RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il) Reynolds number: 500,000 Max Cl/Cd: 58.29 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-bqm34-il-500000-n5.txt Download as CSV file: xf-bqm34-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: RYAN BQM-34 FIREBEE WING AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.250 -0.9610 0.11149 0.10866 0.0030 1.0000 0.0092
-16.000 -1.0127 0.09577 0.09271 -0.0059 1.0000 0.0091
-15.750 -1.0459 0.08454 0.08128 -0.0126 1.0000 0.0090
-15.500 -1.0740 0.07481 0.07137 -0.0186 1.0000 0.0089
-15.250 -1.0940 0.06702 0.06340 -0.0235 1.0000 0.0089
-15.000 -1.1117 0.06012 0.05633 -0.0279 1.0000 0.0089
-14.750 -1.1291 0.05384 0.04990 -0.0316 1.0000 0.0090
-14.500 -1.1404 0.04893 0.04483 -0.0342 1.0000 0.0090
-14.250 -1.1503 0.04466 0.04041 -0.0359 1.0000 0.0090
-14.000 -1.1561 0.04127 0.03688 -0.0369 1.0000 0.0092
-13.750 -1.1623 0.03814 0.03361 -0.0371 1.0000 0.0092
-13.500 -1.1640 0.03575 0.03109 -0.0368 1.0000 0.0093
-13.250 -1.1652 0.03361 0.02882 -0.0358 1.0000 0.0094
-13.000 -1.1615 0.03211 0.02722 -0.0346 1.0000 0.0096
-12.750 -1.1596 0.03054 0.02553 -0.0327 1.0000 0.0097
-12.500 -1.1577 0.02906 0.02392 -0.0304 1.0000 0.0098
-12.250 -1.1521 0.02795 0.02271 -0.0280 1.0000 0.0100
-12.000 -1.1467 0.02680 0.02144 -0.0253 1.0000 0.0101
-11.750 -1.1359 0.02578 0.02030 -0.0234 1.0000 0.0103
-11.500 -1.1234 0.02475 0.01916 -0.0217 1.0000 0.0106
-11.250 -1.1094 0.02378 0.01806 -0.0201 1.0000 0.0108
-11.000 -1.0944 0.02282 0.01698 -0.0185 1.0000 0.0111
-10.750 -1.0778 0.02196 0.01601 -0.0171 1.0000 0.0113
-10.500 -1.0606 0.02113 0.01507 -0.0158 1.0000 0.0116
-10.250 -1.0444 0.02016 0.01403 -0.0143 1.0000 0.0120
-10.000 -1.0254 0.01947 0.01327 -0.0132 1.0000 0.0125
-9.750 -1.0056 0.01884 0.01258 -0.0121 1.0000 0.0130
-9.500 -0.9853 0.01824 0.01192 -0.0110 1.0000 0.0136
-9.250 -0.9646 0.01766 0.01127 -0.0100 1.0000 0.0142
-9.000 -0.9437 0.01711 0.01063 -0.0089 1.0000 0.0148
-8.750 -0.9239 0.01642 0.00989 -0.0077 1.0000 0.0155
-8.500 -0.9029 0.01589 0.00932 -0.0067 1.0000 0.0163
-8.250 -0.8813 0.01541 0.00881 -0.0056 1.0000 0.0172
-8.000 -0.8596 0.01496 0.00830 -0.0046 1.0000 0.0182
-7.750 -0.8379 0.01452 0.00779 -0.0035 1.0000 0.0191
-7.500 -0.8168 0.01402 0.00729 -0.0024 1.0000 0.0206
-7.250 -0.7948 0.01365 0.00690 -0.0014 1.0000 0.0222
-7.000 -0.7724 0.01331 0.00651 -0.0004 1.0000 0.0237
