TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il) Reynolds number: 500,000 Max Cl/Cd: 86.54 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tsagi-r-3a-il-500000.txt Download as CSV file: xf-tsagi-r-3a-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: TsAGI R-3a (12%)
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
------ -------- --------- --------- -------- -------- --------
-9.500 -0.3487 0.09677 0.09480 0.0009 1.0045 0.0279
-9.250 -0.3756 0.08623 0.08426 -0.0068 1.0045 0.0293
-9.000 -0.3810 0.08043 0.07850 -0.0091 1.0045 0.0295
-8.750 -0.3759 0.07734 0.07543 -0.0091 1.0045 0.0296
-8.500 -0.3722 0.07399 0.07210 -0.0097 1.0045 0.0298
-8.250 -0.3697 0.07042 0.06857 -0.0108 1.0045 0.0300
-8.000 -0.3705 0.06624 0.06442 -0.0127 1.0045 0.0303
-7.750 -0.3719 0.06094 0.05913 -0.0168 0.9555 0.0305
-7.500 -0.3867 0.05413 0.05214 -0.0234 0.8773 0.0306
-7.250 -0.3926 0.04857 0.04626 -0.0265 0.8063 0.0310
-7.000 -0.3932 0.04288 0.04023 -0.0292 0.7457 0.0316
-6.750 -0.4605 0.02453 0.01989 -0.0354 0.9424 0.0219
-6.500 -0.4414 0.02262 0.01761 -0.0337 0.8601 0.0216
-6.250 -0.4234 0.02084 0.01524 -0.0317 0.7679 0.0214
-6.000 -0.4016 0.01936 0.01315 -0.0305 0.6806 0.0213
-5.750 -0.3773 0.01816 0.01144 -0.0297 0.6116 0.0214
-5.250 -0.3250 0.01648 0.00908 -0.0286 0.5350 0.0218
-5.000 -0.2988 0.01552 0.00796 -0.0282 0.5161 0.0222
-4.750 -0.2719 0.01494 0.00730 -0.0279 0.5031 0.0226
-4.250 -0.2171 0.01405 0.00626 -0.0273 0.4832 0.0237
-4.000 -0.1896 0.01366 0.00576 -0.0270 0.4751 0.0244
-3.750 -0.1616 0.01336 0.00537 -0.0267 0.4685 0.0254
-3.500 -0.1343 0.01294 0.00495 -0.0264 0.4620 0.0266
-3.250 -0.1066 0.01269 0.00464 -0.0262 0.4562 0.0280
-3.000 -0.0785 0.01239 0.00429 -0.0259 0.4515 0.0295
-2.750 -0.0507 0.01206 0.00397 -0.0257 0.4465 0.0318
-2.500 -0.0229 0.01178 0.00365 -0.0254 0.4419 0.0359
-2.250 0.0049 0.01149 0.00335 -0.0252 0.4376 0.0451
-2.000 0.0331 0.01124 0.00315 -0.0250 0.4335 0.0563
-1.750 0.0612 0.01105 0.00301 -0.0248 0.4291 0.0698
-1.500 0.0890 0.01085 0.00292 -0.0247 0.4247 0.1030
-1.250 0.1169 0.01068 0.00286 -0.0246 0.4202 0.1437
-1.000 0.1450 0.01043 0.00277 -0.0245 0.4157 0.1926
-0.750 0.1717 0.00991 0.00269 -0.0244 0.4107 0.3237
-0.500 0.1960 0.00915 0.00266 -0.0240 0.4059 0.5533
-0.250 0.2189 0.00856 0.00271 -0.0227 0.4015 0.7360
0.000 0.2407 0.00819 0.00277 -0.0207 0.3967 0.8645
0.250 0.2715 0.00814 0.00280 -0.0205 0.3909 0.9402
0.500 0.3144 0.00823 0.00280 -0.0232 0.3842 0.9738
0.750 0.3576 0.00825 0.00277 -0.0261 0.3761 0.9888
1.000 0.3984 0.00832 0.00273 -0.0286 0.3676 0.9955
1.250 0.4247 0.00833 0.00269 -0.0281 0.3584 0.9955
1.500 0.4509 0.00838 0.00266 -0.0276 0.3484 0.9955
1.750 0.4772 0.00847 0.00264 -0.0272 0.3364 0.9955
2.000 0.5036 0.00855 0.00264 -0.0268 0.3225 0.9955
2.250 0.5300 0.00868 0.00267 -0.0263 0.3089 0.9955
2.500 0.5563 0.00884 0.00273 -0.0259 0.2981 0.9955
2.750 0.5826 0.00904 0.00282 -0.0255 0.2896 0.9955
3.000 0.6092 0.00921 0.00293 -0.0252 0.2828 0.9955
3.250 0.6356 0.00944 0.00307 -0.0248 0.2765 0.9955
3.500 0.6624 0.00962 0.00321 -0.0245 0.2717 0.9955
3.750 0.6892 0.00981 0.00336 -0.0243 0.2668 0.9955
4.000 0.7157 0.01006 0.00353 -0.0240 0.2623 0.9955
4.250 0.7422 0.01032 0.00375 -0.0237 0.2584 0.9955
