HAWKER TEMPEST 96.77% SEMISPAN AIRFOIL (tempest3-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HAWKER TEMPEST 96.77% SEMISPAN AIRFOIL (tempest3-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.2 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-tempest3-il-1000000-n5.txt Download as CSV file: xf-tempest3-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HAWKER TEMPEST 96.77% SEMISPAN 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
------ -------- --------- --------- -------- -------- --------
-13.000 -0.9274 0.04370 0.04149 -0.0580 1.0000 0.0031
-12.750 -0.9136 0.04298 0.04078 -0.0580 1.0000 0.0032
-12.500 -0.9469 0.03771 0.03524 -0.0571 1.0000 0.0032
-12.250 -0.9712 0.03423 0.03150 -0.0535 1.0000 0.0031
-12.000 -0.9746 0.03281 0.02997 -0.0501 1.0000 0.0032
-11.750 -0.9829 0.03136 0.02838 -0.0454 1.0000 0.0033
-11.500 -0.9901 0.02945 0.02628 -0.0409 1.0000 0.0033
-11.250 -0.9888 0.02803 0.02470 -0.0373 1.0000 0.0034
-11.000 -0.9881 0.02648 0.02295 -0.0335 1.0000 0.0034
-10.750 -0.9855 0.02507 0.02136 -0.0298 1.0000 0.0035
-10.500 -0.9727 0.02371 0.01983 -0.0280 0.9994 0.0036
-10.250 -0.9501 0.02227 0.01818 -0.0282 0.9977 0.0038
-10.000 -0.9252 0.02124 0.01700 -0.0285 0.9958 0.0039
-9.750 -0.9020 0.01986 0.01543 -0.0286 0.9937 0.0040
-9.500 -0.8778 0.01904 0.01448 -0.0286 0.9914 0.0041
-9.250 -0.8536 0.01799 0.01328 -0.0286 0.9888 0.0042
-9.000 -0.8280 0.01701 0.01216 -0.0288 0.9865 0.0042
-8.750 -0.8002 0.01628 0.01130 -0.0293 0.9847 0.0043
-8.500 -0.7737 0.01515 0.01001 -0.0297 0.9830 0.0045
-8.250 -0.7494 0.01425 0.00900 -0.0295 0.9801 0.0047
-8.000 -0.7233 0.01376 0.00847 -0.0295 0.9768 0.0051
-7.750 -0.6949 0.01325 0.00791 -0.0300 0.9742 0.0054
-7.500 -0.6645 0.01283 0.00745 -0.0309 0.9721 0.0058
-7.250 -0.6334 0.01228 0.00681 -0.0320 0.9701 0.0061
-7.000 -0.6050 0.01182 0.00628 -0.0324 0.9665 0.0064
-6.750 -0.5774 0.01140 0.00580 -0.0326 0.9612 0.0067
-6.500 -0.5464 0.01100 0.00535 -0.0335 0.9572 0.0069
-6.250 -0.5184 0.01050 0.00478 -0.0338 0.9518 0.0073
-6.000 -0.4910 0.01011 0.00433 -0.0339 0.9451 0.0079
-5.750 -0.4626 0.00978 0.00396 -0.0342 0.9392 0.0089
-5.500 -0.4359 0.00953 0.00367 -0.0341 0.9314 0.0098
-5.250 -0.4086 0.00931 0.00341 -0.0341 0.9242 0.0105
-5.000 -0.3829 0.00901 0.00308 -0.0337 0.9157 0.0126
-4.750 -0.3570 0.00879 0.00283 -0.0334 0.9075 0.0147
-4.500 -0.3308 0.00861 0.00259 -0.0330 0.8988 0.0176
-4.250 -0.3056 0.00840 0.00238 -0.0326 0.8894 0.0232
-4.000 -0.2806 0.00817 0.00218 -0.0320 0.8804 0.0354
-3.750 -0.2563 0.00791 0.00198 -0.0314 0.8711 0.0596
-3.500 -0.2316 0.00769 0.00181 -0.0308 0.8611 0.0827
-3.250 -0.2067 0.00750 0.00168 -0.0303 0.8515 0.1047
-3.000 -0.1821 0.00731 0.00154 -0.0297 0.8418 0.1323
-2.750 -0.1575 0.00711 0.00142 -0.0291 0.8318 0.1648
-2.500 -0.1347 0.00676 0.00128 -0.0283 0.8221 0.2311
-2.250 -0.1113 0.00650 0.00117 -0.0275 0.8121 0.2871
-2.000 -0.0878 0.00625 0.00107 -0.0267 0.8016 0.3427
-1.750 -0.0649 0.00597 0.00098 -0.0258 0.7908 0.4114
-1.500 -0.0411 0.00577 0.00090 -0.0250 0.7799 0.4626
-1.250 -0.0176 0.00559 0.00085 -0.0242 0.7684 0.5161
-1.000 0.0059 0.00544 0.00080 -0.0233 0.7562 0.5627
-0.750 0.0297 0.00532 0.00077 -0.0225 0.7433 0.6035
-0.500 0.0532 0.00522 0.00074 -0.0216 0.7294 0.6434
-0.250 0.0766 0.00513 0.00072 -0.0206 0.7135 0.6805
0.000 0.0987 0.00503 0.00072 -0.0194 0.6957 0.7285
0.250 0.1190 0.00489 0.00075 -0.0176 0.6770 0.7916
