[Airfoil] ; obsolete: Airfoilname=MH 64 ; new: Description1=MH 64 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=28 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.50 -0.379 0.02003 -0.0237 1.0000 0.0241 Value02= -3.00 -0.239 0.01367 -0.0218 1.0000 0.3135 Value03= -2.50 -0.171 0.01251 -0.0254 0.9865 0.6002 Value04= -2.00 -0.108 0.01201 -0.0257 0.9504 0.7850 Value05= -1.50 0.001 0.01157 -0.0332 0.9475 0.9921 Value06= -1.00 0.155 0.01362 -0.0513 0.9058 0.9714 Value07= -0.50 0.273 0.01430 -0.0623 0.8756 0.9696 Value08= 0.00 0.375 0.01485 -0.0701 0.8434 0.9634 Value09= 0.50 0.475 0.01520 -0.0769 0.8087 0.9529 Value10= 1.00 0.570 0.01543 -0.0826 0.7681 0.9443 Value11= 1.50 0.656 0.01557 -0.0868 0.7218 0.9400 Value12= 2.00 0.722 0.01556 -0.0872 0.6652 0.9456 Value13= 2.50 0.770 0.01557 -0.0852 0.6085 0.9556 Value14= 3.00 0.801 0.01558 -0.0805 0.5463 0.9710 Value15= 3.50 0.823 0.01576 -0.0741 0.4856 0.9846 Value16= 4.00 0.839 0.01611 -0.0671 0.4243 0.9959 Value17= 4.50 0.853 0.01665 -0.0599 0.3728 1.0000 Value18= 6.00 0.869 0.01900 -0.0330 0.2261 1.0000 Value19= 6.50 0.858 0.01943 -0.0216 0.1698 1.0000 Value20= 7.00 0.865 0.02034 -0.0125 0.1298 1.0000 Value21= 7.50 0.877 0.02247 -0.0049 0.0757 1.0000 Value22= 8.00 0.892 0.02574 0.0015 0.0423 1.0000 Value23= 8.50 0.912 0.02891 0.0062 0.0284 1.0000 Value24= 9.00 0.936 0.03232 0.0101 0.0211 1.0000 Value25= 9.50 0.961 0.03727 0.0135 0.0171 1.0000 Value26= 10.00 0.973 0.04239 0.0175 0.0148 1.0000 Value27= 10.50 0.967 0.04811 0.0222 0.0137 1.0000 Value28= 11.00 0.947 0.05500 0.0245 0.0130 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= -5.00 -0.430 0.01909 -0.0234 1.0000 0.0107 Value02= -4.50 -0.376 0.01642 -0.0234 1.0000 0.0135 Value03= -4.00 -0.306 0.01404 -0.0269 0.9786 0.0194 Value04= -3.50 -0.240 0.01255 -0.0290 0.9476 0.0368 Value05= -3.00 -0.189 0.01114 -0.0279 0.9160 0.2323 Value06= -2.00 -0.100 0.00972 -0.0227 0.8635 0.5857 Value07= -1.00 -0.014 0.00864 -0.0145 0.8196 0.8945 Value08= -0.50 0.103 0.00853 -0.0260 0.8021 1.0000 Value09= 0.00 0.149 0.00859 -0.0239 0.7763 1.0000 Value10= 0.50 0.198 0.00867 -0.0220 0.7508 1.0000 Value11= 1.00 0.246 0.00876 -0.0202 0.7239 1.0000 Value12= 1.50 0.297 0.00886 -0.0186 0.6938 1.0000 Value13= 2.00 0.348 0.00900 -0.0171 0.6597 1.0000 Value14= 2.50 0.399 0.00919 -0.0159 0.6199 1.0000 Value15= 3.00 0.451 0.00947 -0.0147 0.5733 1.0000 Value16= 3.50 0.503 0.00986 -0.0138 0.5204 1.0000 Value17= 4.00 0.555 0.01037 -0.0131 0.4625 1.0000 Value18= 4.50 0.607 0.01098 -0.0125 0.4036 1.0000 Value19= 5.00 0.660 0.01167 -0.0121 0.3481 1.0000 Value20= 5.50 0.712 0.01247 -0.0118 0.2871 1.0000 Value21= 6.00 0.763 0.01347 -0.0116 0.2137 1.0000 Value22= 6.50 0.813 0.01468 -0.0115 0.1384 1.0000 Value23= 7.00 0.862 0.01622 -0.0112 0.0677 1.0000 Value24= 7.50 0.908 0.01872 -0.0104 0.0251 1.0000 Value25= 8.00 0.949 0.02162 -0.0092 0.0160 1.0000 Value26= 8.50 0.986 0.02505 -0.0075 0.0123 1.0000 Value27= 