RAF 30 AIRFOIL (raf30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: RAF 30 AIRFOIL (raf30-il) Reynolds number: 1,000,000 Max Cl/Cd: 69.51 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-raf30-il-1000000.txt Download as CSV file: xf-raf30-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: RAF 30 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1479 0.10707 0.10413 -0.0132 1.0000 0.0126
-19.000 -1.1674 0.09996 0.09691 -0.0168 1.0000 0.0126
-18.750 -1.1868 0.09295 0.08979 -0.0203 1.0000 0.0127
-18.500 -1.1997 0.08710 0.08386 -0.0233 1.0000 0.0129
-18.250 -1.2109 0.08156 0.07823 -0.0261 1.0000 0.0130
-18.000 -1.2266 0.07549 0.07205 -0.0290 1.0000 0.0131
-17.750 -1.2428 0.06959 0.06602 -0.0318 1.0000 0.0130
-17.500 -1.2510 0.06489 0.06123 -0.0340 1.0000 0.0132
-17.250 -1.2528 0.06120 0.05747 -0.0357 1.0000 0.0134
-17.000 -1.2577 0.05724 0.05341 -0.0374 1.0000 0.0136
-16.750 -1.2638 0.05329 0.04935 -0.0389 1.0000 0.0137
-16.500 -1.2643 0.05016 0.04614 -0.0401 1.0000 0.0139
-16.250 -1.2677 0.04680 0.04268 -0.0411 1.0000 0.0141
-16.000 -1.2606 0.04470 0.04051 -0.0417 1.0000 0.0145
-15.750 -1.2627 0.04169 0.03739 -0.0423 1.0000 0.0146
-15.500 -1.2574 0.03956 0.03517 -0.0426 1.0000 0.0148
-15.250 -1.2551 0.03719 0.03270 -0.0428 1.0000 0.0150
-15.000 -1.2516 0.03506 0.03047 -0.0427 1.0000 0.0153
-14.750 -1.2566 0.03224 0.02754 -0.0422 1.0000 0.0155
-14.500 -1.2531 0.03036 0.02561 -0.0417 1.0000 0.0159
-14.250 -1.2451 0.02894 0.02414 -0.0410 1.0000 0.0162
-14.000 -1.2339 0.02786 0.02301 -0.0403 1.0000 0.0165
-13.750 -1.2226 0.02684 0.02194 -0.0395 1.0000 0.0169
-13.500 -1.2140 0.02566 0.02070 -0.0382 1.0000 0.0172
-13.250 -1.2015 0.02485 0.01983 -0.0371 1.0000 0.0176
-13.000 -1.1885 0.02411 0.01902 -0.0359 1.0000 0.0181
-12.750 -1.1748 0.02346 0.01831 -0.0346 1.0000 0.0184
-12.500 -1.1628 0.02274 0.01752 -0.0329 1.0000 0.0187
-12.250 -1.1631 0.02134 0.01604 -0.0296 1.0000 0.0192
-12.000 -1.1538 0.02063 0.01531 -0.0272 1.0000 0.0198
-11.750 -1.1432 0.02005 0.01470 -0.0247 1.0000 0.0201
-11.500 -1.1311 0.01963 0.01425 -0.0223 1.0000 0.0206
-11.250 -1.1191 0.01923 0.01382 -0.0197 1.0000 0.0211
-11.000 -1.1060 0.01875 0.01329 -0.0173 1.0000 0.0216
-10.750 -1.0890 0.01839 0.01289 -0.0156 1.0000 0.0222
-10.500 -1.0724 0.01801 0.01247 -0.0137 1.0000 0.0225
-10.250 -1.0555 0.01764 0.01205 -0.0119 1.0000 0.0228
-10.000 -1.0498 0.01658 0.01094 -0.0083 1.0000 0.0238
-9.750 -1.0344 0.01609 0.01044 -0.0063 1.0000 0.0245
-9.500 -1.0175 0.01569 0.01002 -0.0044 1.0000 0.0251
-9.250 -1.0003 0.01531 0.00961 -0.0025 1.0000 0.0257
-9.000 -0.9830 0.01493 0.00920 -0.0006 1.0000 0.0264
-8.750 -0.9650 0.01461 0.00885 0.0012 1.0000 0.0270
-8.500 -0.9459 0.01436 0.00858 0.0028 1.0000 0.0275
-8.250 -0.9308 0.01388 0.00805 0.0051 1.0000 0.0280
