[Airfoil] Airfoilname=mh44 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=33 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.374 0.01846 -0.0140 1.0000 0.0329 Value02= -3.50 -0.344 0.01679 -0.0107 1.0000 0.0597 Value03= -3.00 -0.275 0.01465 -0.0147 0.9831 0.3572 Value04= -2.50 -0.210 0.01352 -0.0167 0.9599 0.6596 Value05= -2.00 -0.144 0.01305 -0.0160 0.9402 0.8776 Value06= -1.50 0.023 0.01308 -0.0371 0.9558 1.0000 Value07= -1.00 0.100 0.01319 -0.0426 0.9196 1.0000 Value08= -0.50 0.161 0.01344 -0.0441 0.8831 1.0000 Value09= 0.00 0.212 0.01372 -0.0427 0.8472 1.0000 Value10= 0.50 0.257 0.01398 -0.0398 0.8138 1.0000 Value11= 1.00 0.300 0.01416 -0.0364 0.7809 1.0000 Value12= 1.50 0.344 0.01424 -0.0327 0.7488 1.0000 Value13= 2.00 0.389 0.01423 -0.0290 0.7169 1.0000 Value14= 2.50 0.435 0.01423 -0.0257 0.6825 1.0000 Value15= 3.00 0.482 0.01433 -0.0229 0.6445 1.0000 Value16= 3.50 0.531 0.01456 -0.0204 0.6027 1.0000 Value17= 4.00 0.581 0.01492 -0.0184 0.5572 1.0000 Value18= 4.50 0.630 0.01540 -0.0165 0.5092 1.0000 Value19= 5.00 0.680 0.01601 -0.0149 0.4576 1.0000 Value20= 5.50 0.729 0.01675 -0.0133 0.4030 1.0000 Value21= 6.00 0.777 0.01772 -0.0118 0.3476 1.0000 Value22= 6.50 0.823 0.01884 -0.0103 0.2889 1.0000 Value23= 7.00 0.867 0.02023 -0.0088 0.2313 1.0000 Value24= 7.50 0.909 0.02177 -0.0073 0.1746 1.0000 Value25= 8.00 0.948 0.02350 -0.0060 0.1195 1.0000 Value26= 8.50 0.982 0.02646 -0.0037 0.0751 1.0000 Value27= 9.00 1.012 0.03009 -0.0011 0.0484 1.0000 Value28= 9.50 1.044 0.03395 0.0012 0.0355 1.0000 Value29= 10.00 1.073 0.03816 0.0033 0.0282 1.0000 Value30= 10.50 1.094 0.04398 0.0056 0.0234 1.0000 Value31= 11.00 1.107 0.04908 0.0073 0.0201 1.0000 Value32= 11.50 1.100 0.05553 0.0093 0.0185 1.0000 Value33= 12.00 1.076 0.06402 0.0084 0.0177 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 -0.310 0.01449 -0.0252 0.9708 0.0187 Value02= -3.50 -0.242 0.01302 -0.0277 0.9505 0.0429 Value03= -3.00 -0.188 0.01141 -0.0280 0.9271 0.3153 Value04= -2.50 -0.142 0.01061 -0.0259 0.9026 0.5095 Value05= -2.00 -0.097 0.01008 -0.0227 0.8794 0.6392 Value06= -1.50 -0.059 0.00931 -0.0170 0.8575 0.8437 Value07= -1.00 0.034 0.00931 -0.0224 0.8420 0.9666 Value08= -0.50 0.117 0.00923 -0.0275 0.8205 1.0000 Value09= 0.00 0.161 0.00917 -0.0248 0.7929 1.0000 Value10= 0.50 0.209 0.00914 -0.0226 0.7647 1.0000 Value11= 1.00 0.258 0.00913 -0.0207 0.7338 1.0000 Value12= 1.50 0.308 0.00920 -0.0190 0.6991 1.0000 Value13= 2.00 0.359 0.00937 -0.0177 0.6607 1.0000 Value14= 2.50 0.411 0.00963 -0.0167 0.6199 1.0000 Value15= 3.00 0.464 0.00994 -0.0158 0.5772 1.0000 Value16= 3.50 0.516 0.01033 -0.0150 0.5328 1.0000 Value17= 4.00 0.569 0.01079 -0.0142 0.4864 1.0000 Value18= 4.50 0.621 0.01130 -0.0136 0.4414 1.0000 Value19= 5.00 0.672 0.01191 -0.0129 0.3906 1.0000 Value20= 5.50 0.723 0.01260 -0.0122 0.3371 