RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: RYAN BQM-34 FIREBEE WING AIRFOIL (bqm34-il) Reynolds number: 1,000,000 Max Cl/Cd: 72.35 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-bqm34-il-1000000-n5.txt Download as CSV file: xf-bqm34-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.9318 0.15893 0.15689 0.0281 1.0000 0.0065
-18.250 -0.9644 0.14613 0.14399 0.0211 1.0000 0.0066
-18.000 -0.9954 0.13441 0.13216 0.0146 1.0000 0.0065
-17.750 -1.0303 0.12242 0.12006 0.0080 1.0000 0.0064
-17.500 -1.0738 0.10923 0.10673 0.0008 1.0000 0.0064
-17.250 -1.1314 0.09393 0.09126 -0.0077 1.0000 0.0063
-17.000 -1.1788 0.08084 0.07799 -0.0151 1.0000 0.0063
-16.750 -1.2159 0.06991 0.06689 -0.0216 1.0000 0.0063
-16.500 -1.2417 0.06148 0.05829 -0.0268 1.0000 0.0063
-16.250 -1.2624 0.05442 0.05107 -0.0311 1.0000 0.0063
-16.000 -1.2765 0.04887 0.04536 -0.0342 1.0000 0.0063
-15.750 -1.2841 0.04465 0.04100 -0.0363 1.0000 0.0063
-15.500 -1.2934 0.04056 0.03677 -0.0378 1.0000 0.0063
-15.250 -1.2990 0.03728 0.03336 -0.0386 1.0000 0.0063
-15.000 -1.3003 0.03473 0.03069 -0.0386 1.0000 0.0064
-14.750 -1.2998 0.03258 0.02842 -0.0382 1.0000 0.0064
-14.500 -1.2976 0.03078 0.02652 -0.0373 1.0000 0.0065
-14.250 -1.3002 0.02881 0.02441 -0.0357 1.0000 0.0065
-14.000 -1.3016 0.02711 0.02260 -0.0335 1.0000 0.0067
-13.750 -1.2985 0.02586 0.02126 -0.0311 1.0000 0.0068
-13.500 -1.2940 0.02478 0.02009 -0.0285 1.0000 0.0070
-13.250 -1.2869 0.02391 0.01914 -0.0258 1.0000 0.0071
-13.000 -1.2756 0.02313 0.01831 -0.0238 1.0000 0.0073
-12.750 -1.2623 0.02230 0.01739 -0.0220 1.0000 0.0074
-12.500 -1.2481 0.02147 0.01647 -0.0204 1.0000 0.0075
-12.250 -1.2315 0.02077 0.01570 -0.0190 1.0000 0.0077
-12.000 -1.2148 0.02004 0.01489 -0.0176 1.0000 0.0077
-11.750 -1.1966 0.01939 0.01418 -0.0164 1.0000 0.0079
-11.500 -1.1780 0.01875 0.01347 -0.0152 1.0000 0.0081
-11.250 -1.1587 0.01815 0.01278 -0.0140 1.0000 0.0083
-11.000 -1.1390 0.01755 0.01212 -0.0129 1.0000 0.0085
-10.750 -1.1186 0.01701 0.01152 -0.0119 1.0000 0.0086
-10.500 -1.0978 0.01649 0.01094 -0.0109 1.0000 0.0088
-10.250 -1.0779 0.01585 0.01024 -0.0097 1.0000 0.0092
-10.000 -1.0569 0.01534 0.00968 -0.0087 1.0000 0.0096
-9.750 -1.0354 0.01487 0.00919 -0.0077 1.0000 0.0100
-9.500 -1.0135 0.01444 0.00872 -0.0068 1.0000 0.0104
-9.250 -0.9914 0.01404 0.00827 -0.0059 1.0000 0.0108
-9.000 -0.9692 0.01365 0.00785 -0.0049 1.0000 0.0112
-8.750 -0.9468 0.01329 0.00745 -0.0040 1.0000 0.0116
-8.500 -0.9250 0.01286 0.00700 -0.0029 1.0000 0.0125
-8.250 -0.9026 0.01251 0.00664 -0.0020 1.0000 0.0133
-8.000 -0.8799 0.01219 0.00630 -0.0011 1.0000 0.0142
-7.750 -0.8572 0.01190 0.00597 -0.0001 1.0000 0.0148
-7.500 -0.8350 0.01155 0.00561 0.0009 1.0000 0.0159