4.500 0.7694 0.01047 0.00391 -0.0235 0.2558 0.9955
4.750 0.7965 0.01064 0.00408 -0.0232 0.2529 0.9955
5.000 0.8234 0.01085 0.00427 -0.0230 0.2497 0.9955
5.250 0.8499 0.01111 0.00449 -0.0228 0.2465 0.9955
5.500 0.8759 0.01146 0.00479 -0.0225 0.2431 0.9955
5.750 0.9032 0.01160 0.00497 -0.0223 0.2413 0.9955
6.000 0.9302 0.01178 0.00518 -0.0221 0.2390 0.9955
6.250 0.9571 0.01197 0.00539 -0.0219 0.2364 0.9955
6.500 0.9838 0.01218 0.00560 -0.0218 0.2336 0.9955
6.750 1.0099 0.01247 0.00586 -0.0215 0.2305 0.9955
7.000 1.0356 0.01283 0.00620 -0.0212 0.2272 0.9955
7.250 1.0626 0.01297 0.00641 -0.0211 0.2249 0.9955
7.500 1.0891 0.01316 0.00664 -0.0209 0.2221 0.9955
7.750 1.1155 0.01337 0.00687 -0.0207 0.2192 0.9955
8.000 1.1413 0.01364 0.00714 -0.0204 0.2161 0.9955
8.250 1.1659 0.01409 0.00756 -0.0201 0.2123 0.9955
8.500 1.1925 0.01422 0.00778 -0.0199 0.2098 0.9955
8.750 1.2187 0.01440 0.00802 -0.0197 0.2062 0.9955
9.000 1.2443 0.01461 0.00824 -0.0195 0.2021 0.9955
9.250 1.2684 0.01502 0.00862 -0.0191 0.1974 0.9955
9.500 1.2948 0.01512 0.00883 -0.0190 0.1935 0.9955
9.750 1.3203 0.01531 0.00906 -0.0187 0.1887 0.9955
10.000 1.3440 0.01569 0.00940 -0.0183 0.1835 0.9955
10.250 1.3700 0.01583 0.00964 -0.0182 0.1781 0.9955
10.500 1.3941 0.01613 0.00993 -0.0178 0.1725 0.9955
10.750 1.4180 0.01647 0.01031 -0.0174 0.1673 0.9955
11.000 1.4416 0.01682 0.01069 -0.0170 0.1620 0.9955
11.250 1.4636 0.01729 0.01115 -0.0165 0.1569 0.9955
11.500 1.4863 0.01768 0.01160 -0.0160 0.1521 0.9955
11.750 1.5069 0.01823 0.01214 -0.0153 0.1468 0.9955
12.000 1.5277 0.01874 0.01269 -0.0146 0.1424 0.9955
12.250 1.5476 0.01929 0.01328 -0.0139 0.1384 0.9955
12.500 1.5651 0.01999 0.01400 -0.0129 0.1349 0.9955
12.750 1.5829 0.02062 0.01469 -0.0119 0.1318 0.9955
13.000 1.6009 0.02121 0.01536 -0.0110 0.1287 0.9955
13.250 1.6157 0.02196 0.01616 -0.0098 0.1254 0.9955
13.500 1.6243 0.02291 0.01713 -0.0078 0.1224 0.9955
13.750 1.6365 0.02366 0.01798 -0.0063 0.1197 0.9955
14.000 1.6478 0.02451 0.01892 -0.0049 0.1169 0.9955
14.250 1.6554 0.02570 0.02018 -0.0036 0.1142 0.9955
14.500 1.6587 0.02736 0.02190 -0.0026 0.1115 0.9955
14.750 1.6649 0.02902 0.02366 -0.0021 0.1091 0.9955
15.000 1.6725 0.03072 0.02548 -0.0021 0.1063 0.9955
15.250 1.6748 0.03318 0.02802 -0.0026 0.1033 0.9955
15.500 1.6702 0.03670 0.03162 -0.0038 0.1005 0.9955
15.750 1.6701 0.03982 0.03486 -0.0049 0.0981 0.9955
16.000 1.6677 0.04331 0.03848 -0.0062 0.0954 0.9955
16.250 1.6579 0.04775 0.04302 -0.0079 0.0927 0.9955
16.500 1.6415 0.05297 0.04833 -0.0098 0.0906 0.9955
16.750 1.6280 0.05774 0.05321 -0.0113 0.0885 0.9955
17.000 1.6139 0.06255 0.05813 -0.0128 0.0857 0.9955
17.250 1.5937 0.06811 0.06378 -0.0146 0.0833 0.9955
17.500 1.5704 0.07420 0.06995 -0.0167 0.0811 0.9955
17.750 1.5535 0.07962 0.07546 -0.0186 0.0787 0.9955
18.000 1.5353 0.08538 0.08132 -0.0207 0.0756 0.9955
18.250 1.5123 0.09201 0.08802 -0.0233 0.0728 0.9955
18.500 1.4934 0.09813 0.09422 -0.0257 0.0698 0.9955
18.750 1.4715 0.10487 0.10104 -0.0284 0.0661 0.9955
19.000 1.4483 0.11189 0.10812 -0.0314 0.0627 0.9955
19.250 1.4264 0.11887 0.11516 -0.0345 0.0588 0.9955
|
Polar data table (+)
Polar graphs
<< Back to TsAGI R-3a (12%) (tsagi-r-3a-il)