TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il) Reynolds number: 200,000 Max Cl/Cd: 60.81 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tsagi-r-3a-il-200000-n5.txt Download as CSV file: xf-tsagi-r-3a-il-200000-n5.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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.4693 0.10107 0.09766 0.0062 1.0045 0.0256
-9.000 -0.4785 0.08805 0.08468 -0.0011 1.0045 0.0218
-8.750 -0.4750 0.08436 0.08103 -0.0033 1.0045 0.0217
-8.500 -0.4741 0.08000 0.07671 -0.0063 1.0045 0.0215
-8.250 -0.4769 0.07472 0.07148 -0.0110 1.0045 0.0212
-8.000 -0.4813 0.06765 0.06440 -0.0186 1.0045 0.0209
-7.750 -0.4854 0.05906 0.05568 -0.0256 1.0045 0.0204
-7.500 -0.5035 0.04431 0.04034 -0.0319 1.0045 0.0196
-7.250 -0.5107 0.03352 0.02857 -0.0328 1.0045 0.0193
-7.000 -0.4876 0.02965 0.02420 -0.0341 0.9675 0.0195
-6.750 -0.4571 0.02681 0.02087 -0.0357 0.9101 0.0198
-6.500 -0.4328 0.02485 0.01842 -0.0351 0.8414 0.0201
-6.250 -0.4121 0.02340 0.01645 -0.0336 0.7726 0.0204
-6.000 -0.3902 0.02224 0.01478 -0.0322 0.7108 0.0210
-5.750 -0.3666 0.02109 0.01307 -0.0311 0.6598 0.0218
-5.500 -0.3419 0.02057 0.01235 -0.0305 0.6196 0.0224
-5.250 -0.3162 0.01998 0.01154 -0.0300 0.5894 0.0231
-5.000 -0.2902 0.01926 0.01059 -0.0295 0.5658 0.0236
-4.250 -0.2112 0.01735 0.00810 -0.0280 0.5114 0.0258
-4.000 -0.1844 0.01692 0.00758 -0.0277 0.4976 0.0268
-3.750 -0.1574 0.01648 0.00702 -0.0273 0.4871 0.0283
-3.500 -0.1304 0.01608 0.00653 -0.0270 0.4778 0.0301
-3.250 -0.1031 0.01576 0.00613 -0.0267 0.4704 0.0332
-3.000 -0.0758 0.01539 0.00573 -0.0264 0.4632 0.0368
-2.500 -0.0211 0.01474 0.00497 -0.0258 0.4506 0.0483
-2.250 0.0064 0.01450 0.00470 -0.0256 0.4444 0.0570
-1.750 0.0613 0.01402 0.00436 -0.0252 0.4333 0.0987
-1.500 0.0887 0.01378 0.00423 -0.0250 0.4276 0.1362
-1.250 0.1159 0.01358 0.00410 -0.0248 0.4226 0.1771
-1.000 0.1431 0.01328 0.00399 -0.0246 0.4177 0.2346
-0.750 0.1692 0.01281 0.00391 -0.0244 0.4123 0.3517
-0.500 0.1919 0.01207 0.00391 -0.0234 0.4073 0.5619
-0.250 0.2118 0.01150 0.00399 -0.0211 0.4027 0.7541
0.000 0.2411 0.01129 0.00409 -0.0202 0.3966 0.8860
0.250 0.2856 0.01135 0.00408 -0.0230 0.3895 0.9533
0.500 0.3324 0.01142 0.00404 -0.0265 0.3816 0.9875
0.750 0.3669 0.01149 0.00400 -0.0278 0.3735 0.9955
1.000 0.3927 0.01157 0.00398 -0.0273 0.3665 0.9955
1.250 0.4187 0.01164 0.00398 -0.0268 0.3585 0.9955
1.500 0.4446 0.01174 0.00397 -0.0263 0.3510 0.9955
1.750 0.4709 0.01183 0.00400 -0.0259 0.3421 0.9955
2.000 0.4972 0.01195 0.00403 -0.0254 0.3337 0.9955
2.250 0.5236 0.01207 0.00407 -0.0250 0.3242 0.9955
2.500 0.5500 0.01221 0.00413 -0.0247 0.3154 0.9955
2.750 0.5764 0.01236 0.00420 -0.0243 0.3070 0.9955
3.000 0.6029 0.01254 0.00430 -0.0239 0.2992 0.9955
3.250 0.6292 0.01274 0.00440 -0.0236 0.2921 0.9955
3.500 0.6556 0.01295 0.00455 -0.0233 0.2862 0.9955
3.750 0.6820 0.01318 0.00472 -0.0229 0.2812 0.9955
4.000 0.7081 0.01344 0.00490 -0.0226 0.2766 0.9955
4.250 0.7344 0.01370 0.00511 -0.0223 0.2718 0.9955
4.500 0.7606 0.01396 0.00534 -0.0220 0.2663 0.9955
