S1016 (s1016-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1016 (s1016-il) Reynolds number: 1,000,000 Max Cl/Cd: 51.99 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1016-il-1000000-n5.txt Download as CSV file: xf-s1016-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1016
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 -1.2677 0.06371 0.05860 -0.0637 0.8374 0.0169
-19.500 -1.2718 0.06015 0.05496 -0.0648 0.8363 0.0173
-19.250 -1.2738 0.05695 0.05167 -0.0657 0.8352 0.0177
-19.000 -1.2734 0.05414 0.04877 -0.0663 0.8340 0.0180
-18.750 -1.2720 0.05154 0.04609 -0.0668 0.8329 0.0184
-18.500 -1.2717 0.04891 0.04338 -0.0670 0.8317 0.0189
-18.250 -1.2700 0.04652 0.04092 -0.0671 0.8306 0.0195
-18.000 -1.2664 0.04439 0.03871 -0.0670 0.8295 0.0198
-17.750 -1.2621 0.04239 0.03666 -0.0668 0.8284 0.0205
-17.500 -1.2562 0.04062 0.03482 -0.0665 0.8273 0.0211
-17.000 -1.2429 0.03734 0.03142 -0.0655 0.8253 0.0225
-16.750 -1.2354 0.03583 0.02987 -0.0649 0.8247 0.0232
-16.500 -1.2270 0.03443 0.02842 -0.0643 0.8239 0.0240
-16.250 -1.2177 0.03316 0.02710 -0.0635 0.8231 0.0248
-16.000 -1.2071 0.03201 0.02591 -0.0628 0.8222 0.0257
-15.750 -1.1976 0.03081 0.02468 -0.0619 0.8213 0.0268
-15.500 -1.1869 0.02972 0.02356 -0.0610 0.8204 0.0278
-15.250 -1.1752 0.02873 0.02254 -0.0601 0.8196 0.0290
-15.000 -1.1627 0.02782 0.02159 -0.0592 0.8188 0.0299
-14.750 -1.1499 0.02695 0.02067 -0.0583 0.8180 0.0310
-14.500 -1.1376 0.02605 0.01977 -0.0573 0.8172 0.0324
-14.250 -1.1240 0.02526 0.01895 -0.0563 0.8164 0.0339
-14.000 -1.1090 0.02457 0.01822 -0.0554 0.8156 0.0350
-13.750 -1.0952 0.02382 0.01745 -0.0544 0.8149 0.0365
-13.500 -1.0811 0.02311 0.01672 -0.0533 0.8141 0.0383
-13.250 -1.0651 0.02250 0.01609 -0.0524 0.8134 0.0398
-13.000 -1.0488 0.02192 0.01548 -0.0515 0.8127 0.0412
-12.750 -1.0339 0.02129 0.01483 -0.0504 0.8119 0.0431
-12.500 -1.0177 0.02072 0.01425 -0.0494 0.8111 0.0451
-12.250 -1.0002 0.02023 0.01373 -0.0485 0.8104 0.0469
-12.000 -0.9830 0.01973 0.01321 -0.0475 0.8096 0.0485
-11.750 -0.9666 0.01919 0.01268 -0.0465 0.8087 0.0513
-11.500 -0.9487 0.01872 0.01220 -0.0455 0.8083 0.0534
-11.250 -0.9303 0.01828 0.01175 -0.0447 0.8079 0.0556
-11.000 -0.9125 0.01780 0.01129 -0.0437 0.8074 0.0584
-10.750 -0.8939 0.01738 0.01087 -0.0428 0.8070 0.0614
-10.500 -0.8753 0.01696 0.01045 -0.0419 0.8064 0.0642
-10.250 -0.8570 0.01653 0.01003 -0.0409 0.8059 0.0681
-10.000 -0.8373 0.01617 0.00967 -0.0400 0.8053 0.0713
-9.750 -0.8185 0.01576 0.00929 -0.0391 0.8046 0.0754
-9.500 -0.7992 0.01539 0.00893 -0.0381 0.8038 0.0793
-9.250 -0.7791 0.01506 0.00860 -0.0373 0.8032 0.0827
-9.000 -0.7597 0.01469 0.00826 -0.0364 0.8026 0.0874
-8.750 -0.7394 0.01438 0.00795 -0.0355 0.8020 0.0918
-8.500 -0.7192 0.01406 0.00765 -0.0346 0.8013 0.0962
-8.250 -0.6994 0.01373 0.00735 -0.0337 0.8007 0.1013