-7.250 -0.8126 0.01124 0.00530 0.0020 1.0000 0.0171
-7.000 -0.7874 0.01097 0.00502 0.0024 0.9995 0.0183
-6.750 -0.7554 0.01066 0.00470 0.0013 0.9969 0.0198
-6.500 -0.7243 0.01036 0.00440 0.0005 0.9931 0.0218
-6.250 -0.6936 0.01010 0.00414 -0.0003 0.9886 0.0238
-6.000 -0.6615 0.00980 0.00387 -0.0013 0.9844 0.0270
-5.750 -0.6296 0.00956 0.00362 -0.0023 0.9791 0.0298
-5.500 -0.5962 0.00928 0.00337 -0.0036 0.9732 0.0345
-5.250 -0.5623 0.00904 0.00314 -0.0050 0.9657 0.0393
-5.000 -0.5275 0.00878 0.00291 -0.0066 0.9560 0.0458
-4.750 -0.4949 0.00854 0.00269 -0.0077 0.9414 0.0540
-4.500 -0.4653 0.00834 0.00250 -0.0080 0.9224 0.0631
-4.250 -0.4386 0.00815 0.00231 -0.0078 0.9006 0.0756
-4.000 -0.4130 0.00800 0.00214 -0.0072 0.8789 0.0901
-3.750 -0.3876 0.00784 0.00198 -0.0067 0.8584 0.1072
-3.500 -0.3622 0.00767 0.00182 -0.0061 0.8393 0.1265
-3.250 -0.3368 0.00750 0.00169 -0.0056 0.8217 0.1511
-3.000 -0.3113 0.00732 0.00155 -0.0051 0.8055 0.1787
-2.750 -0.2858 0.00712 0.00143 -0.0046 0.7901 0.2104
-2.500 -0.2603 0.00691 0.00131 -0.0041 0.7754 0.2490
-2.250 -0.2349 0.00668 0.00120 -0.0037 0.7612 0.2919
-2.000 -0.2093 0.00647 0.00110 -0.0032 0.7473 0.3367
-1.750 -0.1837 0.00627 0.00101 -0.0028 0.7333 0.3831
-1.500 -0.1580 0.00608 0.00094 -0.0023 0.7193 0.4288
-1.250 -0.1320 0.00594 0.00089 -0.0019 0.7042 0.4687
-1.000 -0.1058 0.00583 0.00085 -0.0015 0.6878 0.5031
-0.750 -0.0794 0.00575 0.00082 -0.0011 0.6702 0.5346
-0.500 -0.0531 0.00571 0.00079 -0.0007 0.6501 0.5606
-0.250 -0.0266 0.00570 0.00078 -0.0004 0.6285 0.5849
0.000 0.0000 0.00569 0.00077 0.0000 0.6067 0.6065
0.250 0.0265 0.00570 0.00078 0.0004 0.5849 0.6286
0.500 0.0531 0.00571 0.00079 0.0007 0.5612 0.6502
0.750 0.0794 0.00576 0.00082 0.0011 0.5343 0.6698
1.000 0.1058 0.00583 0.00085 0.0015 0.5038 0.6879
1.250 0.1320 0.00593 0.00089 0.0019 0.4697 0.7041
1.500 0.1579 0.00608 0.00094 0.0023 0.4287 0.7192
1.750 0.1837 0.00627 0.00101 0.0028 0.3829 0.7334
2.000 0.2093 0.00647 0.00110 0.0032 0.3365 0.7473
2.250 0.2348 0.00669 0.00120 0.0037 0.2913 0.7613
2.500 0.2603 0.00691 0.00131 0.0041 0.2481 0.7755
2.750 0.2858 0.00712 0.00143 0.0046 0.2105 0.7901
3.000 0.3113 0.00732 0.00155 0.0051 0.1788 0.8054
3.500 0.3622 0.00767 0.00182 0.0061 0.1262 0.8394
3.750 0.3876 0.00784 0.00198 0.0067 0.1072 0.8584
4.000 0.4130 0.00800 0.00214 0.0072 0.0898 0.8788
4.250 0.4386 0.00816 0.00231 0.0078 0.0755 0.9006
4.500 0.4654 0.00834 0.00249 0.0080 0.0634 0.9224
4.750 0.4949 0.00854 0.00269 0.0077 0.0541 0.9414
5.000 0.5275 0.00878 0.00291 0.0066 0.0458 0.9560
5.250 0.5624 0.00904 0.00314 0.0050 0.0392 0.9658
5.500 0.5962 0.00928 0.00337 0.0036 0.0345 0.9733
5.750 0.6296 0.00956 0.00362 0.0023 0.0297 0.9792
