[Airfoil] ; obsolete: Airfoilname=MH 45 ; new: Description1=MH 45 NumberSets=1 [Set1] Origin=Berechnung: X-Foil Description1=Bestandteil von 'Profile für Nurflügelmodelle' NumberPolars=5 [Set1-Polar1] Re-Nr=100000 ReynoldsNumber=100000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=27 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.298 0.01695 -0.0286 0.9614 0.0567 Value02= -3.00 -0.182 0.01441 -0.0300 0.8936 0.4826 Value03= -2.50 -0.134 0.01395 -0.0276 0.8643 0.6063 Value04= -2.00 -0.090 0.01355 -0.0236 0.8382 0.7453 Value05= -1.50 -0.029 0.01348 -0.0211 0.8173 0.9086 Value06= -0.50 0.159 0.01355 -0.0354 0.7746 1.0000 Value07= 0.00 0.200 0.01380 -0.0327 0.7482 1.0000 Value08= 0.50 0.242 0.01405 -0.0298 0.7233 1.0000 Value09= 1.00 0.286 0.01426 -0.0270 0.6991 1.0000 Value10= 1.50 0.331 0.01446 -0.0243 0.6737 1.0000 Value11= 2.00 0.377 0.01460 -0.0216 0.6482 1.0000 Value12= 2.50 0.424 0.01469 -0.0188 0.6221 1.0000 Value13= 3.00 0.472 0.01480 -0.0165 0.5928 1.0000 Value14= 3.50 0.521 0.01491 -0.0143 0.5615 1.0000 Value15= 4.00 0.571 0.01510 -0.0123 0.5268 1.0000 Value16= 4.50 0.621 0.01541 -0.0105 0.4879 1.0000 Value17= 5.00 0.671 0.01594 -0.0091 0.4473 1.0000 Value18= 5.50 0.721 0.01655 -0.0078 0.4015 1.0000 Value19= 6.00 0.770 0.01734 -0.0067 0.3528 1.0000 Value20= 6.50 0.819 0.01831 -0.0059 0.3023 1.0000 Value21= 7.00 0.868 0.01962 -0.0051 0.2544 1.0000 Value22= 7.50 0.915 0.02112 -0.0045 0.2082 1.0000 Value23= 8.00 0.960 0.02311 -0.0037 0.1692 1.0000 Value24= 8.50 1.003 0.02524 -0.0029 0.1347 1.0000 Value25= 9.00 1.042 0.02737 -0.0023 0.1031 1.0000 Value26= 9.50 1.078 0.03009 -0.0014 0.0759 1.0000 Value27= 10.00 1.109 0.03369 0.0000 0.0560 1.0000 [Set1-Polar2] Re-Nr=200000 ReynoldsNumber=200000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=33 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.317 0.01488 -0.0182 0.8561 0.0198 Value02= -3.50 -0.270 0.01353 -0.0158 0.8349 0.0402 Value03= -3.00 -0.224 0.01215 -0.0139 0.8146 0.2312 Value04= -2.50 -0.176 0.01137 -0.0123 0.7959 0.3968 Value05= -2.00 -0.128 0.01075 -0.0105 0.7785 0.5364 Value06= -1.50 -0.080 0.01015 -0.0081 0.7606 0.6673 Value07= -1.00 -0.035 0.00954 -0.0048 0.7427 0.8190 Value08= -0.50 0.054 0.00938 -0.0095 0.7251 0.9638 Value09= 0.00 0.159 0.00930 -0.0193 0.7041 1.0000 Value10= 0.50 0.208 0.00932 -0.0177 0.6823 1.0000 Value11= 1.00 0.257 0.00938 -0.0162 0.6588 1.0000 Value12= 1.50 0.307 0.00946 -0.0147 0.6331 1.0000 Value13= 2.00 0.358 0.00958 -0.0134 0.6050 1.0000 Value14= 2.50 0.409 0.00975 -0.0121 0.5736 1.0000 Value15= 3.00 0.459 0.00999 -0.0108 0.5391 1.0000 Value16= 3.50 0.510 0.01031 -0.0096 0.5017 1.0000 Value17= 4.00 0.561 0.01071 -0.0086 0.4653 1.0000 Value18= 4.50 0.613 0.01118 -0.0077 0.4240 1.0000 Value19= 5.00 0.664 0.01172 -0.0070 0.3809 1.0000 Value20= 5.50 0.715 0.01237 -0.0064 0.3349 1.0000 Value21= 6.00 0.767 0.01309 -0.0060 0.2915 1.0000 Value22= 6.50 0.817 0.01399 -0.0057 0.2420 1.0000 Value23= 7.00 0.868 0.01500 -0.0054 0.2006 1.0000 Value24= 7.50 0.918 0.01620 -0.0052 0.1619 