9.00 1.022 0.02917 -0.0057 0.0101 1.0000 Value28= 9.50 1.055 0.03378 -0.0041 0.0087 1.0000 Value29= 10.00 1.079 0.03986 -0.0025 0.0078 1.0000 Value30= 10.50 1.089 0.04768 -0.0015 0.0071 1.0000 Value31= 11.00 1.073 0.05657 -0.0014 0.0069 1.0000 Value32= 11.50 1.041 0.06713 -0.0062 0.0069 1.0000 Value33= 12.00 0.999 0.08183 -0.0183 0.0070 1.0000 [Set1-Polar3] Re-Nr=400000 ReynoldsNumber=400000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=35 ; Alpha Cl Cd Cm T.U. T.L. Value01= -5.00 -0.417 0.01745 -0.0250 0.9395 0.0080 Value02= -4.50 -0.374 0.01360 -0.0209 0.9094 0.0094 Value03= -4.00 -0.327 0.01207 -0.0185 0.8846 0.0116 Value04= -3.50 -0.277 0.01118 -0.0169 0.8635 0.0137 Value05= -3.00 -0.226 0.01038 -0.0156 0.8427 0.0215 Value06= -2.50 -0.175 0.00916 -0.0146 0.8235 0.1939 Value07= -2.00 -0.123 0.00848 -0.0140 0.8043 0.3373 Value08= -1.50 -0.071 0.00789 -0.0131 0.7837 0.4778 Value09= -1.00 -0.021 0.00724 -0.0119 0.7636 0.6412 Value10= -0.50 0.028 0.00661 -0.0097 0.7423 0.8045 Value11= 0.00 0.091 0.00622 -0.0099 0.7198 0.9747 Value12= 0.50 0.184 0.00628 -0.0178 0.6906 1.0000 Value13= 1.00 0.236 0.00640 -0.0168 0.6602 1.0000 Value14= 1.50 0.287 0.00657 -0.0158 0.6249 1.0000 Value15= 2.00 0.339 0.00680 -0.0149 0.5837 1.0000 Value16= 2.50 0.392 0.00711 -0.0141 0.5353 1.0000 Value17= 3.00 0.444 0.00749 -0.0135 0.4827 1.0000 Value18= 3.50 0.497 0.00790 -0.0130 0.4347 1.0000 Value19= 4.00 0.551 0.00840 -0.0126 0.3806 1.0000 Value20= 4.50 0.604 0.00896 -0.0124 0.3265 1.0000 Value21= 5.00 0.657 0.00971 -0.0123 0.2562 1.0000 Value22= 5.50 0.710 0.01042 -0.0122 0.2044 1.0000 Value23= 6.00 0.762 0.01133 -0.0121 0.1424 1.0000 Value24= 6.50 0.814 0.01240 -0.0121 0.0849 1.0000 Value25= 7.00 0.863 0.01401 -0.0118 0.0229 1.0000 Value26= 7.50 0.911 0.01588 -0.0111 0.0124 1.0000 Value27= 8.00 0.957 0.01796 -0.0104 0.0097 1.0000 Value28= 8.50 1.000 0.02049 -0.0093 0.0079 1.0000 Value29= 9.00 1.033 0.02499 -0.0070 0.0067 1.0000 Value30= 9.50 1.065 0.02999 -0.0050 0.0062 1.0000 Value31= 10.00 1.095 0.03455 -0.0036 0.0054 1.0000 Value32= 10.50 1.115 0.04011 -0.0023 0.0048 1.0000 Value33= 11.00 1.116 0.04657 -0.0010 0.0044 1.0000 Value34= 11.50 1.098 0.05459 -0.0022 0.0041 1.0000 Value35= 12.00 1.067 0.06546 -0.0084 0.0041 1.0000 [Set1-Polar4] Re-Nr=600000 ReynoldsNumber=600000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=35 ; Alpha Cl Cd Cm T.U. T.L. Value01= -5.00 -0.441 0.01585 -0.0185 0.8885 0.0058 Value02= -4.50 -0.391 0.01388 -0.0169 0.8676 0.0070 Value03= -4.00 -0.342 0.01105 -0.0144 0.8471 0.0096 Value04= -3.50 -0.290 0.01016 -0.0133 0.8273 0.0111 Value05= -3.00 -0.236 0.00959 -0.0126 0.8090 0.0131 Value06= -2.50 -0.181 0.00899 -0.0120 0.7908 0.0345 Value07= -2.00 -0.129 0.00782 -0.0116 0.7722 0.2583 Value08= -1.50 -0.075 0.00732 -0.0112 0.7531 0.3713 Value09= -1.00 -0.022 0.00684 -0.0108 0.7313 0.4986 Value10= -0.50 0.031 0.00626 -0.0100 0.7093 0.6599 Value11= 0.00 0.082 0.00576 -0.0086 0.6847 0.8077 Value12= 0.50 0.140 0.00538 -0.0081 0.6579 0.9784 Value13= 1.00 0.234 0.00554 -0.0166 0.6179 1.0000 Value14= 1.50 0.287 0.00575 -0.0158 0.5773 1.0000 Value15= 2.00 0.339 0.00600 -0.0150 0.5357 1.0000 Value16= 2.50 0.391 0.00632 -0.0142 0.4869 1.0000 Value17= 3.00 0.443 0.00669 -0.0135 0.4358 1.0000 Value18= 3.50 0.496 0.00711 -0.0130 0.3844 1.0000 Value19= 4.00 0.549 0.00754 -0.0127 0.3402 1.0000 Value20= 4.50 0.602 0.00821 -0.0125 0.2689 1.0000 Value21= 5.00 0.656 0.00881 -0.0124 0.2184 1.0000 Value22= 5.50 0.709 0.00953 -0.0123 0.1642 1.0000 Value23= 6.00 0.762 0.01036 -0.0123 0.1126 1.0000 Value24= 6.50 0.813 0.01161 -0.0123 0.0423 1.0000 Value25= 7.00 0.864 0.01293 -0.0119 0.0139 1.0000 Value26= 7.50 0.914 0.01437 -0.0115 0.0099 1.0000 Value27= 8.00 0.963 0.01615 -0.0109 0.0078 1.0000 Value28= 8.50 1.000 0.02008 -0.0090 0.0063 1.0000 Value29= 9.00 1.043 0.02240 -0.0080 0.0055 1.0000 Value30= 9.50 1.080 0.02535 -0.0067 0.0049 1.0000 Value31= 10.00 1.113 0.02907 -0.0053 0.0043 1.0000 Value32= 10.50 1.138 0.03375 -0.0038 0.0039 1.0000 Value33= 11.00 1.140 0.04126 -0.0017 0.0033 1.0000 Value34= 11.50 1.082 0.05681 -0.0030 0.0027 1.0000 Value35= 12.00 1.048 0.06852 -0.0107 0.0027 1.0000 [Set1-Polar5] Re-Nr=1000000 ReynoldsNumber=1000000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=31 ; Alpha Cl Cd Cm T.U. T.L. Value01= -5.00 -0.455 0.01372 -0.0146 0.8425 0.0045 Value02= -4.50 -0.403 0.01180 -0.0133 0.8243 0.0052 Value03= -4.00 -0.350 0.01070 -0.0125 0.8052 0.0067 Value04= -3.50 -0.298 0.00918 -0.0112 0.7878 0.0092 Value05= -3.00 -0.242 0.00863 -0.0107 0.7703 0.0101 Value06= -2.00 -0.133 0.00741 -0.0100 0.7339 0.1311 Value07= -1.50 -0.079 0.00669 -0.0098 0.7143 0.2827 Value08= -1.00 -0.024 0.00636 -0.0097 0.6903 0.3722 Value09= -0.50 0.032 0.00601 -0.0096 0.6655 0.4821 Value10= 0.00 0.086 0.00558 -0.0093 0.6387 0.6264 Value11= 0.50 0.139 0.00526 -0.0088 0.6062 0.7547 Value12= 1.00 0.188 0.00483 -0.0068 0.5691 0.9198 Value13= 1.50 0.283 0.00500 -0.0152 0.5168 0.9991 Value14= 2.00 0.341 0.00528 -0.0159 0.4686 1.0000 Value15= 2.50 0.394 0.00560 -0.0152 0.4203 1.0000 Value16= 3.00 0.445 0.00596 -0.0142 0.3724 1.0000 Value17= 3.50 0.496 0.00630 -0.0133 0.3319 1.0000 Value18= 4.00 0.548 0.00687 -0.0128 0.2665 1.0000 Value19= 4.50 0.602 0.00735 -0.0126 0.2195 1.0000 Value20= 5.00 0.655 0.00789 -0.0124 0.1770 1.0000 Value21= 5.50 0.709 0.00856 -0.0123 0.1279 1.0000 Value22= 6.00 0.762 0.00945 -0.0123 0.0725 1.0000 Value23= 6.50 0.813 0.01069 -0.0123 0.0167 1.0000 Value24= 7.00 0.866 0.01162 -0.0120 0.0097 1.0000 Value25= 8.00 0.966 0.01498 -0.0109 0.0058 1.0000 Value26= 8.50 1.014 0.01633 -0.0106 0.0050 1.0000 Value27= 9.00 1.060 0.01821 -0.0099 0.0043 1.0000 Value28= 9.50 1.100 0.02070 -0.0088 0.0039 1.0000 Value29= 10.00 1.134 0.02440 -0.0071 0.0035 1.0000 Value30= 11.50 1.166 0.04068 -0.0015 0.0017 1.0000 Value31= 12.00 1.152 0.04798 -0.0032 0.0015 1.0000