-8.000 -0.6783 0.01346 0.00708 -0.0329 0.8001 0.1060
-7.750 -0.6582 0.01314 0.00680 -0.0319 0.7995 0.1116
-7.500 -0.6375 0.01287 0.00654 -0.0311 0.7989 0.1173
-7.250 -0.6171 0.01258 0.00628 -0.0301 0.7982 0.1235
-7.000 -0.5963 0.01231 0.00603 -0.0293 0.7976 0.1295
-6.750 -0.5755 0.01205 0.00579 -0.0284 0.7970 0.1362
-6.500 -0.5551 0.01177 0.00555 -0.0273 0.7964 0.1440
-6.250 -0.5341 0.01153 0.00533 -0.0264 0.7956 0.1509
-6.000 -0.5139 0.01127 0.00511 -0.0254 0.7948 0.1598
-5.750 -0.4939 0.01100 0.00489 -0.0243 0.7941 0.1699
-5.500 -0.4736 0.01077 0.00468 -0.0232 0.7934 0.1803
-5.250 -0.4541 0.01052 0.00449 -0.0220 0.7927 0.1917
-5.000 -0.4348 0.01028 0.00430 -0.0206 0.7918 0.2037
-4.750 -0.4160 0.01003 0.00412 -0.0192 0.7911 0.2171
-4.500 -0.3970 0.00982 0.00396 -0.0178 0.7904 0.2295
-4.000 -0.3640 0.00942 0.00371 -0.0138 0.7888 0.2625
-3.750 -0.3455 0.00922 0.00359 -0.0122 0.7878 0.2812
-3.500 -0.3262 0.00898 0.00347 -0.0108 0.7867 0.3040
-3.250 -0.3056 0.00875 0.00334 -0.0096 0.7854 0.3272
-3.000 -0.2845 0.00853 0.00321 -0.0085 0.7840 0.3514
-2.750 -0.2641 0.00826 0.00308 -0.0072 0.7826 0.3824
-2.500 -0.2428 0.00799 0.00293 -0.0062 0.7809 0.4115
-2.250 -0.2218 0.00768 0.00274 -0.0050 0.7786 0.4471
-2.000 -0.2006 0.00736 0.00255 -0.0039 0.7759 0.4848
-1.750 -0.1790 0.00704 0.00239 -0.0028 0.7728 0.5245
-1.500 -0.1581 0.00665 0.00221 -0.0016 0.7692 0.5714
-1.250 -0.1361 0.00629 0.00203 -0.0006 0.7656 0.6185
-1.000 -0.1136 0.00595 0.00191 0.0004 0.7621 0.6694
-0.750 -0.0876 0.00583 0.00192 0.0008 0.7585 0.7108
-0.500 -0.0587 0.00582 0.00197 0.0006 0.7537 0.7273
-0.250 -0.0295 0.00582 0.00199 0.0003 0.7486 0.7370
0.000 0.0000 0.00580 0.00194 0.0000 0.7435 0.7435
0.250 0.0295 0.00582 0.00199 -0.0003 0.7370 0.7486
0.500 0.0587 0.00582 0.00197 -0.0006 0.7273 0.7538
0.750 0.0875 0.00583 0.00192 -0.0008 0.7105 0.7585
1.000 0.1135 0.00595 0.00191 -0.0004 0.6693 0.7622
1.250 0.1360 0.00629 0.00203 0.0006 0.6179 0.7656
1.500 0.1581 0.00665 0.00221 0.0016 0.5711 0.7692
1.750 0.1792 0.00703 0.00239 0.0028 0.5255 0.7728
2.000 0.2006 0.00736 0.00255 0.0039 0.4848 0.7759
2.250 0.2222 0.00766 0.00274 0.0049 0.4494 0.7786
2.500 0.2429 0.00799 0.00293 0.0061 0.4122 0.7809
2.750 0.2641 0.00826 0.00308 0.0072 0.3822 0.7826
3.000 0.2846 0.00852 0.00321 0.0085 0.3518 0.7840
3.250 0.3054 0.00876 0.00334 0.0096 0.3260 0.7854
3.500 0.3262 0.00898 0.00347 0.0108 0.3039 0.7867
3.750 0.3455 0.00922 0.00359 0.0122 0.2812 0.7878
4.000 0.3638 0.00943 0.00371 0.0138 0.2616 0.7888
4.250 0.3802 0.00961 0.00382 0.0159 0.2449 0.7897
4.500 0.3971 0.00982 0.00396 0.0178 0.2295 0.7904
4.750 0.4155 0.01005 0.00412 0.0193 0.2156 0.7911
5.000 0.4346 0.01029 0.00430 0.0207 0.2029 0.7918
5.250 0.4542 0.01051 0.00448 0.0219 0.1919 0.7927
5.500 0.4737 0.01076 0.00468 0.0232 0.1804 0.7934
