TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il) Reynolds number: 1,000,000 Max Cl/Cd: 112.09 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tsagi-r-3a-il-1000000.txt Download as CSV file: xf-tsagi-r-3a-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.750 -0.3941 0.08891 0.08748 -0.0018 1.0045 0.0188
-9.500 -0.3907 0.08547 0.08405 -0.0028 0.9773 0.0189
-9.250 -0.3929 0.08284 0.08097 -0.0021 0.8061 0.0190
-9.000 -0.3918 0.07959 0.07742 -0.0030 0.7201 0.0191
-8.750 -0.3918 0.07568 0.07333 -0.0045 0.6645 0.0193
-8.500 -0.3929 0.07151 0.06902 -0.0064 0.6201 0.0194
-8.250 -0.6177 0.02871 0.02573 -0.0337 1.0045 0.0153
-8.000 -0.6032 0.02231 0.01862 -0.0347 0.9707 0.0145
-7.750 -0.5854 0.01982 0.01563 -0.0333 0.9028 0.0144
-7.500 -0.5665 0.01871 0.01407 -0.0315 0.8232 0.0145
-7.250 -0.5444 0.01764 0.01251 -0.0305 0.7381 0.0145
-7.000 -0.5206 0.01669 0.01109 -0.0298 0.6551 0.0145
-6.750 -0.4954 0.01593 0.00998 -0.0293 0.5875 0.0146
-6.500 -0.4694 0.01528 0.00905 -0.0289 0.5422 0.0147
-6.250 -0.4429 0.01469 0.00825 -0.0285 0.5096 0.0149
-6.000 -0.4160 0.01416 0.00756 -0.0282 0.4863 0.0151
-5.750 -0.3888 0.01369 0.00696 -0.0278 0.4691 0.0153
-5.500 -0.3613 0.01329 0.00645 -0.0275 0.4574 0.0155
-5.250 -0.3335 0.01295 0.00602 -0.0273 0.4497 0.0157
-5.000 -0.3070 0.01224 0.00521 -0.0269 0.4429 0.0160
-4.750 -0.2796 0.01181 0.00472 -0.0266 0.4374 0.0164
-4.500 -0.2517 0.01147 0.00436 -0.0264 0.4331 0.0167
-4.250 -0.2237 0.01120 0.00405 -0.0262 0.4287 0.0171
-4.000 -0.1955 0.01097 0.00377 -0.0260 0.4247 0.0175
-3.750 -0.1673 0.01075 0.00351 -0.0258 0.4207 0.0180
-3.500 -0.1388 0.01053 0.00326 -0.0256 0.4178 0.0184
-3.250 -0.1105 0.01028 0.00299 -0.0254 0.4145 0.0191
-3.000 -0.0820 0.01010 0.00279 -0.0253 0.4112 0.0203
-2.750 -0.0535 0.00998 0.00264 -0.0251 0.4074 0.0217
-2.500 -0.0250 0.00986 0.00252 -0.0250 0.4035 0.0244
-2.250 0.0038 0.00971 0.00240 -0.0249 0.4010 0.0298
-2.000 0.0325 0.00957 0.00229 -0.0247 0.3976 0.0376
-1.750 0.0611 0.00946 0.00218 -0.0247 0.3938 0.0436
-1.500 0.0898 0.00937 0.00209 -0.0246 0.3900 0.0499
-1.250 0.1183 0.00926 0.00201 -0.0245 0.3860 0.0624
-1.000 0.1467 0.00903 0.00194 -0.0244 0.3831 0.1014
-0.750 0.1753 0.00886 0.00188 -0.0244 0.3791 0.1327
-0.500 0.2038 0.00871 0.00183 -0.0243 0.3744 0.1723
-0.250 0.2317 0.00848 0.00179 -0.0243 0.3692 0.2441
0.000 0.2592 0.00801 0.00174 -0.0243 0.3647 0.3779
0.250 0.2850 0.00736 0.00172 -0.0240 0.3584 0.5888
0.500 0.3100 0.00690 0.00174 -0.0232 0.3514 0.7503
0.750 0.3339 0.00661 0.00178 -0.0220 0.3427 0.8609
1.000 0.3589 0.00654 0.00180 -0.0208 0.3312 0.9206
1.250 0.3905 0.00661 0.00182 -0.0212 0.3110 0.9591
1.500 0.4297 0.00681 0.00187 -0.0235 0.2869 0.9811
1.750 0.4700 0.00702 0.00195 -0.0260 0.2727 0.9914
2.000 0.5066 0.00719 0.00203 -0.0277 0.2647 0.9955
2.250 0.5327 0.00734 0.00211 -0.0273 0.2583 0.9955
2.500 0.5593 0.00743 0.00217 -0.0269 0.2545 0.9955
2.750 0.5859 0.00756 0.00225 -0.0265 0.2503 0.9955
3.000 0.6124 0.00772 0.00236 -0.0261 0.2458 0.9955
