RAF 30 AIRFOIL (raf30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: RAF 30 AIRFOIL (raf30-il) Reynolds number: 1,000,000 Max Cl/Cd: 71.64 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-raf30-il-1000000-n5.txt Download as CSV file: xf-raf30-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1864 0.10873 0.10565 -0.0119 1.0000 0.0082
-19.500 -1.2154 0.09996 0.09674 -0.0164 1.0000 0.0081
-19.250 -1.2405 0.09204 0.08869 -0.0204 1.0000 0.0082
-19.000 -1.2643 0.08453 0.08105 -0.0242 1.0000 0.0082
-18.750 -1.2858 0.07749 0.07387 -0.0277 1.0000 0.0082
-18.500 -1.3027 0.07139 0.06764 -0.0306 1.0000 0.0083
-18.250 -1.3169 0.06582 0.06194 -0.0333 1.0000 0.0083
-18.000 -1.3296 0.06067 0.05667 -0.0356 1.0000 0.0083
-17.750 -1.3375 0.05639 0.05228 -0.0373 1.0000 0.0084
-17.500 -1.3458 0.05219 0.04797 -0.0390 1.0000 0.0086
-17.250 -1.3530 0.04833 0.04400 -0.0402 1.0000 0.0087
-17.000 -1.3582 0.04484 0.04042 -0.0412 1.0000 0.0089
-16.750 -1.3603 0.04183 0.03731 -0.0419 1.0000 0.0090
-16.500 -1.3613 0.03906 0.03447 -0.0423 1.0000 0.0093
-16.250 -1.3602 0.03660 0.03192 -0.0424 1.0000 0.0095
-16.000 -1.3576 0.03441 0.02965 -0.0424 1.0000 0.0098
-15.750 -1.3531 0.03249 0.02766 -0.0421 1.0000 0.0101
-15.500 -1.3482 0.03068 0.02577 -0.0417 1.0000 0.0103
-15.250 -1.3419 0.02909 0.02410 -0.0410 1.0000 0.0106
-15.000 -1.3349 0.02764 0.02257 -0.0402 1.0000 0.0109
-14.750 -1.3272 0.02631 0.02117 -0.0392 1.0000 0.0111
-14.500 -1.3193 0.02508 0.01988 -0.0380 1.0000 0.0116
-14.250 -1.3101 0.02402 0.01878 -0.0367 1.0000 0.0120
-14.000 -1.2999 0.02308 0.01779 -0.0353 1.0000 0.0126
-13.750 -1.2892 0.02223 0.01689 -0.0337 1.0000 0.0130
-13.500 -1.2780 0.02147 0.01608 -0.0320 1.0000 0.0135
-13.250 -1.2664 0.02078 0.01533 -0.0302 1.0000 0.0139
-13.000 -1.2549 0.02014 0.01464 -0.0281 1.0000 0.0144
-12.750 -1.2431 0.01956 0.01403 -0.0260 1.0000 0.0149
-12.500 -1.2300 0.01909 0.01356 -0.0239 1.0000 0.0157
-12.250 -1.2181 0.01864 0.01306 -0.0214 1.0000 0.0163
-12.000 -1.2061 0.01822 0.01262 -0.0188 1.0000 0.0168
-11.750 -1.1919 0.01782 0.01217 -0.0167 1.0000 0.0174
-11.500 -1.1756 0.01741 0.01172 -0.0148 1.0000 0.0178
-11.250 -1.1602 0.01695 0.01123 -0.0128 1.0000 0.0183
-11.000 -1.1438 0.01654 0.01079 -0.0110 1.0000 0.0189
-10.750 -1.1264 0.01617 0.01041 -0.0093 1.0000 0.0195
-10.500 -1.1086 0.01582 0.01005 -0.0076 1.0000 0.0202
-10.250 -1.0900 0.01552 0.00972 -0.0060 1.0000 0.0209
-10.000 -1.0713 0.01522 0.00939 -0.0044 1.0000 0.0215
-9.750 -1.0526 0.01492 0.00906 -0.0028 1.0000 0.0219
-9.500 -1.0338 0.01462 0.00873 -0.0012 1.0000 0.0222
-9.250 -1.0156 0.01429 0.00837 0.0005 1.0000 0.0227
-9.000 -0.9894 0.01381 0.00788 0.0004 0.9990 0.0237
-8.750 -0.9583 0.01342 0.00747 -0.0006 0.9969 0.0245
-8.250 -0.8984 0.01275 0.00677 -0.0021 0.9907 0.0260
