TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il) Reynolds number: 1,000,000 Max Cl/Cd: 108.91 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tsagi-r-3a-il-1000000-n5.txt Download as CSV file: xf-tsagi-r-3a-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.9542 0.04099 0.03852 -0.0361 1.0045 0.0090
-12.000 -0.9627 0.03592 0.03314 -0.0373 1.0045 0.0090
-11.750 -0.9578 0.03265 0.02962 -0.0373 1.0045 0.0090
-11.500 -0.9464 0.03019 0.02696 -0.0371 1.0045 0.0091
-11.250 -0.9308 0.02829 0.02488 -0.0366 1.0045 0.0091
-11.000 -0.9132 0.02661 0.02304 -0.0362 1.0045 0.0092
-10.750 -0.8940 0.02513 0.02140 -0.0357 1.0045 0.0093
-10.500 -0.8734 0.02381 0.01995 -0.0352 1.0045 0.0094
-10.250 -0.8520 0.02258 0.01858 -0.0347 1.0045 0.0095
-10.000 -0.8245 0.02130 0.01713 -0.0354 0.9607 0.0096
-9.750 -0.8053 0.02042 0.01597 -0.0338 0.8909 0.0096
-9.500 -0.7850 0.01968 0.01489 -0.0325 0.8235 0.0097
-9.250 -0.7623 0.01898 0.01388 -0.0317 0.7603 0.0098
-9.000 -0.7383 0.01834 0.01294 -0.0312 0.6998 0.0099
-8.750 -0.7136 0.01775 0.01207 -0.0307 0.6433 0.0099
-8.500 -0.6882 0.01721 0.01129 -0.0303 0.5951 0.0100
-8.250 -0.6624 0.01670 0.01057 -0.0300 0.5564 0.0101
-8.000 -0.6363 0.01622 0.00992 -0.0296 0.5270 0.0102
-7.750 -0.6098 0.01577 0.00932 -0.0293 0.5040 0.0103
-7.500 -0.5830 0.01535 0.00877 -0.0290 0.4840 0.0104
-7.250 -0.5560 0.01498 0.00827 -0.0287 0.4642 0.0104
-7.000 -0.5301 0.01430 0.00746 -0.0284 0.4485 0.0106
-6.750 -0.5032 0.01385 0.00691 -0.0281 0.4369 0.0108
-6.500 -0.4759 0.01347 0.00646 -0.0278 0.4299 0.0110
-6.000 -0.4207 0.01282 0.00570 -0.0273 0.4181 0.0113
-5.750 -0.3929 0.01253 0.00535 -0.0271 0.4130 0.0115
-5.500 -0.3651 0.01225 0.00502 -0.0269 0.4089 0.0117
-5.000 -0.3090 0.01173 0.00442 -0.0265 0.4019 0.0121
-4.750 -0.2808 0.01149 0.00415 -0.0263 0.3991 0.0123
-4.500 -0.2526 0.01127 0.00389 -0.0261 0.3962 0.0125
-4.250 -0.2243 0.01107 0.00365 -0.0259 0.3929 0.0127
-4.000 -0.1959 0.01090 0.00344 -0.0257 0.3895 0.0129
-3.750 -0.1676 0.01068 0.00319 -0.0256 0.3864 0.0133
-3.500 -0.1392 0.01047 0.00297 -0.0254 0.3842 0.0138
-3.250 -0.1107 0.01030 0.00279 -0.0253 0.3810 0.0144
-3.000 -0.0821 0.01015 0.00262 -0.0252 0.3778 0.0150
-2.750 -0.0535 0.01003 0.00247 -0.0250 0.3743 0.0156
-2.500 -0.0249 0.00991 0.00233 -0.0249 0.3703 0.0166
-2.250 0.0038 0.00978 0.00220 -0.0248 0.3669 0.0181
-2.000 0.0324 0.00964 0.00210 -0.0247 0.3624 0.0236
-1.750 0.0611 0.00957 0.00202 -0.0246 0.3569 0.0304
-1.500 0.0899 0.00951 0.00195 -0.0245 0.3519 0.0341
-1.250 0.1186 0.00943 0.00187 -0.0245 0.3467 0.0378
-1.000 0.1473 0.00937 0.00180 -0.0244 0.3395 0.0424
-0.750 0.1760 0.00931 0.00174 -0.0244 0.3322 0.0497
-0.500 0.2044 0.00919 0.00168 -0.0243 0.3202 0.0764
-0.250 0.2327 0.00916 0.00165 -0.0243 0.3011 0.1013
0.000 0.2609 0.00919 0.00165 -0.0242 0.2810 0.1236
0.250 0.2890 0.00912 0.00166 -0.0242 0.2700 0.1658
0.500 0.3167 0.00895 0.00168 -0.0241 0.2621 0.2452
0.750 0.3443 0.00868 0.00170 -0.0241 0.2566 0.3551
1.000 0.3718 0.00844 0.00173 -0.0241 0.2519 0.4593
1.250 0.3992 0.00825 0.00178 -0.0239 0.2472 0.5541
1.500 0.4259 0.00800 0.00185 -0.0236 0.2429 0.6701