3.250 0.6392 0.00786 0.00246 -0.0257 0.2423 0.9955
3.500 0.6664 0.00795 0.00254 -0.0255 0.2398 0.9955
3.750 0.6937 0.00806 0.00263 -0.0252 0.2372 0.9955
4.000 0.7209 0.00820 0.00273 -0.0250 0.2344 0.9955
4.250 0.7481 0.00836 0.00286 -0.0248 0.2313 0.9955
4.500 0.7751 0.00856 0.00302 -0.0245 0.2279 0.9955
4.750 0.8027 0.00866 0.00313 -0.0244 0.2266 0.9955
5.000 0.8304 0.00877 0.00324 -0.0243 0.2251 0.9955
5.250 0.8580 0.00889 0.00337 -0.0241 0.2234 0.9955
5.500 0.8855 0.00903 0.00349 -0.0240 0.2214 0.9955
5.750 0.9129 0.00918 0.00363 -0.0239 0.2190 0.9955
6.000 0.9400 0.00936 0.00380 -0.0237 0.2163 0.9955
6.250 0.9667 0.00961 0.00402 -0.0235 0.2130 0.9955
6.500 0.9942 0.00974 0.00416 -0.0234 0.2116 0.9955
6.750 1.0218 0.00985 0.00430 -0.0234 0.2101 0.9955
7.000 1.0493 0.00998 0.00445 -0.0233 0.2081 0.9955
7.250 1.0766 0.01012 0.00460 -0.0232 0.2059 0.9955
7.500 1.1036 0.01029 0.00477 -0.0231 0.2033 0.9955
7.750 1.1302 0.01052 0.00499 -0.0229 0.2000 0.9955
8.000 1.1570 0.01071 0.00518 -0.0228 0.1967 0.9955
8.250 1.1845 0.01080 0.00531 -0.0228 0.1940 0.9955
8.500 1.2116 0.01095 0.00546 -0.0227 0.1902 0.9955
8.750 1.2380 0.01117 0.00567 -0.0225 0.1857 0.9955
9.000 1.2646 0.01135 0.00587 -0.0224 0.1818 0.9955
9.250 1.2913 0.01152 0.00603 -0.0223 0.1761 0.9955
9.500 1.3171 0.01179 0.00627 -0.0221 0.1696 0.9955
9.750 1.3431 0.01201 0.00650 -0.0220 0.1630 0.9955
10.000 1.3682 0.01234 0.00679 -0.0217 0.1551 0.9955
10.250 1.3925 0.01273 0.00714 -0.0214 0.1467 0.9955
10.500 1.4170 0.01310 0.00749 -0.0211 0.1406 0.9955
10.750 1.4406 0.01353 0.00790 -0.0207 0.1350 0.9955
11.000 1.4648 0.01389 0.00828 -0.0204 0.1312 0.9955
11.250 1.4883 0.01429 0.00869 -0.0200 0.1270 0.9955
11.500 1.5106 0.01479 0.00918 -0.0195 0.1223 0.9955
11.750 1.5344 0.01512 0.00956 -0.0191 0.1199 0.9955
12.000 1.5576 0.01550 0.00997 -0.0186 0.1169 0.9955
12.250 1.5793 0.01598 0.01046 -0.0181 0.1133 0.9955
12.500 1.6007 0.01648 0.01098 -0.0175 0.1098 0.9955
12.750 1.6230 0.01686 0.01140 -0.0169 0.1068 0.9955
13.000 1.6428 0.01743 0.01196 -0.0162 0.1021 0.9955
13.250 1.6626 0.01796 0.01253 -0.0154 0.0980 0.9955
13.500 1.6813 0.01855 0.01312 -0.0146 0.0932 0.9955
13.750 1.6982 0.01923 0.01381 -0.0135 0.0881 0.9955
14.000 1.7118 0.02009 0.01465 -0.0122 0.0808 0.9955
14.250 1.7196 0.02116 0.01568 -0.0101 0.0715 0.9955
14.500 1.7138 0.02289 0.01735 -0.0068 0.0581 0.9955
14.750 1.7006 0.02550 0.01994 -0.0042 0.0464 0.9955
15.000 1.6887 0.02873 0.02321 -0.0034 0.0398 0.9955
15.250 1.6790 0.03255 0.02712 -0.0043 0.0357 0.9955
15.500 1.6673 0.03725 0.03192 -0.0063 0.0325 0.9955
15.750 1.6509 0.04285 0.03765 -0.0088 0.0300 0.9955
16.000 1.6334 0.04853 0.04345 -0.0111 0.0283 0.9955
16.250 1.6097 0.05486 0.04991 -0.0133 0.0267 0.9955
16.750 1.5589 0.06762 0.06291 -0.0174 0.0253 0.9955
17.000 1.5318 0.07421 0.06962 -0.0196 0.0245 0.9955
17.250 1.5061 0.08098 0.07650 -0.0220 0.0233 0.9955
|
Polar data table (+)
Polar graphs
<< Back to TsAGI R-3a (12%) (tsagi-r-3a-il)