6.000 0.6615 0.00980 0.00387 0.0013 0.0270 0.9844
6.250 0.6937 0.01010 0.00414 0.0003 0.0238 0.9886
6.500 0.7244 0.01036 0.00440 -0.0005 0.0218 0.9931
6.750 0.7555 0.01067 0.00470 -0.0014 0.0197 0.9970
7.000 0.7875 0.01097 0.00502 -0.0024 0.0183 0.9996
7.250 0.8124 0.01124 0.00530 -0.0019 0.0171 1.0000
7.500 0.8349 0.01154 0.00561 -0.0009 0.0160 1.0000
7.750 0.8571 0.01189 0.00597 0.0001 0.0148 1.0000
8.000 0.8799 0.01219 0.00630 0.0011 0.0141 1.0000
8.250 0.9026 0.01251 0.00663 0.0020 0.0133 1.0000
8.500 0.9250 0.01286 0.00700 0.0030 0.0125 1.0000
8.750 0.9467 0.01330 0.00745 0.0040 0.0116 1.0000
9.000 0.9691 0.01366 0.00785 0.0049 0.0112 1.0000
9.250 0.9914 0.01404 0.00828 0.0059 0.0108 1.0000
9.500 1.0135 0.01444 0.00872 0.0068 0.0104 1.0000
9.750 1.0354 0.01487 0.00918 0.0077 0.0100 1.0000
10.000 1.0570 0.01533 0.00968 0.0087 0.0096 1.0000
10.250 1.0781 0.01585 0.01024 0.0097 0.0092 1.0000
10.500 1.0981 0.01648 0.01092 0.0108 0.0088 1.0000
10.750 1.1186 0.01703 0.01153 0.0119 0.0086 1.0000
11.000 1.1391 0.01756 0.01213 0.0129 0.0085 1.0000
11.250 1.1589 0.01814 0.01278 0.0140 0.0083 1.0000
11.500 1.1783 0.01875 0.01346 0.0151 0.0081 1.0000
11.750 1.1968 0.01940 0.01418 0.0163 0.0080 1.0000
12.000 1.2151 0.02004 0.01489 0.0176 0.0078 1.0000
12.250 1.2319 0.02076 0.01569 0.0189 0.0076 1.0000
12.500 1.2485 0.02147 0.01646 0.0203 0.0074 1.0000
12.750 1.2632 0.02226 0.01734 0.0219 0.0073 1.0000
13.000 1.2771 0.02306 0.01822 0.0236 0.0072 1.0000
13.250 1.2877 0.02390 0.01913 0.0257 0.0070 1.0000
13.500 1.2940 0.02483 0.02013 0.0284 0.0069 1.0000
13.750 1.2992 0.02587 0.02127 0.0310 0.0069 1.0000
14.000 1.3011 0.02720 0.02270 0.0334 0.0067 1.0000
14.250 1.3011 0.02880 0.02441 0.0355 0.0065 1.0000
14.500 1.2985 0.03079 0.02652 0.0371 0.0065 1.0000
14.750 1.3002 0.03265 0.02849 0.0380 0.0064 1.0000
15.000 1.2997 0.03491 0.03087 0.0384 0.0064 1.0000
15.250 1.3011 0.03720 0.03328 0.0384 0.0063 1.0000
15.500 1.2950 0.04055 0.03676 0.0376 0.0063 1.0000
15.750 1.2909 0.04398 0.04032 0.0363 0.0063 1.0000
16.000 1.2783 0.04889 0.04539 0.0339 0.0063 1.0000
16.250 1.2662 0.05416 0.05080 0.0310 0.0062 1.0000
16.500 1.2516 0.06018 0.05697 0.0274 0.0062 1.0000
16.750 1.2232 0.06903 0.06599 0.0218 0.0063 1.0000
17.000 1.1794 0.08116 0.07832 0.0145 0.0063 1.0000
17.250 1.1356 0.09357 0.09090 0.0075 0.0063 1.0000
17.500 1.0803 0.10841 0.10591 -0.0006 0.0064 1.0000
17.750 1.0305 0.12282 0.12046 -0.0085 0.0064 1.0000
18.000 0.9947 0.13502 0.13278 -0.0152 0.0065 1.0000
18.250 0.9624 0.14705 0.14492 -0.0218 0.0065 1.0000
18.500 0.9314 0.15963 0.15761 -0.0287 0.0066 1.0000
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Polar data table (+)
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