BOEING VERTOL V13006-.7 AIRFOIL (v13006-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: BOEING VERTOL V13006-.7 AIRFOIL (v13006-il) Reynolds number: 200,000 Max Cl/Cd: 46.35 at α=2.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-v13006-il-200000.txt Download as CSV file: xf-v13006-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: BOEING VERTOL V13006-.7 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.500 -0.5257 0.08503 0.08170 0.0048 1.0000 0.0375
-8.250 -0.5248 0.08109 0.07777 0.0042 1.0000 0.0382
-8.000 -0.5260 0.07698 0.07369 0.0031 1.0000 0.0389
-7.750 -0.5292 0.07266 0.06939 0.0013 1.0000 0.0395
-7.500 -0.6255 0.07610 0.07254 -0.0062 1.0000 0.0367
-7.250 -0.6173 0.07259 0.06903 -0.0060 1.0000 0.0376
-7.000 -0.6074 0.06886 0.06528 -0.0071 1.0000 0.0386
-6.750 -0.5959 0.06487 0.06119 -0.0090 1.0000 0.0399
-6.500 -0.5826 0.06069 0.05689 -0.0111 1.0000 0.0416
-6.250 -0.5664 0.05639 0.05242 -0.0132 1.0000 0.0441
-6.000 -0.5405 0.05478 0.05008 -0.0150 1.0000 0.0475
-5.750 -0.5317 0.04707 0.04241 -0.0161 1.0000 0.0492
-5.500 -0.5150 0.04412 0.03950 -0.0160 1.0000 0.0514
-5.250 -0.4624 0.02688 0.02198 -0.0168 1.0000 0.0612
-5.000 -0.4499 0.02233 0.01761 -0.0170 1.0000 0.0637
-4.750 -0.4316 0.01996 0.01517 -0.0166 1.0000 0.0677
-4.500 -0.4123 0.01726 0.01205 -0.0160 1.0000 0.0767
-4.250 -0.3928 0.01534 0.01013 -0.0155 1.0000 0.0818
-4.000 -0.3729 0.01334 0.00788 -0.0148 1.0000 0.0925
-3.750 -0.3525 0.01171 0.00607 -0.0141 1.0000 0.1061
-3.500 -0.3322 0.01024 0.00449 -0.0134 1.0000 0.1213
-3.250 -0.3013 0.01947 0.01197 -0.0101 1.0000 0.0450
-3.000 -0.2754 0.01806 0.01032 -0.0092 1.0000 0.0458
-2.750 -0.2496 0.01631 0.00841 -0.0083 1.0000 0.0446
-2.500 -0.2239 0.01498 0.00696 -0.0074 1.0000 0.0443
-2.250 -0.1986 0.01392 0.00585 -0.0065 1.0000 0.0452
-2.000 -0.1737 0.01311 0.00500 -0.0056 1.0000 0.0470
-1.750 -0.1500 0.01205 0.00402 -0.0048 1.0000 0.0530
-1.500 -0.1252 0.01143 0.00341 -0.0041 1.0000 0.0592
-1.250 -0.1002 0.01079 0.00281 -0.0034 1.0000 0.0754
-1.000 -0.0387 0.00736 0.00254 -0.0094 1.0000 1.0000
-0.750 -0.0182 0.00734 0.00240 -0.0080 1.0000 1.0000
-0.500 0.0022 0.00733 0.00231 -0.0066 1.0000 1.0000
-0.250 0.0231 0.00735 0.00225 -0.0053 1.0000 1.0000
0.000 0.0445 0.00738 0.00223 -0.0041 1.0000 1.0000
0.250 0.0664 0.00744 0.00226 -0.0031 1.0000 1.0000
0.500 0.0885 0.00752 0.00232 -0.0022 1.0000 1.0000
0.750 0.1205 0.00761 0.00240 -0.0034 0.9959 1.0000
1.000 0.1733 0.00762 0.00244 -0.0088 0.9801 1.0000
1.250 0.2216 0.00759 0.00245 -0.0129 0.9585 1.0000
1.500 0.2633 0.00755 0.00245 -0.0154 0.9290 1.0000
1.750 0.2966 0.00753 0.00242 -0.0159 0.8869 1.0000
2.000 0.3225 0.00759 0.00239 -0.0147 0.8330 1.0000
2.250 0.3453 0.00777 0.00241 -0.0128 0.7716 1.0000
2.500 0.3680 0.00805 0.00246 -0.0112 0.7058 1.0000
2.750 0.3907 0.00843 0.00255 -0.0097 0.6316 1.0000
3.000 0.4125 0.00900 0.00265 -0.0082 0.5297 1.0000
3.250 0.4349 0.00964 0.00281 -0.0072 0.4261 1.0000
3.500 0.4590 0.01018 0.00303 -0.0065 0.3557 1.0000
3.750 0.4837 0.01065 0.00329 -0.0061 0.3015 1.0000
4.000 0.5085 0.01116 0.00357 -0.0057 0.2433 1.0000
4.250 0.5296 0.01281 0.00422 -0.0051 0.0626 1.0000
4.500 0.5540 0.01389 0.00528 -0.0044 0.0457 1.0000
4.750 0.5791 0.01467 0.00616 -0.0037 0.0418 1.0000
5.000 0.6034 0.01560 0.00713 -0.0031 0.0394 1.0000
5.250 0.6273 0.01674 0.00828 -0.0023 0.0379 1.0000
5.500 0.6504 0.01838 0.00995 -0.0015 0.0362 1.0000
5.750 0.6749 0.01990 0.01157 -0.0008 0.0347 1.0000
6.000 0.6999 0.02140 0.01324 -0.0001 0.0344 1.0000
6.250 0.7245 0.02327 0.01532 0.0006 0.0343 1.0000
6.500 0.7481 0.02568 0.01802 0.0014 0.0346 1.0000
6.750 0.7703 0.02910 0.02174 0.0022 0.0357 1.0000
8.250 0.8483 0.06094 0.05692 0.0063 0.0722 1.0000
8.500 0.8487 0.06809 0.06408 0.0054 0.0701 1.0000
8.750 0.8136 0.07785 0.07445 -0.0055 0.0662 1.0000
9.000 0.7987 0.08634 0.08293 -0.0150 0.0656 1.0000
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Polar data table (+)
Polar graphs
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