NACA 63(3)-018 (naca633018-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(3)-018 (naca633018-il) Reynolds number: 1,000,000 Max Cl/Cd: 65.4 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca633018-il-1000000-n5.txt Download as CSV file: xf-naca633018-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(3)-018
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2926 0.08680 0.08241 -0.0137 1.0000 0.0091
-19.500 -1.2972 0.08270 0.07824 -0.0154 1.0000 0.0094
-19.250 -1.3010 0.07879 0.07425 -0.0170 1.0000 0.0099
-19.000 -1.3034 0.07516 0.07056 -0.0183 1.0000 0.0105
-18.500 -1.3065 0.06834 0.06362 -0.0206 1.0000 0.0118
-18.250 -1.3084 0.06499 0.06022 -0.0216 1.0000 0.0131
-18.000 -1.3074 0.06207 0.05725 -0.0224 1.0000 0.0141
-17.750 -1.3071 0.05914 0.05427 -0.0231 1.0000 0.0151
-17.500 -1.3051 0.05643 0.05152 -0.0237 1.0000 0.0163
-17.250 -1.3010 0.05401 0.04905 -0.0242 1.0000 0.0171
-17.000 -1.2987 0.05146 0.04649 -0.0246 1.0000 0.0191
-16.750 -1.2939 0.04921 0.04419 -0.0249 1.0000 0.0203
-16.500 -1.2878 0.04713 0.04207 -0.0251 1.0000 0.0210
-16.250 -1.2816 0.04509 0.03998 -0.0253 1.0000 0.0213
-16.000 -1.2760 0.04305 0.03793 -0.0254 1.0000 0.0229
-15.750 -1.2683 0.04125 0.03610 -0.0254 1.0000 0.0238
-15.500 -1.2602 0.03952 0.03431 -0.0254 1.0000 0.0245
-15.250 -1.2515 0.03787 0.03261 -0.0253 1.0000 0.0250
-15.000 -1.2438 0.03618 0.03089 -0.0251 1.0000 0.0258
-14.750 -1.2357 0.03459 0.02927 -0.0248 1.0000 0.0266
-14.500 -1.2271 0.03307 0.02773 -0.0245 1.0000 0.0275
-14.250 -1.2175 0.03167 0.02630 -0.0242 1.0000 0.0283
-14.000 -1.2071 0.03035 0.02494 -0.0238 1.0000 0.0290
-13.500 -1.1717 0.02784 0.02232 -0.0256 0.9473 0.0301
-13.250 -1.1524 0.02671 0.02101 -0.0266 0.8914 0.0311
-13.000 -1.1449 0.02562 0.01981 -0.0253 0.8638 0.0321
-12.750 -1.1357 0.02458 0.01868 -0.0242 0.8459 0.0330
-12.500 -1.1249 0.02363 0.01766 -0.0231 0.8306 0.0339
-12.250 -1.1134 0.02272 0.01668 -0.0221 0.8184 0.0347
-12.000 -1.1013 0.02187 0.01575 -0.0210 0.8077 0.0353
-11.750 -1.0879 0.02110 0.01491 -0.0200 0.7972 0.0360
-11.500 -1.0757 0.02028 0.01403 -0.0189 0.7878 0.0368
-11.250 -1.0648 0.01943 0.01312 -0.0175 0.7783 0.0379
-11.000 -1.0529 0.01865 0.01231 -0.0162 0.7702 0.0391
-10.750 -1.0405 0.01796 0.01156 -0.0148 0.7616 0.0401
-10.500 -1.0272 0.01732 0.01087 -0.0134 0.7540 0.0410
-10.250 -1.0135 0.01676 0.01026 -0.0120 0.7459 0.0422
-10.000 -0.9995 0.01624 0.00968 -0.0104 0.7390 0.0429
-9.750 -0.9861 0.01575 0.00914 -0.0087 0.7315 0.0437
-9.500 -0.9754 0.01525 0.00860 -0.0064 0.7248 0.0453
-9.250 -0.9632 0.01486 0.00818 -0.0041 0.7178 0.0468
-9.000 -0.9457 0.01451 0.00780 -0.0027 0.7113 0.0484
-8.750 -0.9257 0.01418 0.00744 -0.0018 0.7054 0.0502