-8.000 -0.8684 0.01243 0.00643 -0.0028 0.9867 0.0267
-7.750 -0.8377 0.01214 0.00612 -0.0037 0.9826 0.0273
-7.500 -0.8098 0.01186 0.00581 -0.0038 0.9759 0.0277
-7.250 -0.7788 0.01153 0.00546 -0.0047 0.9697 0.0284
-7.000 -0.7457 0.01116 0.00508 -0.0060 0.9622 0.0296
-6.750 -0.7076 0.01082 0.00473 -0.0085 0.9545 0.0307
-6.500 -0.6665 0.01050 0.00440 -0.0116 0.9440 0.0319
-6.250 -0.6259 0.01021 0.00408 -0.0145 0.9278 0.0333
-6.000 -0.5922 0.01002 0.00381 -0.0158 0.9056 0.0344
-5.750 -0.5654 0.00986 0.00357 -0.0156 0.8835 0.0367
-5.500 -0.5409 0.00969 0.00336 -0.0149 0.8646 0.0404
-5.250 -0.5175 0.00948 0.00313 -0.0140 0.8476 0.0496
-5.000 -0.4957 0.00915 0.00288 -0.0129 0.8316 0.0757
-4.750 -0.4724 0.00892 0.00269 -0.0120 0.8175 0.0945
-4.500 -0.4480 0.00875 0.00253 -0.0113 0.8040 0.1074
-4.250 -0.4240 0.00855 0.00236 -0.0105 0.7907 0.1253
-4.000 -0.4006 0.00829 0.00218 -0.0097 0.7781 0.1517
-3.750 -0.3769 0.00806 0.00202 -0.0089 0.7657 0.1787
-3.500 -0.3533 0.00782 0.00187 -0.0080 0.7534 0.2102
-3.250 -0.3291 0.00762 0.00174 -0.0073 0.7393 0.2396
-3.000 -0.3051 0.00747 0.00163 -0.0065 0.7213 0.2677
-2.750 -0.2805 0.00735 0.00153 -0.0058 0.7019 0.2912
-2.500 -0.2556 0.00723 0.00144 -0.0052 0.6860 0.3128
-2.000 -0.2046 0.00701 0.00128 -0.0042 0.6616 0.3567
-1.750 -0.1797 0.00685 0.00121 -0.0035 0.6506 0.3888
-1.500 -0.1558 0.00663 0.00114 -0.0028 0.6396 0.4364
-1.250 -0.1310 0.00647 0.00109 -0.0021 0.6289 0.4761
-1.000 -0.1056 0.00636 0.00106 -0.0015 0.6185 0.5070
-0.500 -0.0535 0.00625 0.00103 -0.0006 0.5968 0.5501
-0.250 -0.0267 0.00624 0.00102 -0.0003 0.5866 0.5634
0.000 0.0000 0.00624 0.00102 0.0000 0.5753 0.5756
0.250 0.0267 0.00624 0.00102 0.0003 0.5632 0.5866
0.500 0.0534 0.00626 0.00103 0.0007 0.5481 0.5963
0.750 0.0797 0.00631 0.00104 0.0011 0.5302 0.6078
1.000 0.1056 0.00636 0.00106 0.0015 0.5070 0.6184
1.250 0.1310 0.00647 0.00109 0.0021 0.4763 0.6287
1.500 0.1556 0.00664 0.00114 0.0028 0.4341 0.6398
1.750 0.1797 0.00684 0.00121 0.0035 0.3893 0.6504
2.000 0.2046 0.00701 0.00128 0.0041 0.3564 0.6613
2.500 0.2556 0.00723 0.00144 0.0052 0.3127 0.6860
2.750 0.2805 0.00735 0.00153 0.0058 0.2916 0.7021
3.000 0.3050 0.00747 0.00163 0.0065 0.2672 0.7216
3.250 0.3290 0.00763 0.00175 0.0073 0.2380 0.7391
3.500 0.3532 0.00783 0.00187 0.0080 0.2097 0.7533
3.750 0.3768 0.00806 0.00202 0.0089 0.1778 0.7658
4.000 0.4005 0.00829 0.00218 0.0097 0.1514 0.7785
4.250 0.4239 0.00855 0.00237 0.0106 0.1244 0.7909
4.500 0.4480 0.00875 0.00253 0.0113 0.1072 0.8038
4.750 0.4723 0.00892 0.00269 0.0120 0.0939 0.8172
5.000 0.4955 0.00915 0.00288 0.0129 0.0750 0.8318
5.250 0.5173 0.00949 0.00314 0.0141 0.0484 0.8475
5.500 0.5409 0.00969 0.00336 0.0149 0.0402 0.8648
5.750 0.5654 0.00985 0.00357 0.0156 0.0368 0.8835
