TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il) Reynolds number: 500,000 Max Cl/Cd: 88.29 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tsagi-r-3a-il-500000-n5.txt Download as CSV file: xf-tsagi-r-3a-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.000 -0.5150 0.11840 0.11611 0.0195 1.0045 0.0128
-10.750 -0.5118 0.11430 0.11202 0.0177 1.0045 0.0128
-9.250 -0.7138 0.03066 0.02688 -0.0347 1.0045 0.0121
-9.000 -0.7017 0.02711 0.02288 -0.0342 1.0045 0.0122
-8.750 -0.6830 0.02473 0.02016 -0.0339 0.9976 0.0123
-8.500 -0.6536 0.02272 0.01782 -0.0352 0.9417 0.0124
-8.250 -0.6331 0.02149 0.01621 -0.0339 0.8712 0.0125
-7.750 -0.5912 0.01980 0.01368 -0.0313 0.7336 0.0128
-7.500 -0.5672 0.01913 0.01263 -0.0306 0.6722 0.0129
-7.250 -0.5426 0.01843 0.01160 -0.0301 0.6204 0.0130
-7.000 -0.5179 0.01760 0.01053 -0.0296 0.5805 0.0132
-6.750 -0.4922 0.01698 0.00974 -0.0293 0.5497 0.0134
-6.500 -0.4659 0.01646 0.00907 -0.0289 0.5259 0.0136
-6.250 -0.4394 0.01598 0.00845 -0.0286 0.5051 0.0138
-6.000 -0.4126 0.01553 0.00787 -0.0283 0.4862 0.0141
-5.750 -0.3856 0.01510 0.00732 -0.0280 0.4697 0.0143
-5.500 -0.3586 0.01471 0.00680 -0.0277 0.4562 0.0146
-5.250 -0.3313 0.01433 0.00632 -0.0274 0.4461 0.0149
-5.000 -0.3039 0.01398 0.00587 -0.0272 0.4383 0.0152
-4.750 -0.2762 0.01364 0.00547 -0.0269 0.4334 0.0155
-4.500 -0.2486 0.01330 0.00507 -0.0267 0.4290 0.0159
-4.250 -0.2210 0.01299 0.00471 -0.0264 0.4244 0.0166
-4.000 -0.1931 0.01275 0.00442 -0.0262 0.4200 0.0173
-3.750 -0.1650 0.01250 0.00414 -0.0260 0.4156 0.0179
-3.500 -0.1369 0.01228 0.00387 -0.0258 0.4113 0.0186
-3.250 -0.1089 0.01208 0.00364 -0.0256 0.4072 0.0196
-3.000 -0.0807 0.01192 0.00345 -0.0254 0.4034 0.0209
-2.750 -0.0523 0.01174 0.00329 -0.0253 0.4004 0.0233
-2.500 -0.0239 0.01160 0.00315 -0.0251 0.3966 0.0278
-2.250 0.0045 0.01148 0.00301 -0.0250 0.3927 0.0331
-2.000 0.0328 0.01137 0.00288 -0.0248 0.3890 0.0383
-1.750 0.0611 0.01126 0.00276 -0.0247 0.3856 0.0439
-1.500 0.0896 0.01111 0.00265 -0.0246 0.3820 0.0514
-1.250 0.1179 0.01096 0.00255 -0.0245 0.3775 0.0640
-1.000 0.1461 0.01081 0.00247 -0.0244 0.3724 0.0921
-0.750 0.1744 0.01066 0.00241 -0.0243 0.3675 0.1222
-0.500 0.2027 0.01050 0.00236 -0.0242 0.3617 0.1562
-0.250 0.2306 0.01030 0.00230 -0.0242 0.3554 0.2073
0.000 0.2579 0.00992 0.00225 -0.0241 0.3493 0.3215
0.250 0.2844 0.00943 0.00222 -0.0240 0.3414 0.4740
0.750 0.3361 0.00877 0.00223 -0.0229 0.3212 0.7073
1.000 0.3594 0.00850 0.00228 -0.0215 0.3071 0.8216
1.250 0.3843 0.00842 0.00235 -0.0203 0.2919 0.9176
1.500 0.4238 0.00855 0.00241 -0.0224 0.2790 0.9654
1.750 0.4689 0.00872 0.00247 -0.0258 0.2699 0.9911
2.000 0.5013 0.00888 0.00254 -0.0267 0.2637 0.9955
2.250 0.5274 0.00904 0.00262 -0.0263 0.2586 0.9955
2.500 0.5540 0.00916 0.00270 -0.0259 0.2546 0.9955
2.750 0.5806 0.00930 0.00280 -0.0255 0.2505 0.9955
3.000 0.6071 0.00947 0.00291 -0.0252 0.2465 0.9955
3.250 0.6338 0.00965 0.00303 -0.0248 0.2426 0.9955