1.750 0.4519 0.00776 0.00192 -0.0231 0.2401 0.7734
2.000 0.4766 0.00759 0.00200 -0.0221 0.2367 0.8593
2.250 0.5011 0.00753 0.00209 -0.0209 0.2330 0.9327
2.500 0.5468 0.00764 0.00219 -0.0244 0.2276 0.9880
2.750 0.5848 0.00773 0.00225 -0.0264 0.2251 0.9955
3.000 0.6116 0.00783 0.00232 -0.0261 0.2224 0.9955
3.250 0.6385 0.00794 0.00239 -0.0258 0.2197 0.9955
3.500 0.6655 0.00807 0.00248 -0.0255 0.2166 0.9955
3.750 0.6926 0.00821 0.00258 -0.0252 0.2134 0.9955
4.000 0.7200 0.00832 0.00267 -0.0250 0.2116 0.9955
4.250 0.7475 0.00842 0.00277 -0.0248 0.2100 0.9955
4.500 0.7750 0.00853 0.00287 -0.0246 0.2083 0.9955
4.750 0.8026 0.00865 0.00297 -0.0245 0.2065 0.9955
5.000 0.8301 0.00878 0.00309 -0.0243 0.2046 0.9955
5.250 0.8576 0.00892 0.00321 -0.0242 0.2026 0.9955
5.500 0.8849 0.00908 0.00335 -0.0241 0.2003 0.9955
5.750 0.9122 0.00925 0.00350 -0.0239 0.1977 0.9955
6.000 0.9399 0.00936 0.00363 -0.0238 0.1963 0.9955
6.250 0.9674 0.00948 0.00376 -0.0237 0.1944 0.9955
6.500 0.9949 0.00962 0.00390 -0.0236 0.1923 0.9955
6.750 1.0222 0.00977 0.00405 -0.0235 0.1898 0.9955
7.000 1.0493 0.00994 0.00421 -0.0234 0.1870 0.9955
7.250 1.0763 0.01014 0.00439 -0.0233 0.1840 0.9955
7.500 1.1036 0.01028 0.00456 -0.0232 0.1820 0.9955
7.750 1.1307 0.01044 0.00473 -0.0231 0.1789 0.9955
8.000 1.1574 0.01065 0.00491 -0.0230 0.1729 0.9955
8.250 1.1839 0.01087 0.00512 -0.0228 0.1672 0.9955
8.500 1.2100 0.01113 0.00534 -0.0227 0.1590 0.9955
8.750 1.2359 0.01142 0.00560 -0.0225 0.1511 0.9955
9.000 1.2611 0.01177 0.00590 -0.0222 0.1427 0.9955
9.500 1.3110 0.01250 0.00658 -0.0217 0.1289 0.9955
9.750 1.3356 0.01287 0.00693 -0.0214 0.1241 0.9955
10.000 1.3604 0.01321 0.00728 -0.0211 0.1202 0.9955
10.250 1.3851 0.01354 0.00762 -0.0208 0.1162 0.9955
10.500 1.4088 0.01397 0.00803 -0.0204 0.1116 0.9955
10.750 1.4332 0.01430 0.00839 -0.0201 0.1086 0.9955
11.000 1.4573 0.01464 0.00875 -0.0197 0.1058 0.9955
11.250 1.4802 0.01509 0.00919 -0.0193 0.1016 0.9955
11.500 1.5032 0.01551 0.00962 -0.0188 0.0978 0.9955
11.750 1.5260 0.01592 0.01005 -0.0184 0.0943 0.9955
12.000 1.5473 0.01645 0.01058 -0.0177 0.0900 0.9955
12.250 1.5692 0.01689 0.01104 -0.0172 0.0862 0.9955
12.500 1.5886 0.01754 0.01167 -0.0164 0.0802 0.9955
12.750 1.6058 0.01831 0.01241 -0.0154 0.0715 0.9955
13.000 1.6123 0.01987 0.01383 -0.0133 0.0516 0.9955
13.250 1.6138 0.02162 0.01552 -0.0108 0.0379 0.9955
13.500 1.6161 0.02289 0.01681 -0.0081 0.0327 0.9955
13.750 1.6183 0.02429 0.01825 -0.0060 0.0288 0.9955
14.000 1.6160 0.02628 0.02029 -0.0044 0.0231 0.9955
14.250 1.5987 0.03029 0.02434 -0.0042 0.0136 0.9955
14.500 1.5916 0.03416 0.02832 -0.0056 0.0116 0.9955
14.750 1.5855 0.03841 0.03269 -0.0076 0.0110 0.9955
15.000 1.5760 0.04323 0.03764 -0.0099 0.0105 0.9955
15.250 1.5625 0.04850 0.04304 -0.0120 0.0103 0.9955
15.500 1.5444 0.05420 0.04887 -0.0141 0.0101 0.9955
15.750 1.5236 0.06014 0.05494 -0.0161 0.0100 0.9955
16.000 1.5016 0.06612 0.06103 -0.0180 0.0100 0.9955
16.250 1.4768 0.07248 0.06752 -0.0201 0.0099 0.9955
16.500 1.4541 0.07880 0.07397 -0.0223 0.0099 0.9955
16.750 1.4335 0.08507 0.08034 -0.0245 0.0098 0.9955
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