-6.750 -0.7509 0.01288 0.00608 0.0007 1.0000 0.0259
-6.500 -0.7289 0.01254 0.00573 0.0018 1.0000 0.0281
-6.250 -0.7067 0.01224 0.00540 0.0029 1.0000 0.0302
-6.000 -0.6852 0.01188 0.00506 0.0041 1.0000 0.0337
-5.750 -0.6600 0.01159 0.00475 0.0045 0.9991 0.0370
-5.500 -0.6268 0.01123 0.00442 0.0031 0.9949 0.0428
-5.250 -0.5948 0.01091 0.00412 0.0020 0.9897 0.0492
-5.000 -0.5615 0.01061 0.00383 0.0007 0.9846 0.0572
-4.750 -0.5300 0.01029 0.00356 -0.0002 0.9781 0.0685
-4.500 -0.4961 0.00995 0.00330 -0.0016 0.9722 0.0843
-4.250 -0.4638 0.00962 0.00305 -0.0027 0.9642 0.1046
-4.000 -0.4295 0.00928 0.00282 -0.0043 0.9561 0.1296
-3.750 -0.3973 0.00894 0.00260 -0.0054 0.9445 0.1604
-3.500 -0.3654 0.00859 0.00238 -0.0064 0.9312 0.1973
-3.250 -0.3353 0.00824 0.00218 -0.0069 0.9153 0.2406
-3.000 -0.3078 0.00791 0.00200 -0.0069 0.8976 0.2893
-2.500 -0.2571 0.00731 0.00169 -0.0059 0.8610 0.3964
-2.250 -0.2323 0.00708 0.00159 -0.0052 0.8434 0.4465
-2.000 -0.2073 0.00690 0.00151 -0.0045 0.8267 0.4910
-1.750 -0.1820 0.00677 0.00144 -0.0039 0.8107 0.5287
-1.500 -0.1564 0.00667 0.00139 -0.0033 0.7953 0.5610
-1.250 -0.1305 0.00660 0.00135 -0.0027 0.7802 0.5893
-1.000 -0.1045 0.00654 0.00132 -0.0021 0.7652 0.6145
-0.750 -0.0784 0.00650 0.00130 -0.0016 0.7501 0.6367
-0.500 -0.0522 0.00648 0.00129 -0.0011 0.7343 0.6581
-0.250 -0.0260 0.00646 0.00128 -0.0006 0.7175 0.6792
0.000 0.0000 0.00645 0.00128 0.0000 0.6991 0.6991
0.250 0.0260 0.00646 0.00128 0.0006 0.6790 0.7175
0.500 0.0522 0.00648 0.00129 0.0011 0.6579 0.7344
0.750 0.0784 0.00650 0.00130 0.0016 0.6366 0.7502
1.000 0.1045 0.00654 0.00132 0.0022 0.6144 0.7653
1.250 0.1306 0.00659 0.00135 0.0027 0.5897 0.7802
1.500 0.1564 0.00667 0.00139 0.0033 0.5609 0.7953
1.750 0.1819 0.00677 0.00144 0.0039 0.5287 0.8108
2.000 0.2073 0.00690 0.00151 0.0045 0.4909 0.8267
2.250 0.2322 0.00709 0.00159 0.0052 0.4452 0.8434
2.500 0.2570 0.00732 0.00169 0.0059 0.3946 0.8610
3.000 0.3078 0.00791 0.00200 0.0069 0.2899 0.8975
3.250 0.3353 0.00825 0.00218 0.0069 0.2401 0.9153
3.500 0.3654 0.00859 0.00238 0.0064 0.1975 0.9314
3.750 0.3973 0.00894 0.00260 0.0054 0.1602 0.9446
4.000 0.4296 0.00928 0.00282 0.0043 0.1293 0.9562
4.250 0.4638 0.00962 0.00305 0.0027 0.1045 0.9642
4.500 0.4962 0.00995 0.00330 0.0016 0.0841 0.9723
4.750 0.5299 0.01029 0.00356 0.0002 0.0688 0.9782
5.000 0.5616 0.01061 0.00383 -0.0008 0.0574 0.9847