4.750 0.7864 0.01426 0.00556 -0.0217 0.2613 0.9955
5.000 0.8124 0.01457 0.00582 -0.0214 0.2574 0.9955
5.250 0.8388 0.01482 0.00611 -0.0211 0.2535 0.9955
5.500 0.8648 0.01511 0.00639 -0.0208 0.2498 0.9955
5.750 0.8905 0.01543 0.00668 -0.0205 0.2462 0.9955
6.000 0.9159 0.01582 0.00701 -0.0201 0.2431 0.9955
6.250 0.9421 0.01609 0.00734 -0.0199 0.2402 0.9955
6.500 0.9680 0.01638 0.00767 -0.0196 0.2368 0.9955
6.750 0.9935 0.01669 0.00800 -0.0193 0.2333 0.9955
7.000 1.0186 0.01705 0.00835 -0.0189 0.2300 0.9955
7.250 1.0436 0.01745 0.00873 -0.0186 0.2271 0.9955
7.500 1.0691 0.01776 0.00913 -0.0183 0.2240 0.9955
7.750 1.0942 0.01809 0.00954 -0.0180 0.2208 0.9955
8.000 1.1189 0.01845 0.00994 -0.0176 0.2175 0.9955
8.250 1.1431 0.01885 0.01034 -0.0172 0.2143 0.9955
8.500 1.1672 0.01927 0.01079 -0.0168 0.2110 0.9955
8.750 1.1916 0.01961 0.01126 -0.0164 0.2072 0.9955
9.000 1.2155 0.01999 0.01173 -0.0160 0.2034 0.9955
9.250 1.2387 0.02042 0.01218 -0.0155 0.2001 0.9955
9.500 1.2614 0.02090 0.01268 -0.0150 0.1969 0.9955
9.750 1.2846 0.02131 0.01325 -0.0145 0.1931 0.9955
10.000 1.3071 0.02175 0.01379 -0.0140 0.1892 0.9955
10.250 1.3287 0.02222 0.01430 -0.0133 0.1856 0.9955
10.500 1.3498 0.02274 0.01489 -0.0127 0.1820 0.9955
10.750 1.3710 0.02324 0.01554 -0.0120 0.1777 0.9955
11.000 1.3911 0.02377 0.01614 -0.0113 0.1737 0.9955
11.250 1.4097 0.02435 0.01675 -0.0104 0.1704 0.9955
11.500 1.4288 0.02496 0.01751 -0.0096 0.1661 0.9955
11.750 1.4462 0.02559 0.01823 -0.0087 0.1618 0.9955
12.000 1.4612 0.02629 0.01896 -0.0076 0.1579 0.9955
12.250 1.4762 0.02706 0.01985 -0.0065 0.1534 0.9955
12.500 1.4872 0.02789 0.02077 -0.0049 0.1493 0.9955
12.750 1.4941 0.02892 0.02183 -0.0031 0.1459 0.9955
13.000 1.5020 0.03009 0.02311 -0.0018 0.1425 0.9955
13.250 1.5083 0.03148 0.02462 -0.0007 0.1391 0.9955
13.500 1.5115 0.03323 0.02645 -0.0001 0.1360 0.9955
14.000 1.5148 0.03773 0.03115 -0.0001 0.1305 0.9955
14.250 1.5152 0.04044 0.03400 -0.0008 0.1279 0.9955
14.500 1.5128 0.04361 0.03729 -0.0018 0.1255 0.9955
14.750 1.5078 0.04721 0.04098 -0.0031 0.1233 0.9955
15.000 1.5011 0.05103 0.04485 -0.0045 0.1213 0.9955
15.250 1.4952 0.05492 0.04893 -0.0059 0.1192 0.9955
15.500 1.4861 0.05922 0.05338 -0.0075 0.1169 0.9955
15.750 1.4747 0.06381 0.05809 -0.0092 0.1148 0.9955
16.000 1.4623 0.06849 0.06286 -0.0109 0.1129 0.9955
16.250 1.4500 0.07311 0.06753 -0.0126 0.1110 0.9955
16.500 1.4367 0.07811 0.07266 -0.0145 0.1091 0.9955
16.750 1.4209 0.08370 0.07841 -0.0167 0.1071 0.9955
17.000 1.4039 0.08960 0.08445 -0.0192 0.1051 0.9955
17.250 1.3876 0.09550 0.09046 -0.0217 0.1031 0.9955
17.500 1.3745 0.10095 0.09598 -0.0241 0.1010 0.9955
17.750 1.3618 0.10641 0.10151 -0.0264 0.0990 0.9955
18.000 1.3379 0.11407 0.10936 -0.0300 0.0972 0.9955
18.250 1.3106 0.12250 0.11795 -0.0341 0.0949 0.9955
18.500 1.2895 0.12993 0.12549 -0.0377 0.0927 0.9955
18.750 1.2871 0.13389 0.12946 -0.0397 0.0903 0.9955
19.000 1.2500 0.14478 0.14052 -0.0455 0.0878 0.9955
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