3.500 0.6608 0.00978 0.00314 -0.0246 0.2395 0.9955
3.750 0.6879 0.00992 0.00325 -0.0243 0.2360 0.9955
4.000 0.7148 0.01010 0.00338 -0.0240 0.2321 0.9955
4.250 0.7415 0.01030 0.00354 -0.0238 0.2283 0.9955
4.500 0.7687 0.01045 0.00368 -0.0236 0.2263 0.9955
4.750 0.7959 0.01060 0.00383 -0.0234 0.2242 0.9955
5.000 0.8230 0.01076 0.00398 -0.0232 0.2217 0.9955
5.250 0.8500 0.01093 0.00414 -0.0230 0.2190 0.9955
5.500 0.8769 0.01113 0.00432 -0.0228 0.2164 0.9955
5.750 0.9036 0.01135 0.00452 -0.0226 0.2140 0.9955
6.000 0.9303 0.01156 0.00473 -0.0224 0.2119 0.9955
6.250 0.9574 0.01172 0.00492 -0.0222 0.2102 0.9955
6.500 0.9843 0.01189 0.00511 -0.0221 0.2080 0.9955
6.750 1.0111 0.01208 0.00532 -0.0219 0.2053 0.9955
7.000 1.0376 0.01229 0.00553 -0.0217 0.2024 0.9955
7.250 1.0638 0.01254 0.00577 -0.0215 0.1995 0.9955
7.500 1.0900 0.01278 0.00602 -0.0213 0.1970 0.9955
7.750 1.1167 0.01296 0.00625 -0.0211 0.1948 0.9955
8.000 1.1432 0.01316 0.00648 -0.0209 0.1919 0.9955
8.250 1.1693 0.01339 0.00674 -0.0207 0.1886 0.9955
8.500 1.1949 0.01366 0.00701 -0.0205 0.1853 0.9955
8.750 1.2207 0.01391 0.00729 -0.0202 0.1821 0.9955
9.000 1.2466 0.01412 0.00755 -0.0200 0.1773 0.9955
9.250 1.2718 0.01442 0.00783 -0.0198 0.1716 0.9955
9.500 1.2970 0.01470 0.00814 -0.0195 0.1661 0.9955
9.750 1.3216 0.01503 0.00846 -0.0192 0.1593 0.9955
10.000 1.3457 0.01539 0.00883 -0.0189 0.1524 0.9955
10.250 1.3687 0.01586 0.00926 -0.0184 0.1447 0.9955
10.500 1.3919 0.01629 0.00971 -0.0180 0.1387 0.9955
10.750 1.4138 0.01682 0.01022 -0.0174 0.1336 0.9955
11.000 1.4365 0.01725 0.01071 -0.0169 0.1302 0.9955
11.250 1.4582 0.01775 0.01123 -0.0163 0.1263 0.9955
11.500 1.4784 0.01836 0.01185 -0.0156 0.1223 0.9955
11.750 1.4994 0.01886 0.01241 -0.0150 0.1186 0.9955
12.000 1.5191 0.01945 0.01303 -0.0142 0.1141 0.9955
12.250 1.5368 0.02016 0.01375 -0.0133 0.1104 0.9955
12.500 1.5562 0.02069 0.01436 -0.0125 0.1080 0.9955
12.750 1.5741 0.02130 0.01503 -0.0116 0.1052 0.9955
13.000 1.5895 0.02204 0.01582 -0.0104 0.1020 0.9955
13.250 1.6021 0.02286 0.01668 -0.0089 0.0990 0.9955
13.500 1.6135 0.02363 0.01753 -0.0073 0.0957 0.9955
13.750 1.6207 0.02474 0.01868 -0.0055 0.0914 0.9955
14.000 1.6276 0.02599 0.01999 -0.0042 0.0880 0.9955
14.250 1.6331 0.02750 0.02158 -0.0033 0.0838 0.9955
14.500 1.6342 0.02966 0.02379 -0.0029 0.0796 0.9955
14.750 1.6338 0.03231 0.02652 -0.0032 0.0743 0.9955
15.000 1.6281 0.03598 0.03027 -0.0045 0.0690 0.9955
15.250 1.6164 0.04077 0.03515 -0.0066 0.0639 0.9955
15.500 1.5996 0.04632 0.04080 -0.0089 0.0588 0.9955
15.750 1.5796 0.05220 0.04679 -0.0111 0.0556 0.9955
16.000 1.5576 0.05825 0.05295 -0.0133 0.0530 0.9955
16.250 1.5321 0.06463 0.05944 -0.0154 0.0509 0.9955
16.500 1.5069 0.07096 0.06587 -0.0175 0.0491 0.9955
16.750 1.4835 0.07720 0.07222 -0.0196 0.0476 0.9955
17.000 1.4603 0.08370 0.07882 -0.0220 0.0458 0.9955
17.250 1.4380 0.09031 0.08553 -0.0244 0.0442 0.9955
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