RAF 34 AIRFOIL (raf34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: RAF 34 AIRFOIL (raf34-il) Reynolds number: 1,000,000 Max Cl/Cd: 84.75 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-raf34-il-1000000-n5.txt Download as CSV file: xf-raf34-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: RAF 34 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-18.250 -1.1254 0.08832 0.08581 -0.0272 1.0000 0.0107
-18.000 -1.2447 0.06286 0.05990 -0.0436 1.0000 0.0101
-17.750 -1.2811 0.05257 0.04938 -0.0511 1.0000 0.0100
-17.500 -1.2994 0.04640 0.04304 -0.0552 1.0000 0.0101
-17.250 -1.3101 0.04196 0.03845 -0.0574 1.0000 0.0103
-17.000 -1.3168 0.03848 0.03485 -0.0585 1.0000 0.0104
-16.750 -1.3199 0.03574 0.03199 -0.0588 1.0000 0.0105
-16.500 -1.3199 0.03353 0.02968 -0.0584 1.0000 0.0108
-16.250 -1.3186 0.03163 0.02768 -0.0576 1.0000 0.0110
-16.000 -1.3155 0.03002 0.02596 -0.0564 1.0000 0.0113
-15.750 -1.3110 0.02862 0.02446 -0.0549 1.0000 0.0116
-15.500 -1.3045 0.02742 0.02320 -0.0532 1.0000 0.0120
-15.250 -1.2973 0.02634 0.02204 -0.0514 1.0000 0.0123
-15.000 -1.2875 0.02546 0.02111 -0.0496 1.0000 0.0126
-14.750 -1.2752 0.02477 0.02038 -0.0479 1.0000 0.0132
-14.500 -1.2640 0.02403 0.01958 -0.0459 1.0000 0.0136
-14.250 -1.2537 0.02328 0.01876 -0.0437 1.0000 0.0138
-14.000 -1.2415 0.02267 0.01808 -0.0415 1.0000 0.0142
-13.750 -1.2299 0.02205 0.01739 -0.0392 1.0000 0.0146
-13.500 -1.2183 0.02147 0.01674 -0.0367 1.0000 0.0149
-13.250 -1.2044 0.02093 0.01616 -0.0346 1.0000 0.0152
-13.000 -1.1864 0.02052 0.01573 -0.0331 1.0000 0.0157
-12.750 -1.1676 0.02015 0.01534 -0.0317 1.0000 0.0161
-12.500 -1.1492 0.01974 0.01490 -0.0303 1.0000 0.0165
-12.250 -1.1305 0.01933 0.01444 -0.0289 1.0000 0.0169
-12.000 -1.1111 0.01895 0.01402 -0.0275 1.0000 0.0174
-11.750 -1.0915 0.01858 0.01360 -0.0262 1.0000 0.0178
-11.500 -1.0720 0.01818 0.01315 -0.0248 1.0000 0.0182
-11.250 -1.0524 0.01779 0.01270 -0.0234 1.0000 0.0184
-10.750 -0.9733 0.01658 0.01141 -0.0294 0.9477 0.0195
-10.500 -0.9271 0.01620 0.01087 -0.0337 0.8979 0.0200
-10.250 -0.9059 0.01601 0.01053 -0.0324 0.8640 0.0204
-10.000 -0.8846 0.01578 0.01019 -0.0312 0.8426 0.0208
-9.750 -0.8632 0.01550 0.00981 -0.0300 0.8254 0.0212
-9.500 -0.8409 0.01526 0.00949 -0.0290 0.8104 0.0216
-9.250 -0.8186 0.01496 0.00910 -0.0280 0.7970 0.0220
-9.000 -0.7959 0.01469 0.00873 -0.0271 0.7847 0.0223
-8.750 -0.7724 0.01445 0.00842 -0.0262 0.7731 0.0226
-8.500 -0.7489 0.01420 0.00808 -0.0254 0.7617 0.0228
-8.250 -0.7252 0.01395 0.00776 -0.0246 0.7514 0.0230
-8.000 -0.7046 0.01337 0.00710 -0.0234 0.7407 0.0237
-7.750 -0.6817 0.01299 0.00667 -0.0225 0.7308 0.0241
-7.500 -0.6582 0.01268 0.00630 -0.0216 0.7214 0.0245
-7.250 -0.6340 0.01241 0.00597 -0.0209 0.7116 0.0248
