
8.250 1.0028 0.02614 0.01843 0.0092 0.2735 0.9747
8.500 1.0323 0.02655 0.01884 0.0079 0.2677 0.9805
8.750 1.0756 0.02703 0.01915 0.0043 0.2622 0.9841
9.000 1.0984 0.02757 0.01984 0.0039 0.2575 0.9912
9.250 1.1308 0.02788 0.02018 0.0017 0.2520 0.9960
9.500 1.1692 0.02828 0.02047 -0.0012 0.2470 1.0000
9.750 1.1700 0.02872 0.02093 0.0025 0.2439 1.0000
10.000 1.1613 0.02917 0.02147 0.0075 0.2411 1.0000
10.250 1.1571 0.02964 0.02198 0.0119 0.2381 1.0000
10.500 1.1570 0.03008 0.02243 0.0156 0.2352 1.0000
10.750 1.1612 0.03052 0.02281 0.0187 0.2322 1.0000
11.000 1.1732 0.03106 0.02328 0.0206 0.2288 1.0000
11.250 1.1637 0.03178 0.02411 0.0254 0.2263 1.0000
11.500 1.1591 0.03250 0.02491 0.0293 0.2233 1.0000
11.750 1.1606 0.03317 0.02559 0.0324 0.2204 1.0000
12.000 1.1680 0.03375 0.02613 0.0347 0.2175 1.0000
12.250 1.1884 0.03427 0.02652 0.0354 0.2140 1.0000
12.500 1.1775 0.03543 0.02784 0.0395 0.2117 1.0000
12.750 1.1735 0.03654 0.02905 0.0426 0.2089 1.0000
13.000 1.1756 0.03750 0.03004 0.0450 0.2059 1.0000
13.250 1.1844 0.03825 0.03076 0.0467 0.2032 1.0000
13.500 1.2107 0.03860 0.03095 0.0468 0.1998 1.0000
13.750 1.1951 0.04039 0.03293 0.0502 0.1976 1.0000
14.000 1.1883 0.04201 0.03468 0.0526 0.1950 1.0000
14.250 1.1886 0.04338 0.03611 0.0544 0.1922 1.0000
14.500 1.1977 0.04428 0.03698 0.0556 0.1895 1.0000
14.750 1.2235 0.04451 0.03705 0.0558 0.1866 1.0000
15.000 1.2089 0.04686 0.03960 0.0580 0.1844 1.0000
15.250 1.1952 0.04938 0.04227 0.0597 0.1818 1.0000
15.500 1.1915 0.05136 0.04433 0.0609 0.1792 1.0000
15.750 1.1991 0.05254 0.04550 0.0616 0.1767 1.0000
16.000 1.2241 0.05257 0.04539 0.0620 0.1740 1.0000
16.250 1.2095 0.05558 0.04857 0.0630 0.1718 1.0000
16.500 1.1860 0.05949 0.05269 0.0638 0.1693 1.0000
16.750 1.1760 0.06247 0.05577 0.0642 0.1669 1.0000
17.000 1.1831 0.06391 0.05721 0.0645 0.1645 1.0000
17.250 1.2140 0.06318 0.05631 0.0649 0.1620 1.0000
17.500 1.1926 0.06747 0.06078 0.0650 0.1599 1.0000
17.750 1.1467 0.07456 0.06816 0.0640 0.1574 1.0000
18.000 1.1199 0.08007 0.07384 0.0630 0.1549 1.0000
18.250 1.1351 0.08075 0.07447 0.0631 0.1526 1.0000
18.500 1.1809 0.07796 0.07146 0.0643 0.1506 1.0000
18.750 1.1037 0.08971 0.08362 0.0611 0.1480 1.0000
19.000 0.5502 0.19082 0.18576 0.0216 0.1209 1.0000
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