-8.500 -0.9044 0.01389 0.00711 -0.0010 0.6987 0.0517
-8.250 -0.8835 0.01354 0.00675 -0.0001 0.6928 0.0551
-8.000 -0.8615 0.01322 0.00642 0.0006 0.6869 0.0588
-7.750 -0.8387 0.01292 0.00610 0.0012 0.6807 0.0632
-7.500 -0.8161 0.01258 0.00578 0.0017 0.6751 0.0704
-7.250 -0.7933 0.01221 0.00544 0.0023 0.6692 0.0801
-7.000 -0.7701 0.01186 0.00512 0.0028 0.6637 0.0918
-6.750 -0.7466 0.01150 0.00482 0.0032 0.6587 0.1061
-6.500 -0.7224 0.01115 0.00452 0.0036 0.6531 0.1220
-6.250 -0.6981 0.01081 0.00423 0.0039 0.6471 0.1392
-6.000 -0.6737 0.01043 0.00394 0.0042 0.6422 0.1599
-5.750 -0.6492 0.01003 0.00365 0.0044 0.6372 0.1858
-5.500 -0.6252 0.00958 0.00334 0.0048 0.6320 0.2192
-5.250 -0.6003 0.00918 0.00306 0.0050 0.6270 0.2518
-5.000 -0.5747 0.00881 0.00281 0.0051 0.6219 0.2824
-4.750 -0.5487 0.00847 0.00258 0.0051 0.6164 0.3137
-4.250 -0.4951 0.00792 0.00223 0.0051 0.6074 0.3725
-4.000 -0.4677 0.00769 0.00210 0.0050 0.6024 0.4006
-3.750 -0.4399 0.00751 0.00199 0.0048 0.5972 0.4244
-3.500 -0.4114 0.00740 0.00191 0.0046 0.5926 0.4413
-3.250 -0.3822 0.00734 0.00185 0.0043 0.5881 0.4506
-3.000 -0.3533 0.00726 0.00179 0.0040 0.5834 0.4608
-2.750 -0.3244 0.00720 0.00173 0.0038 0.5787 0.4720
-2.500 -0.2949 0.00716 0.00169 0.0034 0.5743 0.4801
-2.250 -0.2656 0.00712 0.00164 0.0031 0.5694 0.4855
-2.000 -0.2362 0.00709 0.00160 0.0028 0.5649 0.4910
-1.750 -0.2067 0.00708 0.00157 0.0024 0.5608 0.4963
-1.500 -0.1772 0.00704 0.00154 0.0021 0.5563 0.5016
-1.250 -0.1478 0.00702 0.00152 0.0018 0.5514 0.5072
-1.000 -0.1182 0.00703 0.00150 0.0014 0.5471 0.5119
-0.750 -0.0887 0.00701 0.00148 0.0010 0.5432 0.5163
-0.500 -0.0591 0.00698 0.00147 0.0007 0.5386 0.5210
-0.250 -0.0296 0.00699 0.00146 0.0004 0.5340 0.5257
0.000 0.0000 0.00701 0.00146 0.0000 0.5297 0.5297
0.250 0.0296 0.00699 0.00146 -0.0004 0.5257 0.5340
0.500 0.0591 0.00698 0.00147 -0.0007 0.5210 0.5387
0.750 0.0887 0.00701 0.00148 -0.0011 0.5163 0.5432
1.000 0.1182 0.00703 0.00150 -0.0014 0.5120 0.5471
1.250 0.1478 0.00702 0.00152 -0.0018 0.5072 0.5514
1.500 0.1772 0.00704 0.00154 -0.0021 0.5016 0.5563
1.750 0.2067 0.00708 0.00157 -0.0024 0.4963 0.5608
2.000 0.2362 0.00709 0.00160 -0.0028 0.4910 0.5649
2.250 0.2656 0.00712 0.00164 -0.0031 0.4855 0.5694
2.500 0.2949 0.00716 0.00169 -0.0034 0.4802 0.5743
2.750 0.3244 0.00720 0.00173 -0.0038 0.4719 0.5787
3.000 0.3533 0.00726 0.00179 -0.0040 0.4608 0.5834
3.250 0.3822 0.00734 0.00185 -0.0043 0.4506 0.5881
3.500 0.4114 0.00740 0.00191 -0.0046 0.4416 0.5926
3.750 0.4399 0.00751 0.00199 -0.0048 0.4245 0.5972
4.000 0.4677 0.00769 0.00210 -0.0050 0.4008 0.6024
4.250 0.4952 0.00791 0.00223 -0.0051 0.3729 0.6074
4.750 0.5487 0.00847 0.00258 -0.0051 0.3136 0.6165
5.000 0.5747 0.00881 0.00281 -0.0051 0.2824 0.6219