-7.000 -0.6097 0.01217 0.00567 -0.0202 0.7026 0.0252
-6.750 -0.5849 0.01194 0.00539 -0.0196 0.6936 0.0257
-6.500 -0.5603 0.01169 0.00509 -0.0189 0.6856 0.0260
-6.250 -0.5355 0.01146 0.00480 -0.0182 0.6770 0.0264
-6.000 -0.5105 0.01123 0.00453 -0.0176 0.6693 0.0268
-5.750 -0.4853 0.01102 0.00426 -0.0171 0.6616 0.0271
-5.500 -0.4599 0.01083 0.00403 -0.0165 0.6544 0.0275
-5.250 -0.4343 0.01064 0.00380 -0.0160 0.6470 0.0278
-5.000 -0.4087 0.01047 0.00357 -0.0155 0.6403 0.0281
-4.750 -0.3827 0.01032 0.00339 -0.0151 0.6335 0.0283
-4.500 -0.3573 0.01012 0.00314 -0.0145 0.6268 0.0290
-4.250 -0.3315 0.00992 0.00291 -0.0140 0.6207 0.0299
-4.000 -0.3056 0.00976 0.00273 -0.0135 0.6139 0.0307
-3.750 -0.2795 0.00962 0.00257 -0.0131 0.6080 0.0314
-3.500 -0.2532 0.00949 0.00241 -0.0127 0.6014 0.0323
-3.250 -0.2269 0.00938 0.00227 -0.0123 0.5950 0.0332
-3.000 -0.2003 0.00927 0.00215 -0.0120 0.5891 0.0342
-2.750 -0.1737 0.00917 0.00202 -0.0116 0.5826 0.0360
-2.500 -0.1475 0.00905 0.00191 -0.0112 0.5762 0.0399
-2.250 -0.1218 0.00886 0.00178 -0.0107 0.5699 0.0560
-2.000 -0.0967 0.00865 0.00167 -0.0102 0.5633 0.0873
-1.750 -0.0706 0.00850 0.00159 -0.0098 0.5574 0.1065
-1.500 -0.0445 0.00837 0.00152 -0.0094 0.5506 0.1265
-1.000 0.0074 0.00810 0.00138 -0.0085 0.5375 0.1752
-0.750 0.0322 0.00791 0.00132 -0.0079 0.5304 0.2237
-0.500 0.0571 0.00770 0.00127 -0.0073 0.5218 0.2761
-0.250 0.0823 0.00756 0.00123 -0.0068 0.5126 0.3176
0.000 0.1066 0.00739 0.00118 -0.0061 0.5004 0.3698
0.250 0.1295 0.00709 0.00114 -0.0051 0.4909 0.4541
0.500 0.1505 0.00676 0.00111 -0.0038 0.4805 0.5581
0.750 0.1692 0.00640 0.00110 -0.0019 0.4703 0.6685
1.000 0.1890 0.00616 0.00112 0.0000 0.4618 0.7494
1.250 0.2114 0.00606 0.00116 0.0013 0.4527 0.8005
1.500 0.2358 0.00599 0.00120 0.0022 0.4431 0.8406
1.750 0.2627 0.00598 0.00126 0.0026 0.4334 0.8754
2.000 0.2949 0.00602 0.00135 0.0017 0.4233 0.9044
2.250 0.3313 0.00611 0.00145 -0.0001 0.4120 0.9217
2.500 0.3651 0.00623 0.00154 -0.0014 0.4014 0.9320
2.750 0.4024 0.00638 0.00164 -0.0035 0.3903 0.9388
3.000 0.4344 0.00651 0.00174 -0.0044 0.3792 0.9470
3.250 0.4721 0.00667 0.00185 -0.0066 0.3661 0.9510
3.500 0.5015 0.00683 0.00197 -0.0069 0.3552 0.9575
3.750 0.5311 0.00700 0.00209 -0.0073 0.3435 0.9616
4.000 0.5634 0.00716 0.00221 -0.0083 0.3319 0.9636
4.250 0.5945 0.00732 0.00234 -0.0091 0.3215 0.9661
4.500 0.6223 0.00753 0.00249 -0.0092 0.3056 0.9699
4.750 0.6492 0.00778 0.00265 -0.0091 0.2862 0.9735
5.000 0.6813 0.00806 0.00283 -0.0102 0.2648 0.9750
5.250 0.7119 0.00840 0.00305 -0.0111 0.2381 0.9769
5.500 0.7407 0.00876 0.00329 -0.0116 0.2105 0.9793
5.750 0.7653 0.00921 0.00357 -0.0112 0.1793 0.9828
6.000 0.7924 0.00971 0.00391 -0.0115 0.1441 0.9848
6.250 0.8229 0.01006 0.00418 -0.0125 0.1285 0.9860