0.500 0.1415 0.00485 0.00079 -0.0164 0.6589 0.8346
0.750 0.1664 0.00487 0.00083 -0.0157 0.6422 0.8589
1.000 0.1920 0.00491 0.00088 -0.0151 0.6259 0.8785
1.250 0.2182 0.00498 0.00093 -0.0148 0.6091 0.8925
1.500 0.2449 0.00506 0.00099 -0.0145 0.5926 0.9036
1.750 0.2709 0.00518 0.00105 -0.0141 0.5703 0.9137
2.000 0.2973 0.00534 0.00113 -0.0139 0.5407 0.9226
2.250 0.3243 0.00549 0.00121 -0.0137 0.5150 0.9300
2.500 0.3515 0.00565 0.00131 -0.0137 0.4900 0.9372
2.750 0.3788 0.00584 0.00141 -0.0137 0.4583 0.9431
3.000 0.4066 0.00612 0.00154 -0.0139 0.4149 0.9485
3.250 0.4303 0.00645 0.00169 -0.0132 0.3663 0.9550
3.500 0.4578 0.00704 0.00194 -0.0136 0.2793 0.9586
3.750 0.4850 0.00749 0.00216 -0.0138 0.2226 0.9628
4.000 0.5068 0.00800 0.00240 -0.0129 0.1593 0.9688
4.250 0.5378 0.00846 0.00267 -0.0140 0.1126 0.9706
4.500 0.5688 0.00887 0.00293 -0.0150 0.0782 0.9727
4.750 0.5988 0.00927 0.00321 -0.0158 0.0502 0.9754
5.000 0.6270 0.00964 0.00349 -0.0162 0.0323 0.9787
5.250 0.6527 0.00997 0.00377 -0.0160 0.0220 0.9824
5.500 0.6841 0.01025 0.00405 -0.0171 0.0171 0.9836
5.750 0.7146 0.01056 0.00436 -0.0179 0.0136 0.9850
6.000 0.7447 0.01085 0.00466 -0.0187 0.0118 0.9866
6.250 0.7734 0.01122 0.00502 -0.0192 0.0098 0.9885
6.500 0.8017 0.01154 0.00539 -0.0196 0.0088 0.9904
6.750 0.8293 0.01187 0.00575 -0.0199 0.0082 0.9924
7.000 0.8563 0.01222 0.00614 -0.0200 0.0075 0.9942
7.250 0.8852 0.01261 0.00655 -0.0207 0.0069 0.9956
7.500 0.9127 0.01318 0.00716 -0.0211 0.0061 0.9972
7.750 0.9404 0.01366 0.00770 -0.0215 0.0058 0.9986
8.000 0.9687 0.01405 0.00815 -0.0220 0.0054 0.9997
8.250 0.9892 0.01444 0.00858 -0.0209 0.0050 1.0000
8.500 1.0051 0.01484 0.00903 -0.0187 0.0048 1.0000
8.750 1.0207 0.01527 0.00950 -0.0166 0.0045 1.0000
9.000 1.0366 0.01569 0.00997 -0.0145 0.0043 1.0000
9.250 1.0519 0.01615 0.01047 -0.0123 0.0041 1.0000
9.500 1.0656 0.01676 0.01113 -0.0099 0.0039 1.0000
9.750 1.0782 0.01743 0.01189 -0.0073 0.0038 1.0000
10.000 1.0878 0.01835 0.01292 -0.0042 0.0036 1.0000
10.250 1.1000 0.01906 0.01373 -0.0017 0.0035 1.0000
10.500 1.1141 0.01963 0.01438 0.0005 0.0035 1.0000
10.750 1.1256 0.02026 0.01509 0.0031 0.0034 1.0000
11.000 1.1320 0.02109 0.01602 0.0066 0.0033 1.0000
11.250 1.1432 0.02166 0.01667 0.0092 0.0032 1.0000
11.500 1.1512 0.02252 0.01763 0.0120 0.0031 1.0000
11.750 1.1596 0.02341 0.01862 0.0147 0.0031 1.0000
12.000 1.1670 0.02443 0.01975 0.0173 0.0030 1.0000
12.250 1.1732 0.02557 0.02102 0.0198 0.0029 1.0000
12.500 1.1812 0.02660 0.02215 0.0219 0.0028 1.0000
12.750 1.1843 0.02807 0.02377 0.0243 0.0028 1.0000
13.000 1.1874 0.02959 0.02543 0.0265 0.0027 1.0000
13.250 1.1901 0.03120 0.02717 0.0283 0.0027 1.0000
13.500 1.1915 0.03301 0.02911 0.0300 0.0026 1.0000
13.750 1.1910 0.03511 0.03135 0.0314 0.0026 1.0000
14.000 1.1951 0.03685 0.03318 0.0322 0.0025 1.0000
14.250 1.1965 0.03897 0.03541 0.0328 0.0024 1.0000
14.500 1.1883 0.04228 0.03889 0.0332 0.0024 1.0000
14.750 1.1733 0.04669 0.04352 0.0329 0.0025 1.0000
15.000 1.1799 0.04869 0.04554 0.0324 0.0023 1.0000
15.250 1.1534 0.05534 0.05245 0.0302 0.0024 1.0000
15.500 1.1586 0.05788 0.05502 0.0290 0.0023 1.0000
15.750 1.1359 0.06496 0.06230 0.0256 0.0023 1.0000
16.000 1.1156 0.07231 0.06981 0.0215 0.0023 1.0000
16.250 1.0988 0.07957 0.07719 0.0174 0.0023 1.0000
16.500 1.0520 0.09349 0.09134 0.0095 0.0023 1.0000
16.750 0.9965 0.11012 0.10818 0.0010 0.0024 1.0000
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