5.250 0.5948 0.01091 0.00412 -0.0021 0.0492 0.9898
5.500 0.6269 0.01122 0.00442 -0.0031 0.0428 0.9949
5.750 0.6601 0.01159 0.00475 -0.0045 0.0370 0.9992
6.000 0.6851 0.01188 0.00506 -0.0040 0.0338 1.0000
6.250 0.7066 0.01224 0.00540 -0.0029 0.0302 1.0000
6.500 0.7288 0.01254 0.00573 -0.0018 0.0280 1.0000
6.750 0.7508 0.01288 0.00608 -0.0007 0.0258 1.0000
7.000 0.7723 0.01331 0.00651 0.0004 0.0237 1.0000
7.250 0.7947 0.01365 0.00690 0.0014 0.0222 1.0000
7.500 0.8167 0.01402 0.00729 0.0024 0.0206 1.0000
7.750 0.8379 0.01451 0.00779 0.0036 0.0191 1.0000
8.000 0.8597 0.01495 0.00829 0.0046 0.0182 1.0000
8.250 0.8813 0.01541 0.00880 0.0057 0.0172 1.0000
8.500 0.9030 0.01587 0.00931 0.0066 0.0163 1.0000
8.750 0.9239 0.01643 0.00990 0.0077 0.0155 1.0000
9.000 0.9437 0.01712 0.01064 0.0089 0.0148 1.0000
9.250 0.9647 0.01767 0.01127 0.0100 0.0142 1.0000
9.500 0.9852 0.01826 0.01194 0.0110 0.0136 1.0000
9.750 1.0055 0.01886 0.01261 0.0121 0.0130 1.0000
10.000 1.0257 0.01946 0.01327 0.0131 0.0125 1.0000
10.250 1.0447 0.02016 0.01403 0.0143 0.0120 1.0000
10.500 1.0612 0.02109 0.01503 0.0157 0.0116 1.0000
10.750 1.0780 0.02197 0.01602 0.0171 0.0113 1.0000
11.000 1.0946 0.02282 0.01698 0.0185 0.0111 1.0000
11.250 1.1097 0.02377 0.01805 0.0200 0.0109 1.0000
11.500 1.1239 0.02474 0.01914 0.0216 0.0106 1.0000
11.750 1.1364 0.02577 0.02029 0.0233 0.0103 1.0000
12.000 1.1473 0.02680 0.02144 0.0252 0.0101 1.0000
12.250 1.1529 0.02793 0.02269 0.0279 0.0099 1.0000
12.500 1.1591 0.02900 0.02385 0.0302 0.0097 1.0000
12.750 1.1618 0.03041 0.02538 0.0325 0.0096 1.0000
13.000 1.1651 0.03185 0.02694 0.0343 0.0095 1.0000
13.250 1.1666 0.03356 0.02876 0.0357 0.0093 1.0000
13.500 1.1665 0.03556 0.03088 0.0366 0.0092 1.0000
13.750 1.1613 0.03834 0.03382 0.0370 0.0092 1.0000
14.000 1.1581 0.04113 0.03672 0.0367 0.0091 1.0000
14.250 1.1510 0.04468 0.04043 0.0358 0.0090 1.0000
14.500 1.1424 0.04881 0.04470 0.0340 0.0090 1.0000
14.750 1.1294 0.05397 0.05004 0.0314 0.0090 1.0000
15.000 1.1159 0.05968 0.05591 0.0280 0.0090 1.0000
15.250 1.0964 0.06684 0.06321 0.0234 0.0089 1.0000
15.500 1.0755 0.07483 0.07140 0.0184 0.0090 1.0000
15.750 1.0508 0.08394 0.08068 0.0127 0.0090 1.0000
16.000 1.0141 0.09578 0.09271 0.0057 0.0090 1.0000
16.250 0.9702 0.10976 0.10690 -0.0023 0.0092 1.0000
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