6.500 0.8531 0.01036 0.00443 -0.0133 0.1183 0.9873
6.750 0.8829 0.01063 0.00468 -0.0140 0.1116 0.9889
7.000 0.9121 0.01088 0.00492 -0.0146 0.1050 0.9906
7.250 0.9403 0.01116 0.00518 -0.0149 0.0979 0.9923
7.500 0.9675 0.01145 0.00546 -0.0151 0.0900 0.9939
7.750 0.9935 0.01229 0.00602 -0.0156 0.0500 0.9954
8.000 1.0217 0.01274 0.00643 -0.0163 0.0409 0.9968
8.250 1.0503 0.01311 0.00679 -0.0169 0.0367 0.9981
8.500 1.0787 0.01350 0.00718 -0.0175 0.0329 0.9992
8.750 1.1062 0.01385 0.00754 -0.0179 0.0306 1.0000
9.000 1.1230 0.01423 0.00792 -0.0161 0.0285 1.0000
9.250 1.1400 0.01458 0.00828 -0.0143 0.0269 1.0000
9.500 1.1567 0.01492 0.00865 -0.0125 0.0252 1.0000
9.750 1.1722 0.01532 0.00906 -0.0105 0.0237 1.0000
10.000 1.1866 0.01574 0.00948 -0.0083 0.0219 1.0000
10.250 1.2013 0.01612 0.00990 -0.0062 0.0207 1.0000
10.500 1.2143 0.01657 0.01035 -0.0038 0.0191 1.0000
10.750 1.2254 0.01706 0.01086 -0.0012 0.0177 1.0000
11.000 1.2320 0.01749 0.01131 0.0023 0.0168 1.0000
11.250 1.2372 0.01794 0.01180 0.0060 0.0161 1.0000
11.500 1.2433 0.01852 0.01240 0.0092 0.0151 1.0000
11.750 1.2498 0.01922 0.01313 0.0119 0.0141 1.0000
12.000 1.2582 0.01997 0.01393 0.0141 0.0135 1.0000
12.250 1.2673 0.02081 0.01481 0.0159 0.0129 1.0000
12.500 1.2760 0.02177 0.01582 0.0175 0.0123 1.0000
12.750 1.2846 0.02285 0.01694 0.0189 0.0119 1.0000
13.000 1.2920 0.02410 0.01823 0.0201 0.0113 1.0000
13.250 1.3000 0.02538 0.01957 0.0211 0.0110 1.0000
13.500 1.3078 0.02677 0.02101 0.0220 0.0106 1.0000
13.750 1.3158 0.02819 0.02249 0.0228 0.0102 1.0000
14.000 1.3224 0.02978 0.02415 0.0234 0.0100 1.0000
14.250 1.3289 0.03144 0.02586 0.0239 0.0096 1.0000
14.500 1.3343 0.03324 0.02772 0.0244 0.0092 1.0000
14.750 1.3381 0.03524 0.02979 0.0247 0.0090 1.0000
15.000 1.3415 0.03733 0.03193 0.0250 0.0088 1.0000
15.250 1.3435 0.03960 0.03427 0.0252 0.0086 1.0000
15.500 1.3428 0.04220 0.03694 0.0252 0.0082 1.0000
15.750 1.3441 0.04464 0.03945 0.0252 0.0081 1.0000
16.000 1.3452 0.04718 0.04207 0.0250 0.0080 1.0000
16.250 1.3453 0.04991 0.04489 0.0247 0.0079 1.0000
16.500 1.3448 0.05279 0.04785 0.0243 0.0077 1.0000
16.750 1.3432 0.05590 0.05104 0.0237 0.0076 1.0000
17.000 1.3419 0.05903 0.05425 0.0230 0.0074 1.0000
17.250 1.3379 0.06255 0.05785 0.0222 0.0073 1.0000
17.500 1.3333 0.06625 0.06164 0.0212 0.0071 1.0000
17.750 1.3279 0.07014 0.06562 0.0201 0.0072 1.0000
18.000 1.3227 0.07404 0.06960 0.0189 0.0070 1.0000
18.250 1.3168 0.07812 0.07376 0.0175 0.0068 1.0000
18.500 1.3082 0.08267 0.07840 0.0160 0.0067 1.0000
18.750 1.3002 0.08720 0.08301 0.0143 0.0067 1.0000
19.000 1.2908 0.09199 0.08789 0.0126 0.0066 1.0000
19.250 1.2796 0.09714 0.09313 0.0106 0.0065 1.0000
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