6.000 0.5922 0.01002 0.00381 0.0158 0.0343 0.9057
6.250 0.6261 0.01022 0.00408 0.0145 0.0332 0.9282
6.500 0.6663 0.01050 0.00440 0.0116 0.0319 0.9440
6.750 0.7074 0.01083 0.00474 0.0085 0.0307 0.9544
7.000 0.7454 0.01115 0.00507 0.0061 0.0297 0.9620
7.250 0.7788 0.01153 0.00546 0.0047 0.0285 0.9697
7.500 0.8098 0.01186 0.00581 0.0038 0.0277 0.9759
7.750 0.8376 0.01214 0.00612 0.0037 0.0273 0.9826
8.000 0.8682 0.01243 0.00644 0.0029 0.0267 0.9867
8.250 0.8983 0.01275 0.00677 0.0022 0.0260 0.9906
8.750 0.9584 0.01342 0.00748 0.0006 0.0245 0.9969
9.000 0.9893 0.01381 0.00786 -0.0004 0.0236 0.9989
9.250 1.0158 0.01428 0.00836 -0.0005 0.0227 1.0000
9.500 1.0339 0.01463 0.00873 0.0012 0.0223 1.0000
9.750 1.0530 0.01490 0.00904 0.0028 0.0219 1.0000
10.000 1.0715 0.01521 0.00938 0.0044 0.0215 1.0000
10.250 1.0898 0.01554 0.00975 0.0061 0.0210 1.0000
10.500 1.1082 0.01586 0.01009 0.0077 0.0203 1.0000
10.750 1.1261 0.01619 0.01044 0.0093 0.0197 1.0000
11.000 1.1437 0.01655 0.01081 0.0110 0.0190 1.0000
11.250 1.1604 0.01695 0.01122 0.0128 0.0183 1.0000
11.500 1.1757 0.01740 0.01171 0.0148 0.0178 1.0000
11.750 1.1921 0.01781 0.01216 0.0166 0.0173 1.0000
12.000 1.2061 0.01822 0.01261 0.0188 0.0168 1.0000
12.250 1.2185 0.01861 0.01303 0.0214 0.0162 1.0000
12.500 1.2309 0.01905 0.01350 0.0237 0.0155 1.0000
12.750 1.2432 0.01955 0.01402 0.0260 0.0149 1.0000
13.000 1.2549 0.02014 0.01463 0.0281 0.0142 1.0000
13.250 1.2667 0.02077 0.01531 0.0301 0.0138 1.0000
13.500 1.2784 0.02146 0.01606 0.0320 0.0135 1.0000
13.750 1.2896 0.02222 0.01687 0.0337 0.0130 1.0000
14.000 1.3003 0.02306 0.01777 0.0353 0.0126 1.0000
14.250 1.3105 0.02400 0.01876 0.0367 0.0120 1.0000
14.500 1.3196 0.02507 0.01987 0.0380 0.0115 1.0000
14.750 1.3277 0.02629 0.02115 0.0392 0.0112 1.0000
15.000 1.3352 0.02763 0.02256 0.0402 0.0108 1.0000
15.250 1.3430 0.02902 0.02402 0.0410 0.0105 1.0000
15.500 1.3487 0.03066 0.02575 0.0416 0.0104 1.0000
15.750 1.3541 0.03243 0.02759 0.0421 0.0101 1.0000
16.000 1.3585 0.03437 0.02960 0.0423 0.0097 1.0000
16.250 1.3613 0.03654 0.03186 0.0423 0.0095 1.0000
16.500 1.3622 0.03903 0.03443 0.0422 0.0092 1.0000
16.750 1.3616 0.04177 0.03725 0.0417 0.0090 1.0000
17.000 1.3592 0.04481 0.04039 0.0411 0.0088 1.0000
17.250 1.3543 0.04828 0.04396 0.0401 0.0087 1.0000
17.500 1.3468 0.05220 0.04798 0.0388 0.0086 1.0000
17.750 1.3399 0.05620 0.05209 0.0372 0.0084 1.0000
18.000 1.3301 0.06076 0.05677 0.0353 0.0084 1.0000
18.250 1.3185 0.06577 0.06190 0.0331 0.0083 1.0000
18.500 1.3051 0.07122 0.06747 0.0305 0.0083 1.0000
18.750 1.2891 0.07719 0.07357 0.0276 0.0082 1.0000
19.000 1.2667 0.08437 0.08089 0.0240 0.0082 1.0000
19.250 1.2442 0.09169 0.08834 0.0203 0.0081 1.0000
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