1.0000 Value21= 6.00 0.773 0.01341 -0.0115 0.2815 1.0000 Value22= 6.50 0.821 0.01440 -0.0108 0.2219 1.0000 Value23= 7.00 0.869 0.01550 -0.0100 0.1653 1.0000 Value24= 7.50 0.915 0.01673 -0.0092 0.1167 1.0000 Value25= 8.00 0.959 0.01828 -0.0080 0.0724 1.0000 Value26= 8.50 0.997 0.02072 -0.0060 0.0381 1.0000 Value27= 9.00 1.029 0.02362 -0.0036 0.0249 1.0000 Value28= 9.50 1.064 0.02597 -0.0017 0.0194 1.0000 Value29= 10.00 1.089 0.02949 0.0010 0.0156 1.0000 Value30= 10.50 1.116 0.03273 0.0033 0.0137 1.0000 Value31= 11.00 1.133 0.03653 0.0061 0.0123 1.0000 Value32= 11.50 1.140 0.04150 0.0088 0.0112 1.0000 Value33= 12.00 1.132 0.04843 0.0103 0.0105 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 -0.321 0.01257 -0.0186 0.9038 0.0098 Value02= -3.50 -0.273 0.01149 -0.0165 0.8852 0.0132 Value03= -3.00 -0.223 0.01064 -0.0148 0.8674 0.0275 Value04= -2.50 -0.174 0.00934 -0.0134 0.8494 0.2343 Value05= -2.00 -0.125 0.00849 -0.0121 0.8309 0.4085 Value06= -1.50 -0.076 0.00782 -0.0106 0.8113 0.5554 Value07= -1.00 -0.031 0.00690 -0.0077 0.7900 0.7601 Value08= -0.50 0.019 0.00633 -0.0051 0.7664 0.9319 Value09= 0.00 0.126 0.00651 -0.0152 0.7355 0.9909 Value10= 0.50 0.189 0.00658 -0.0167 0.7003 1.0000 Value11= 1.00 0.243 0.00672 -0.0162 0.6631 1.0000 Value12= 1.50 0.296 0.00692 -0.0157 0.6215 1.0000 Value13= 2.00 0.350 0.00716 -0.0153 0.5839 1.0000 Value14= 2.50 0.404 0.00743 -0.0149 0.5429 1.0000 Value15= 3.00 0.458 0.00776 -0.0145 0.5013 1.0000 Value16= 3.50 0.511 0.00813 -0.0141 0.4586 1.0000 Value17= 4.00 0.564 0.00857 -0.0137 0.4130 1.0000 Value18= 4.50 0.617 0.00902 -0.0133 0.3709 1.0000 Value19= 5.00 0.669 0.00962 -0.0129 0.3162 1.0000 Value20= 5.50 0.721 0.01034 -0.0125 0.2569 1.0000 Value21= 6.00 0.771 0.01115 -0.0121 0.2004 1.0000 Value22= 6.50 0.821 0.01197 -0.0115 0.1569 1.0000 Value23= 7.00 0.870 0.01291 -0.0109 0.1115 1.0000 Value24= 7.50 0.918 0.01399 -0.0101 0.0718 1.0000 Value25= 8.00 0.963 0.01547 -0.0090 0.0321 1.0000 Value26= 8.50 1.006 0.01711 -0.0076 0.0174 1.0000 Value27= 9.00 1.047 0.01890 -0.0060 0.0136 1.0000 Value28= 9.50 1.085 0.02091 -0.0042 0.0115 1.0000 Value29= 10.00 1.109 0.02436 -0.0011 0.0099 1.0000 Value30= 10.50 1.140 0.02676 0.0010 0.0090 1.0000 Value31= 11.00 1.159 0.02971 0.0039 0.0082 1.0000 Value32= 11.50 1.169 0.03344 0.0067 0.0075 1.0000 Value33= 12.00 1.172 0.03830 0.0084 0.0070 1.0000 [Set1-Polar4] Re-Nr=600000 ReynoldsNumber=600000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=31 ; Alpha Cl Cd Cm T.U. T.L. Value01= -3.00 -0.238 0.00983 -0.0103 0.8402 0.0135 Value02= -2.50 -0.184 0.00901 -0.0095 0.8229 0.0759 Value03= -2.00 -0.133 0.00792 -0.0089 0.8040 0.2788 Value04= -1.50 -0.081 0.00711 -0.0082 0.7826 0.4575 Value05= -1.00 -0.029 0.00661 -0.0073 0.7572 0.5831 Value06= -0.50 0.019 0.00588 -0.0053 0.7296 0.7709 Value07= 0.00 0.071 0.00541 -0.0035 0.6952 0.9504 Value08= 0.50 0.172 0.00571 -0.0130 0.6564 0.9906 Value09= 1.00 0.240 0.00587 -0.0157 0.6172 1.0000 Value10= 1.50 0.295 0.00607 -0.0154 0.5779 1.0000 Value11= 2.00 0.349 0.00631 -0.0151 0.5379 1.0000 Value12= 2.50 0.403 0.00659 -0.0149 0.4975 1.0000 Value13= 3.00 0.457 0.00690 -0.0146 0.4567 1.0000 Value14= 3.50 0.511 0.00726 -0.0143 0.4136 1.0000 Value15= 4.00 0.564 0.00764 -0.0140 0.3739 1.0000 Value16= 4.50 0.617 0.00813 -0.0137 0.3243 1.0000 Value17= 5.00 0.669 0.00876 -0.0133 0.2658 1.0000 Value18= 5.50 0.721 0.00941 -0.0129 0.2160 1.0000 Value19= 6.00 0.772 0.01015 -0.0124 0.1661 1.0000 Value20= 6.50 0.823 0.01090 -0.0119 0.1272 1.0000 Value21= 7.00 0.872 0.01183 -0.0112 0.0857 1.0000 Value22= 7.50 0.919 0.01296 -0.0104 0.0434 1.0000 Value23= 8.00 0.965 0.01440 -0.0092 0.0156 1.0000 Value24= 8.50 1.011 0.01559 -0.0082 0.0123 1.0000 Value25= 9.00 1.050 0.01767 -0.0063 0.0099 1.0000 Value26= 9.50 1.092 0.01910 -0.0049 0.0091 1.0000 Value27= 10.00 1.130 0.02090 -0.0033 0.0082 1.0000 Value28= 10.50 1.163 0.02312 -0.0013 0.0074 1.0000 Value29= 11.00 1.184 0.02633 0.0018 0.0066 1.0000 Value30= 11.50 1.179 0.03159 0.0065 0.0059 1.0000 Value31= 12.00 1.170 0.03803 0.0092 0.0057 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= -3.00 -0.247 0.00912 -0.0078 0.8070 0.0079 Value02= -2.50 -0.192 0.00835 -0.0071 0.7882 0.0142 Value03= -2.00 -0.138 0.00741 -0.0067 0.7662 0.1584 Value04= -1.50 -0.084 0.00677 -0.0065 0.7382 0.2945 Value05= -1.00 -0.031 0.00616 -0.0062 0.7090 0.4534 Value06= -0.50 0.022 0.00570 -0.0057 0.6732 0.6045 Value07= 0.00 0.075 0.00536 -0.0049 0.6385 0.7300 Value08= 0.50 0.122 0.00488 -0.0026 0.6029 0.8983 Value09= 1.00 0.211 0.00504 -0.0095 0.5619 0.9854 Value10= 1.50 0.294 0.00530 -0.0157 0.5195 0.9981 Value11= 2.00 0.349 0.00552 -0.0156 0.4811 1.0000 Value12= 2.50 0.404 0.00577 -0.0153 0.4425 1.0000 Value13= 3.00 0.458 0.00604 -0.0151 0.4073 1.0000 Value14= 3.50 0.512 0.00637 -0.0148 0.3667 1.0000 Value15= 4.00 0.565 0.00688 -0.0146 0.3060 1.0000 Value16= 4.50 0.618 0.00734 -0.0142 0.2600 1.0000 Value17= 5.00 0.671 0.00789 -0.0139 0.2136 1.0000 Value18= 5.50 0.722 0.00850 -0.0134 0.1663 1.0000 Value19= 6.00 0.774 0.00913 -0.0129 0.1288 1.0000 Value20= 6.50 0.824 0.00990 -0.0123 0.0896 1.0000 Value21= 7.00 0.873 0.01093 -0.0116 0.0439 1.0000 Value22= 7.50 0.920 0.01208 -0.0106 0.0139 1.0000 Value23= 8.00 0.968 0.01315 -0.0095 0.0096 1.0000 Value24= 8.50 1.016 0.01404 -0.0087 0.0087 1.0000 Value25= 9.00 1.063 0.01508 -0.0076 0.0080 1.0000 Value26= 9.50 1.107 0.01633 -0.0065 0.0073 1.0000 Value27= 10.00 1.147 0.01812 -0.0047 0.0066 1.0000 Value28= 10.50 1.153 0.02396 0.0007 0.0055 1.0000 Value29= 11.00 1.181 0.02627 0.0029 0.0051 1.0000 Value30= 11.50 1.197 0.02914 0.0059 0.0048 1.0000 Value31= 12.00 1.208 0.03258 0.0078 0.0045 1.0000