5.250 0.6004 0.00918 0.00306 -0.0050 0.2519 0.6270
5.500 0.6251 0.00959 0.00334 -0.0047 0.2184 0.6320
5.750 0.6493 0.01003 0.00365 -0.0045 0.1862 0.6372
6.000 0.6737 0.01043 0.00394 -0.0042 0.1600 0.6422
6.250 0.6981 0.01080 0.00423 -0.0039 0.1394 0.6472
6.500 0.7225 0.01115 0.00452 -0.0036 0.1220 0.6531
6.750 0.7466 0.01150 0.00482 -0.0032 0.1058 0.6587
7.000 0.7702 0.01186 0.00513 -0.0028 0.0917 0.6637
7.250 0.7934 0.01221 0.00544 -0.0023 0.0800 0.6692
7.500 0.8162 0.01258 0.00578 -0.0018 0.0704 0.6750
7.750 0.8387 0.01292 0.00610 -0.0012 0.0632 0.6807
8.000 0.8615 0.01322 0.00642 -0.0006 0.0588 0.6869
8.250 0.8837 0.01354 0.00675 0.0001 0.0552 0.6927
8.500 0.9044 0.01389 0.00711 0.0009 0.0517 0.6987
8.750 0.9258 0.01418 0.00744 0.0018 0.0501 0.7054
9.000 0.9459 0.01451 0.00779 0.0027 0.0485 0.7114
9.250 0.9634 0.01486 0.00818 0.0041 0.0468 0.7179
9.500 0.9755 0.01525 0.00860 0.0064 0.0453 0.7248
9.750 0.9863 0.01575 0.00914 0.0087 0.0436 0.7316
10.000 0.9998 0.01623 0.00968 0.0104 0.0429 0.7391
10.250 1.0139 0.01674 0.01024 0.0119 0.0420 0.7458
10.500 1.0276 0.01731 0.01087 0.0134 0.0412 0.7536
11.000 1.0534 0.01864 0.01229 0.0161 0.0391 0.7702
11.250 1.0651 0.01943 0.01311 0.0175 0.0378 0.7784
11.500 1.0762 0.02027 0.01401 0.0188 0.0367 0.7877
11.750 1.0884 0.02109 0.01489 0.0200 0.0360 0.7971
12.000 1.1017 0.02186 0.01574 0.0210 0.0354 0.8077
12.250 1.1142 0.02268 0.01664 0.0220 0.0346 0.8185
12.500 1.1257 0.02359 0.01762 0.0230 0.0340 0.8309
12.750 1.1364 0.02456 0.01865 0.0241 0.0328 0.8456
13.000 1.1458 0.02558 0.01977 0.0252 0.0321 0.8640
13.500 1.1721 0.02786 0.02234 0.0255 0.0302 0.9476
14.500 1.2285 0.03301 0.02766 0.0244 0.0275 1.0000
14.750 1.2371 0.03453 0.02921 0.0247 0.0265 1.0000
15.000 1.2451 0.03613 0.03084 0.0250 0.0257 1.0000
15.250 1.2530 0.03779 0.03254 0.0251 0.0251 1.0000
15.500 1.2619 0.03943 0.03422 0.0252 0.0243 1.0000
15.750 1.2701 0.04115 0.03599 0.0252 0.0235 1.0000
16.000 1.2776 0.04296 0.03784 0.0252 0.0228 1.0000
16.250 1.2838 0.04495 0.03985 0.0251 0.0217 1.0000
16.500 1.2893 0.04705 0.04198 0.0249 0.0207 1.0000
16.750 1.2954 0.04913 0.04410 0.0247 0.0197 1.0000
17.000 1.3006 0.05134 0.04637 0.0244 0.0190 1.0000
17.250 1.3037 0.05380 0.04885 0.0240 0.0174 1.0000
17.500 1.3068 0.05633 0.05142 0.0235 0.0161 1.0000
17.750 1.3082 0.05910 0.05423 0.0229 0.0148 1.0000
18.000 1.3089 0.06200 0.05717 0.0222 0.0138 1.0000
18.250 1.3100 0.06491 0.06013 0.0214 0.0128 1.0000
18.500 1.3087 0.06818 0.06346 0.0204 0.0119 1.0000
18.750 1.3072 0.07156 0.06689 0.0193 0.0112 1.0000
19.000 1.3056 0.07500 0.07040 0.0182 0.0105 1.0000
19.250 1.3034 0.07859 0.07405 0.0168 0.0099 1.0000
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