1.0000 Value25= 8.00 0.967 0.01746 -0.0052 0.1244 1.0000 Value26= 8.50 1.014 0.01894 -0.0049 0.0953 1.0000 Value27= 9.00 1.060 0.02044 -0.0045 0.0725 1.0000 Value28= 9.50 1.099 0.02290 -0.0037 0.0487 1.0000 Value29= 10.00 1.133 0.02585 -0.0026 0.0336 1.0000 Value30= 10.50 1.160 0.02916 -0.0013 0.0243 1.0000 Value31= 11.00 1.185 0.03211 -0.0002 0.0206 1.0000 Value32= 11.50 1.195 0.03613 0.0013 0.0177 1.0000 Value33= 12.00 1.196 0.04167 0.0022 0.0155 1.0000 [Set1-Polar3] Re-Nr=400000 ReynoldsNumber=400000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=33 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.349 0.01284 -0.0084 0.7951 0.0099 Value02= -3.50 -0.298 0.01183 -0.0071 0.7799 0.0136 Value03= -3.00 -0.245 0.01087 -0.0059 0.7644 0.0305 Value04= -2.50 -0.195 0.00961 -0.0051 0.7486 0.2226 Value05= -2.00 -0.142 0.00896 -0.0045 0.7323 0.3503 Value06= -1.50 -0.090 0.00842 -0.0037 0.7154 0.4675 Value07= -1.00 -0.038 0.00785 -0.0026 0.6977 0.6024 Value08= -0.50 0.013 0.00730 -0.0010 0.6788 0.7374 Value09= 0.00 0.060 0.00668 0.0020 0.6600 0.9148 Value10= 0.50 0.165 0.00674 -0.0078 0.6335 0.9916 Value11= 1.00 0.250 0.00684 -0.0140 0.6040 1.0000 Value12= 1.50 0.302 0.00697 -0.0130 0.5751 1.0000 Value13= 2.00 0.354 0.00717 -0.0122 0.5421 1.0000 Value14= 2.50 0.406 0.00742 -0.0114 0.5064 1.0000 Value15= 3.00 0.458 0.00773 -0.0107 0.4691 1.0000 Value16= 3.50 0.510 0.00809 -0.0100 0.4309 1.0000 Value17= 4.00 0.562 0.00849 -0.0091 0.3923 1.0000 Value18= 4.50 0.612 0.00892 -0.0080 0.3569 1.0000 Value19= 5.00 0.662 0.00944 -0.0071 0.3158 1.0000 Value20= 5.50 0.713 0.01003 -0.0065 0.2725 1.0000 Value21= 6.00 0.765 0.01070 -0.0061 0.2318 1.0000 Value22= 6.50 0.817 0.01152 -0.0060 0.1840 1.0000 Value23= 7.00 0.869 0.01238 -0.0059 0.1469 1.0000 Value24= 7.50 0.920 0.01332 -0.0058 0.1147 1.0000 Value25= 8.00 0.971 0.01426 -0.0058 0.0907 1.0000 Value26= 8.50 1.021 0.01532 -0.0057 0.0690 1.0000 Value27= 9.00 1.070 0.01658 -0.0055 0.0475 1.0000 Value28= 9.50 1.116 0.01811 -0.0052 0.0288 1.0000 Value29= 10.00 1.159 0.02006 -0.0047 0.0192 1.0000 Value30= 10.50 1.194 0.02267 -0.0038 0.0147 1.0000 Value31= 11.00 1.227 0.02516 -0.0030 0.0127 1.0000 Value32= 11.50 1.239 0.02904 -0.0015 0.0111 1.0000 Value33= 12.00 1.232 0.03477 -0.0005 0.0101 1.0000 [Set1-Polar4] Re-Nr=600000 ReynoldsNumber=600000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=37 ; Alpha Cl Cd Cm T.U. T.L. Value01= -3.50 -0.306 0.01079 -0.0048 0.7524 0.0097 Value02= -3.00 -0.252 0.00999 -0.0038 0.7368 0.0166 Value03= -2.50 -0.199 0.00917 -0.0031 0.7217 0.0938 Value04= -2.00 -0.147 0.00824 -0.0026 0.7058 0.2621 Value05= -1.50 -0.093 0.00770 -0.0022 0.6899 0.3779 Value06= -1.00 -0.040 0.00714 -0.0016 0.6714 0.5154 Value07= -0.50 0.014 0.00675 -0.0010 0.6514 0.6210 Value08= 0.00 0.067 0.00633 0.0000 0.6295 0.7421 Value09= 0.50 0.114 0.00578 0.0026 0.6048 0.9148 Value10= 1.00 0.212 0.00589 -0.0060 0.5715 0.9925 Value11= 1.50 0.303 0.00608 -0.0135 0.5352 1.0000 Value12= 2.00 0.355 0.00629 -0.0128 0.5006 1.0000 Value13= 2.50 0.408 