5.750 0.4940 0.01100 0.00489 0.0242 0.1701 0.7941
6.000 0.5142 0.01126 0.00510 0.0253 0.1605 0.7948
6.250 0.5344 0.01152 0.00533 0.0264 0.1513 0.7956
6.500 0.5553 0.01177 0.00555 0.0273 0.1443 0.7964
6.750 0.5752 0.01206 0.00580 0.0284 0.1351 0.7970
7.000 0.5965 0.01231 0.00603 0.0292 0.1295 0.7976
7.250 0.6172 0.01258 0.00628 0.0301 0.1234 0.7983
7.500 0.6378 0.01286 0.00653 0.0310 0.1175 0.7989
7.750 0.6587 0.01313 0.00679 0.0319 0.1122 0.7995
8.000 0.6786 0.01345 0.00708 0.0329 0.1059 0.8001
8.250 0.6998 0.01372 0.00734 0.0336 0.1021 0.8007
8.500 0.7196 0.01405 0.00764 0.0346 0.0962 0.8014
8.750 0.7397 0.01437 0.00795 0.0355 0.0919 0.8020
9.000 0.7599 0.01469 0.00826 0.0363 0.0872 0.8026
9.250 0.7794 0.01506 0.00859 0.0373 0.0827 0.8032
9.500 0.7996 0.01538 0.00892 0.0381 0.0795 0.8039
9.750 0.8189 0.01575 0.00928 0.0390 0.0755 0.8046
10.000 0.8377 0.01616 0.00966 0.0400 0.0714 0.8053
10.250 0.8575 0.01652 0.01003 0.0408 0.0682 0.8059
10.500 0.8757 0.01696 0.01044 0.0418 0.0641 0.8065
10.750 0.8944 0.01737 0.01085 0.0427 0.0615 0.8070
11.000 0.9129 0.01780 0.01128 0.0436 0.0582 0.8074
11.250 0.9307 0.01827 0.01174 0.0446 0.0554 0.8079
11.500 0.9492 0.01871 0.01219 0.0455 0.0533 0.8083
11.750 0.9671 0.01918 0.01267 0.0464 0.0513 0.8087
12.000 0.9839 0.01969 0.01318 0.0474 0.0488 0.8096
12.250 1.0007 0.02022 0.01372 0.0484 0.0467 0.8104
12.500 1.0183 0.02071 0.01423 0.0493 0.0449 0.8111
12.750 1.0344 0.02127 0.01481 0.0503 0.0430 0.8119
13.000 1.0495 0.02191 0.01546 0.0514 0.0411 0.8127
13.250 1.0658 0.02248 0.01606 0.0523 0.0399 0.8134
13.500 1.0819 0.02308 0.01669 0.0532 0.0384 0.8141
13.750 1.0959 0.02380 0.01742 0.0543 0.0364 0.8149
14.000 1.1098 0.02454 0.01819 0.0553 0.0351 0.8157
14.250 1.1248 0.02524 0.01892 0.0562 0.0337 0.8164
14.500 1.1384 0.02602 0.01973 0.0572 0.0323 0.8172
14.750 1.1508 0.02690 0.02063 0.0582 0.0311 0.8180
15.000 1.1635 0.02779 0.02155 0.0592 0.0299 0.8188
15.250 1.1762 0.02868 0.02249 0.0600 0.0289 0.8196
15.500 1.1880 0.02967 0.02351 0.0609 0.0279 0.8204
15.750 1.1990 0.03073 0.02460 0.0618 0.0268 0.8213
16.000 1.2083 0.03195 0.02585 0.0627 0.0258 0.8222
16.250 1.2190 0.03308 0.02703 0.0634 0.0247 0.8231
16.500 1.2284 0.03436 0.02835 0.0641 0.0240 0.8240
16.750 1.2368 0.03574 0.02978 0.0648 0.0232 0.8247
17.000 1.2439 0.03729 0.03135 0.0654 0.0223 0.8253
17.500 1.2577 0.04051 0.03471 0.0664 0.0212 0.8273
17.750 1.2638 0.04227 0.03653 0.0667 0.0205 0.8285
18.000 1.2685 0.04423 0.03856 0.0669 0.0200 0.8296
18.250 1.2715 0.04641 0.04080 0.0670 0.0193 0.8307
18.500 1.2733 0.04879 0.04325 0.0669 0.0188 0.8318
18.750 1.2744 0.05132 0.04586 0.0667 0.0184 0.8329
19.000 1.2758 0.05392 0.04855 0.0663 0.0181 0.8341
19.250 1.2758 0.05677 0.05148 0.0657 0.0177 0.8353
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