S8064 (s8064-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: S8064 (s8064-il) Reynolds number: 1,000,000 Max Cl/Cd: 89.95 at α=3.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-s8064-il-1000000.txt Download as CSV file: xf-s8064-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: S8064
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
------ -------- --------- --------- -------- -------- --------
-13.000 -0.6911 0.06751 0.06564 -0.0580 1.0000 0.0070
-12.750 -0.7289 0.05647 0.05440 -0.0664 0.9870 0.0067
-12.500 -0.7351 0.04968 0.04738 -0.0743 0.9698 0.0068
-12.250 -0.7523 0.04396 0.04139 -0.0781 0.9532 0.0068
-12.000 -0.7640 0.04096 0.03820 -0.0777 0.9422 0.0068
-11.750 -0.7926 0.03686 0.03381 -0.0753 0.9325 0.0065
-11.500 -0.8122 0.03371 0.03039 -0.0721 0.9256 0.0064
-11.250 -0.8310 0.03069 0.02706 -0.0679 0.9197 0.0063
-11.000 -0.8326 0.02925 0.02545 -0.0647 0.9156 0.0063
-10.750 -0.8312 0.02794 0.02399 -0.0615 0.9124 0.0064
-10.500 -0.8326 0.02566 0.02143 -0.0580 0.9089 0.0063
-10.250 -0.8210 0.02452 0.02014 -0.0562 0.9064 0.0065
-10.000 -0.8108 0.02281 0.01820 -0.0541 0.9042 0.0065
-9.750 -0.7971 0.02145 0.01665 -0.0524 0.9018 0.0065
-9.500 -0.7816 0.02004 0.01508 -0.0509 0.9000 0.0065
-9.250 -0.7647 0.01881 0.01370 -0.0496 0.8981 0.0065
-9.000 -0.7470 0.01772 0.01248 -0.0482 0.8960 0.0066
-8.750 -0.7282 0.01682 0.01147 -0.0471 0.8939 0.0067
-8.500 -0.7086 0.01601 0.01056 -0.0459 0.8920 0.0069
-8.250 -0.6884 0.01531 0.00976 -0.0449 0.8902 0.0070
-8.000 -0.6668 0.01476 0.00913 -0.0440 0.8884 0.0072
-7.750 -0.6445 0.01425 0.00855 -0.0433 0.8867 0.0073
-7.500 -0.6271 0.01316 0.00734 -0.0418 0.8849 0.0080
-7.250 -0.6042 0.01265 0.00678 -0.0411 0.8830 0.0083
-7.000 -0.5805 0.01223 0.00632 -0.0406 0.8811 0.0088
-6.750 -0.5563 0.01186 0.00591 -0.0401 0.8792 0.0094
-6.500 -0.5318 0.01151 0.00551 -0.0396 0.8774 0.0099
-6.250 -0.5073 0.01117 0.00510 -0.0391 0.8757 0.0105
-6.000 -0.4835 0.01077 0.00467 -0.0385 0.8738 0.0131
-5.750 -0.4598 0.01032 0.00430 -0.0380 0.8720 0.0244
-5.500 -0.4349 0.00996 0.00402 -0.0376 0.8701 0.0391
-5.250 -0.4095 0.00968 0.00379 -0.0374 0.8681 0.0521
-5.000 -0.3839 0.00941 0.00357 -0.0372 0.8660 0.0668
-4.750 -0.3585 0.00912 0.00336 -0.0369 0.8640 0.0865
-4.500 -0.3334 0.00882 0.00315 -0.0366 0.8620 0.1138
-4.250 -0.3090 0.00846 0.00295 -0.0362 0.8600 0.1547
-4.000 -0.2853 0.00804 0.00276 -0.0357 0.8578 0.2137
-3.750 -0.2622 0.00752 0.00255 -0.0351 0.8554 0.2916
-3.500 -0.2385 0.00707 0.00237 -0.0346 0.8528 0.3635
-3.250 -0.2146 0.00665 0.00220 -0.0341 0.8503 0.4388
-3.000 -0.1899 0.00632 0.00207 -0.0337 0.8479 0.5010
-2.750 -0.1645 0.00608 0.00196 -0.0333 0.8456 0.5496
-2.500 -0.1382 0.00591 0.00190 -0.0331 0.8432 0.5865
-2.250 -0.1120 0.00571 0.00183 -0.0328 0.8404 0.6249
-2.000 -0.0856 0.00556 0.00179 -0.0326 0.8375 0.6632
-1.750 -0.0583 0.00547 0.00176 -0.0325 0.8346 0.6913
-1.500 -0.0306 0.00542 0.00172 -0.0324 0.8320 0.7112
-1.250 -0.0026 0.00541 0.00171 -0.0325 0.8292 0.7264
-1.000 0.0255 0.00537 0.00170 -0.0326 0.8259 0.7386
-0.750 0.0538 0.00534 0.00167 -0.0326 0.8222 0.7499
-0.500 0.0819 0.00529 0.00164 -0.0327 0.8187 0.7598
-0.250 0.1101 0.00528 0.00161 -0.0327 0.8153 0.7689
0.000 0.1383 0.00525 0.00160 -0.0328 0.8106 0.7771
0.250 0.1665 0.00519 0.00156 -0.0329 0.8055 0.7839
0.500 0.1948 0.00517 0.00152 -0.0329 0.8008 0.7902
0.750 0.2231 0.00513 0.00150 -0.0331 0.7939 0.7957
1.000 0.2512 0.00508 0.00146 -0.0331 0.7873 0.8007