0.00655 -0.0120 0.4642 1.0000 Value14= 3.00 0.461 0.00686 -0.0114 0.4272 1.0000 Value15= 3.50 0.513 0.00718 -0.0109 0.3931 1.0000 Value16= 4.00 0.566 0.00757 -0.0103 0.3552 1.0000 Value17= 4.50 0.617 0.00801 -0.0096 0.3168 1.0000 Value18= 5.00 0.667 0.00850 -0.0084 0.2767 1.0000 Value19= 5.50 0.715 0.00904 -0.0070 0.2393 1.0000 Value20= 6.00 0.765 0.00975 -0.0063 0.1933 1.0000 Value21= 6.50 0.817 0.01048 -0.0060 0.1540 1.0000 Value22= 7.00 0.869 0.01125 -0.0059 0.1224 1.0000 Value23= 7.50 0.921 0.01203 -0.0058 0.0964 1.0000 Value24= 8.00 0.973 0.01288 -0.0058 0.0750 1.0000 Value25= 8.50 1.024 0.01386 -0.0058 0.0552 1.0000 Value26= 9.00 1.074 0.01506 -0.0058 0.0326 1.0000 Value27= 9.50 1.121 0.01653 -0.0055 0.0183 1.0000 Value28= 10.00 1.166 0.01816 -0.0051 0.0138 1.0000 Value29= 10.50 1.206 0.02045 -0.0044 0.0110 1.0000 Value30= 11.00 1.239 0.02310 -0.0035 0.0097 1.0000 Value31= 11.50 1.270 0.02550 -0.0028 0.0090 1.0000 Value32= 12.00 1.283 0.02884 -0.0016 0.0084 1.0000 Value33= 12.50 1.287 0.03344 -0.0017 0.0079 1.0000 Value34= 13.00 1.283 0.03940 -0.0031 0.0073 1.0000 Value35= 13.50 1.267 0.04765 -0.0064 0.0069 1.0000 Value36= 14.00 1.243 0.05801 -0.0115 0.0066 1.0000 Value37= 14.50 1.214 0.07036 -0.0184 0.0064 1.0000 [Set1-Polar5] Re-Nr=1000000 ReynoldsNumber=1000000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=33 ; Alpha Cl Cd Cm T.U. T.L. Value01= -3.50 -0.312 0.00983 -0.0032 0.7186 0.0065 Value02= -3.00 -0.257 0.00938 -0.0027 0.7044 0.0081 Value03= -2.50 -0.203 0.00854 -0.0017 0.6889 0.0206 Value04= -2.00 -0.150 0.00767 -0.0013 0.6734 0.1525 Value05= -1.50 -0.096 0.00700 -0.0010 0.6551 0.2906 Value06= -1.00 -0.041 0.00657 -0.0008 0.6351 0.3964 Value07= -0.50 0.014 0.00623 -0.0005 0.6130 0.5014 Value08= 0.00 0.069 0.00598 -0.0003 0.5871 0.5939 Value09= 0.50 0.124 0.00572 0.0001 0.5600 0.6968 Value10= 1.00 0.175 0.00532 0.0013 0.5290 0.8464 Value11= 1.50 0.245 0.00520 -0.0011 0.4903 0.9883 Value12= 2.00 0.343 0.00548 -0.0104 0.4490 0.9978 Value13= 2.50 0.413 0.00574 -0.0135 0.4106 1.0000 Value14= 3.00 0.466 0.00600 -0.0129 0.3808 1.0000 Value15= 3.50 0.519 0.00632 -0.0123 0.3455 1.0000 Value16= 4.00 0.572 0.00668 -0.0118 0.3091 1.0000 Value17= 4.50 0.625 0.00712 -0.0114 0.2697 1.0000 Value18= 5.00 0.677 0.00765 -0.0111 0.2229 1.0000 Value19= 5.50 0.730 0.00822 -0.0107 0.1826 1.0000 Value20= 6.00 0.782 0.00880 -0.0103 0.1489 1.0000 Value21= 7.00 0.869 0.01002 -0.0058 0.0976 1.0000 Value22= 7.50 0.922 0.01072 -0.0057 0.0762 1.0000 Value23= 8.00 0.974 0.01156 -0.0058 0.0543 1.0000 Value24= 8.50 1.026 0.01248 -0.0058 0.0343 1.0000 Value25= 9.00 1.076 0.01370 -0.0058 0.0159 1.0000 Value26= 9.50 1.125 0.01514 -0.0055 0.0106 1.0000 Value27= 10.00 1.173 0.01635 -0.0053 0.0095 1.0000 Value28= 10.50 1.220 0.01764 -0.0050 0.0087 1.0000 Value29= 11.00 1.263 0.01919 -0.0046 0.0080 1.0000 Value30= 11.50 1.301 0.02122 -0.0038 0.0073 1.0000 Value31= 12.00 1.319 0.02500 -0.0024 0.0064 1.0000 Value32= 12.50 1.280 0.03361 -0.0013 0.0059 1.0000 Value33= 13.00 1.272 0.04022 -0.0029 0.0056 1.0000