-8.000 -0.9181 0.01327 0.00740 0.0078 1.0000 0.0290
-7.750 -0.8923 0.01284 0.00697 0.0079 0.9991 0.0301
-7.500 -0.8579 0.01246 0.00657 0.0062 0.9971 0.0312
-7.250 -0.8232 0.01210 0.00619 0.0045 0.9949 0.0322
-7.000 -0.7892 0.01178 0.00584 0.0030 0.9925 0.0331
-6.750 -0.7570 0.01135 0.00538 0.0018 0.9889 0.0345
-6.500 -0.7233 0.01092 0.00495 0.0004 0.9856 0.0364
-6.250 -0.6879 0.01058 0.00461 -0.0014 0.9831 0.0383
-6.000 -0.6578 0.01029 0.00430 -0.0020 0.9770 0.0400
-5.750 -0.6248 0.00989 0.00394 -0.0032 0.9722 0.0456
-5.500 -0.5950 0.00932 0.00355 -0.0039 0.9647 0.0724
-5.250 -0.5602 0.00877 0.00320 -0.0057 0.9580 0.1122
-5.000 -0.5250 0.00836 0.00292 -0.0075 0.9486 0.1399
-4.750 -0.4892 0.00787 0.00261 -0.0095 0.9369 0.1822
-4.500 -0.4576 0.00741 0.00234 -0.0106 0.9198 0.2352
-4.250 -0.4298 0.00713 0.00216 -0.0106 0.9010 0.2728
-4.000 -0.4039 0.00695 0.00201 -0.0102 0.8832 0.3000
-3.750 -0.3794 0.00677 0.00188 -0.0095 0.8664 0.3284
-3.500 -0.3550 0.00661 0.00176 -0.0087 0.8509 0.3547
-3.250 -0.3311 0.00643 0.00165 -0.0079 0.8358 0.3873
-3.000 -0.3075 0.00626 0.00155 -0.0069 0.8190 0.4231
-2.750 -0.2836 0.00612 0.00146 -0.0060 0.8017 0.4560
-2.500 -0.2590 0.00602 0.00139 -0.0053 0.7860 0.4818
-2.250 -0.2336 0.00595 0.00133 -0.0047 0.7729 0.5053
-2.000 -0.2086 0.00586 0.00129 -0.0040 0.7601 0.5313
-1.750 -0.1832 0.00579 0.00125 -0.0033 0.7472 0.5552
-1.500 -0.1570 0.00575 0.00122 -0.0029 0.7346 0.5710
-1.250 -0.1312 0.00571 0.00119 -0.0023 0.7224 0.5895
-1.000 -0.1055 0.00567 0.00117 -0.0017 0.7104 0.6096
-0.500 -0.0531 0.00563 0.00115 -0.0008 0.6862 0.6392
-0.250 -0.0264 0.00563 0.00114 -0.0004 0.6746 0.6514
0.000 0.0000 0.00563 0.00114 0.0000 0.6630 0.6629
0.250 0.0264 0.00563 0.00114 0.0004 0.6514 0.6745
0.500 0.0531 0.00563 0.00115 0.0008 0.6397 0.6862
1.000 0.1055 0.00567 0.00117 0.0017 0.6101 0.7103
1.250 0.1311 0.00571 0.00119 0.0023 0.5893 0.7225
1.500 0.1570 0.00575 0.00122 0.0029 0.5711 0.7347
1.750 0.1832 0.00579 0.00125 0.0033 0.5553 0.7473
2.000 0.2086 0.00586 0.00129 0.0040 0.5317 0.7601
2.500 0.2590 0.00602 0.00139 0.0053 0.4819 0.7860
2.750 0.2836 0.00612 0.00146 0.0060 0.4563 0.8018
3.000 0.3074 0.00626 0.00155 0.0070 0.4231 0.8191
3.250 0.3311 0.00643 0.00165 0.0079 0.3879 0.8358
3.500 0.3550 0.00661 0.00176 0.0087 0.3544 0.8509
3.750 0.3794 0.00677 0.00188 0.0095 0.3287 0.8665
4.000 0.4039 0.00695 0.00201 0.0102 0.3000 0.8831
4.250 0.4298 0.00713 0.00216 0.0107 0.2722 0.9010
4.500 0.4575 0.00742 0.00235 0.0106 0.2342 0.9199
4.750 0.4891 0.00789 0.00262 0.0095 0.1798 0.9370
5.000 0.5251 0.00836 0.00292 0.0075 0.1399 0.9487
5.250 0.5603 0.00877 0.00320 0.0057 0.1114 0.9582
5.500 0.5950 0.00933 0.00355 0.0039 0.0712 0.9647
5.750 0.6248 0.00990 0.00394 0.0032 0.0453 0.9722
6.000 0.6578 0.01029 0.00430 0.0020 0.0400 0.9770