1.250 0.2794 0.00505 0.00145 -0.0332 0.7783 0.8058
1.500 0.3076 0.00503 0.00142 -0.0333 0.7685 0.8105
1.750 0.3353 0.00501 0.00140 -0.0332 0.7562 0.8150
2.000 0.3628 0.00503 0.00139 -0.0332 0.7406 0.8196
2.250 0.3899 0.00509 0.00139 -0.0331 0.7222 0.8240
2.500 0.4162 0.00517 0.00142 -0.0328 0.7002 0.8282
2.750 0.4421 0.00529 0.00148 -0.0324 0.6750 0.8326
3.000 0.4678 0.00544 0.00155 -0.0321 0.6487 0.8372
3.250 0.4935 0.00557 0.00163 -0.0317 0.6251 0.8415
3.500 0.5180 0.00576 0.00175 -0.0312 0.5930 0.8462
3.750 0.5415 0.00602 0.00188 -0.0305 0.5546 0.8513
4.000 0.5633 0.00634 0.00204 -0.0295 0.5041 0.8564
4.250 0.5833 0.00677 0.00224 -0.0281 0.4430 0.8621
4.500 0.6029 0.00726 0.00248 -0.0268 0.3795 0.8683
4.750 0.6218 0.00773 0.00274 -0.0254 0.3185 0.8751
5.000 0.6409 0.00823 0.00301 -0.0240 0.2611 0.8830
5.250 0.6590 0.00872 0.00330 -0.0224 0.2066 0.8919
5.500 0.6780 0.00915 0.00358 -0.0210 0.1643 0.9023
5.750 0.6963 0.00959 0.00388 -0.0194 0.1253 0.9148
6.000 0.7161 0.00994 0.00416 -0.0180 0.0993 0.9299
6.250 0.7393 0.01029 0.00447 -0.0174 0.0786 0.9478
6.500 0.7703 0.01072 0.00484 -0.0186 0.0620 0.9634
6.750 0.8052 0.01113 0.00521 -0.0207 0.0512 0.9756
7.000 0.8398 0.01151 0.00558 -0.0226 0.0439 0.9859
7.250 0.8732 0.01198 0.00600 -0.0244 0.0363 0.9939
7.750 0.9235 0.01270 0.00669 -0.0244 0.0275 1.0000
8.000 0.9406 0.01293 0.00694 -0.0225 0.0250 1.0000
8.250 0.9547 0.01334 0.00731 -0.0202 0.0201 1.0000
8.500 0.9683 0.01371 0.00767 -0.0177 0.0167 1.0000
8.750 0.9815 0.01416 0.00813 -0.0152 0.0141 1.0000
9.000 0.9964 0.01459 0.00859 -0.0131 0.0128 1.0000
9.250 1.0090 0.01524 0.00926 -0.0107 0.0112 1.0000
9.500 1.0239 0.01579 0.00986 -0.0087 0.0106 1.0000
9.750 1.0402 0.01627 0.01039 -0.0071 0.0102 1.0000
10.000 1.0558 0.01682 0.01099 -0.0054 0.0096 1.0000
10.250 1.0709 0.01741 0.01163 -0.0037 0.0092 1.0000
10.500 1.0859 0.01803 0.01228 -0.0021 0.0087 1.0000
10.750 1.0986 0.01882 0.01312 -0.0002 0.0084 1.0000
11.000 1.1017 0.02029 0.01474 0.0030 0.0078 1.0000
11.250 1.1160 0.02099 0.01551 0.0046 0.0076 1.0000
11.500 1.1284 0.02185 0.01644 0.0063 0.0074 1.0000
11.750 1.1398 0.02277 0.01744 0.0081 0.0073 1.0000
12.000 1.1506 0.02377 0.01853 0.0098 0.0071 1.0000
12.250 1.1608 0.02481 0.01965 0.0116 0.0070 1.0000
12.500 1.1694 0.02599 0.02093 0.0134 0.0068 1.0000
12.750 1.1788 0.02712 0.02214 0.0150 0.0066 1.0000
13.000 1.1867 0.02839 0.02350 0.0167 0.0065 1.0000
13.250 1.1925 0.02985 0.02507 0.0184 0.0064 1.0000
13.500 1.1981 0.03134 0.02665 0.0199 0.0062 1.0000
13.750 1.2049 0.03274 0.02813 0.0212 0.0060 1.0000
14.000 1.2074 0.03457 0.03006 0.0227 0.0060 1.0000
14.250 1.2089 0.03655 0.03214 0.0240 0.0058 1.0000
14.500 1.2034 0.03928 0.03500 0.0254 0.0056 1.0000
14.750 1.1952 0.04242 0.03830 0.0266 0.0055 1.0000
15.000 1.1775 0.04684 0.04294 0.0274 0.0054 1.0000
15.250 1.1651 0.05098 0.04727 0.0275 0.0053 1.0000
15.500 1.1543 0.05520 0.05165 0.0271 0.0053 1.0000
15.750 1.1663 0.05673 0.05324 0.0265 0.0052 1.0000
16.000 1.1473 0.06245 0.05914 0.0250 0.0053 1.0000
16.250 1.1390 0.06712 0.06395 0.0232 0.0052 1.0000
16.500 1.1245 0.07305 0.07003 0.0207 0.0052 1.0000
16.750 1.1156 0.07844 0.07556 0.0179 0.0052 1.0000
17.000 1.0845 0.08807 0.08538 0.0129 0.0053 1.0000
17.250 1.0799 0.09347 0.09089 0.0097 0.0051 1.0000
17.500 1.0471 0.10460 0.10220 0.0034 0.0052 1.0000
17.750 1.0207 0.11501 0.11277 -0.0026 0.0053 1.0000
18.000 0.9929 0.12616 0.12406 -0.0090 0.0053 1.0000
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