6.250 0.6880 0.01058 0.00462 0.0014 0.0383 0.9832
6.500 0.7234 0.01093 0.00496 -0.0004 0.0364 0.9857
6.750 0.7570 0.01136 0.00539 -0.0018 0.0344 0.9889
7.000 0.7893 0.01178 0.00585 -0.0030 0.0331 0.9925
7.250 0.8233 0.01210 0.00619 -0.0045 0.0322 0.9949
7.500 0.8581 0.01246 0.00657 -0.0062 0.0312 0.9972
7.750 0.8925 0.01284 0.00697 -0.0079 0.0301 0.9991
8.000 0.9179 0.01328 0.00741 -0.0078 0.0290 1.0000
8.250 0.9312 0.01385 0.00802 -0.0052 0.0281 1.0000
8.500 0.9458 0.01437 0.00859 -0.0028 0.0275 1.0000
8.750 0.9644 0.01465 0.00889 -0.0011 0.0270 1.0000
9.000 0.9826 0.01496 0.00923 0.0007 0.0264 1.0000
9.250 1.0004 0.01531 0.00961 0.0025 0.0257 1.0000
9.500 1.0174 0.01570 0.01003 0.0044 0.0251 1.0000
9.750 1.0343 0.01610 0.01045 0.0063 0.0245 1.0000
10.000 1.0498 0.01658 0.01095 0.0084 0.0239 1.0000
10.250 1.0599 0.01738 0.01178 0.0112 0.0231 1.0000
10.500 1.0722 0.01803 0.01249 0.0138 0.0226 1.0000
10.750 1.0893 0.01838 0.01288 0.0155 0.0222 1.0000
11.000 1.1065 0.01873 0.01327 0.0172 0.0216 1.0000
11.250 1.1203 0.01919 0.01377 0.0195 0.0211 1.0000
11.500 1.1317 0.01961 0.01423 0.0222 0.0206 1.0000
11.750 1.1430 0.02008 0.01474 0.0247 0.0202 1.0000
12.000 1.1545 0.02061 0.01529 0.0271 0.0198 1.0000
12.250 1.1647 0.02127 0.01598 0.0294 0.0193 1.0000
12.500 1.1651 0.02262 0.01739 0.0326 0.0186 1.0000
12.750 1.1785 0.02325 0.01809 0.0341 0.0184 1.0000
13.000 1.1913 0.02396 0.01887 0.0356 0.0181 1.0000
13.250 1.2046 0.02468 0.01965 0.0368 0.0176 1.0000
13.500 1.2147 0.02567 0.02071 0.0381 0.0172 1.0000
13.750 1.2253 0.02669 0.02179 0.0392 0.0169 1.0000
14.000 1.2380 0.02761 0.02274 0.0400 0.0165 1.0000
14.250 1.2464 0.02892 0.02411 0.0408 0.0162 1.0000
14.500 1.2558 0.03022 0.02545 0.0414 0.0157 1.0000
14.750 1.2577 0.03226 0.02756 0.0420 0.0155 1.0000
15.000 1.2478 0.03555 0.03097 0.0426 0.0151 1.0000
15.250 1.2595 0.03690 0.03240 0.0425 0.0149 1.0000
15.500 1.2628 0.03916 0.03476 0.0424 0.0148 1.0000
15.750 1.2642 0.04170 0.03740 0.0420 0.0146 1.0000
16.000 1.2685 0.04402 0.03981 0.0415 0.0143 1.0000
16.250 1.2662 0.04716 0.04305 0.0407 0.0142 1.0000
16.500 1.2650 0.05028 0.04628 0.0398 0.0139 1.0000
16.750 1.2640 0.05349 0.04957 0.0386 0.0137 1.0000
17.000 1.2597 0.05722 0.05339 0.0371 0.0136 1.0000
17.250 1.2520 0.06154 0.05782 0.0353 0.0135 1.0000
17.500 1.2442 0.06608 0.06245 0.0332 0.0133 1.0000
17.750 1.2459 0.06944 0.06587 0.0315 0.0130 1.0000
18.000 1.2312 0.07517 0.07171 0.0288 0.0130 1.0000
18.250 1.2186 0.08078 0.07743 0.0260 0.0129 1.0000
18.500 1.2046 0.08674 0.08348 0.0230 0.0128 1.0000
18.750 1.1858 0.09347 0.09033 0.0197 0.0128 1.0000
19.000 1.1691 0.10009 0.09704 0.0163 0.0126 1.0000
19.250 1.1517 0.10690 0.10394 0.0128 0.0125 1.0000
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