[Airfoil] ; obsolete: Airfoilname=MH 18 ; new: Description1=MH 18 NumberSets=1 [Set1] Origin=Berechnung: X-Foil Description1=Bestandteil von 'Profile für Nurflügelmodelle' NumberPolars=5 [Set1-Polar1] Re-Nr=200000 ReynoldsNumber=200000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=28 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.220 0.01720 -0.0360 0.7729 0.0236 Value02= -3.50 -0.174 0.01570 -0.0337 0.7638 0.0422 Value03= -3.00 -0.127 0.01455 -0.0319 0.7544 0.1187 Value04= -2.50 -0.080 0.01364 -0.0306 0.7458 0.2812 Value05= -2.00 -0.044 0.01228 -0.0272 0.7364 0.5937 Value06= -1.00 0.204 0.01190 -0.0517 0.7265 0.9743 Value07= -0.50 0.277 0.01177 -0.0558 0.7176 0.9955 Value08= 0.00 0.339 0.01175 -0.0578 0.7089 1.0000 Value09= 0.50 0.387 0.01184 -0.0569 0.6991 1.0000 Value10= 1.00 0.435 0.01192 -0.0559 0.6897 1.0000 Value11= 1.50 0.484 0.01204 -0.0549 0.6795 1.0000 Value12= 2.00 0.532 0.01213 -0.0536 0.6696 1.0000 Value13= 2.50 0.581 0.01226 -0.0524 0.6585 1.0000 Value14= 3.00 0.629 0.01233 -0.0510 0.6472 1.0000 Value15= 3.50 0.678 0.01236 -0.0495 0.6349 1.0000 Value16= 4.00 0.726 0.01230 -0.0478 0.6204 1.0000 Value17= 4.50 0.775 0.01224 -0.0462 0.6041 1.0000 Value18= 5.00 0.824 0.01214 -0.0444 0.5840 1.0000 Value19= 5.50 0.872 0.01204 -0.0425 0.5548 1.0000 Value20= 6.00 0.918 0.01221 -0.0405 0.5155 1.0000 Value21= 6.50 0.960 0.01286 -0.0381 0.4559 1.0000 Value22= 9.00 1.009 0.02405 -0.0070 0.0195 1.0000 Value23= 9.50 0.998 0.02725 0.0002 0.0130 1.0000 Value24= 10.00 0.999 0.03038 0.0049 0.0100 1.0000 Value25= 10.50 0.988 0.03484 0.0096 0.0079 1.0000 Value26= 11.00 0.994 0.03855 0.0126 0.0065 1.0000 Value27= 11.50 1.003 0.04239 0.0153 0.0057 1.0000 Value28= 12.00 1.018 0.04663 0.0179 0.0047 1.0000 [Set1-Polar2] Re-Nr=400000 ReynoldsNumber=400000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=28 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.248 0.01358 -0.0261 0.7414 0.0131 Value02= -3.50 -0.197 0.01266 -0.0251 0.7338 0.0190 Value03= -3.00 -0.148 0.01143 -0.0234 0.7255 0.0569 Value04= -2.50 -0.096 0.01079 -0.0227 0.7179 0.1417 Value05= -2.00 -0.047 0.01002 -0.0219 0.7105 0.2922 Value06= -1.50 -0.005 0.00887 -0.0195 0.7022 0.5618 Value07= -1.00 0.030 0.00758 -0.0147 0.6951 0.8710 Value08= -0.50 0.182 0.00804 -0.0340 0.6884 0.9574 Value09= 0.00 0.268 0.00822 -0.0403 0.6813 0.9734 Value10= 0.50 0.337 0.00817 -0.0432 0.6736 0.9878 Value11= 1.00 0.406 0.00812 -0.0464 0.6643 0.9956 Value12= 1.50 0.475 0.00809 -0.0497 0.6556 1.0000 Value13= 2.00 0.526 0.00812 -0.0490 0.6455 1.0000 Value14= 2.50 0.577 0.00814 -0.0483 0.6349 1.0000 Value15= 3.00 0.628 0.00816 -0.0476 0.6228 1.0000 Value16= 3.50 0.679 0.00820 -0.0469 0.6083 1.0000 Value17= 4.00 0.730 0.00824 -0.0461 0.5888 1.0000 Value18= 4.50 0.781 0.00834 -0.0452 0.5647 1.0000 Value19= 5.00 0.831 0.00859 -0.0444 0.5301 1.0000 Value20= 5.50 0.878 0.00914 -0.0432 0.4748 1.0000 Value21= 6.00 0.922 0.01004 -0.0418 0.4090 1.0000 Value22= 6.50 0.961 0.01129 -0.0397 0.3261 1.0000 Value23= 9.50 1.011 0.02446 -0.0019 0.0046 1.0000 Value24= 10.00 0.998 0.02861 0.0041 0.0040 1.0000 Value25= 10.50 1.001 0.03215 0.0077 0.0036 1.0000 Value26= 11.00 1.010 0.03558 0.0104 0.0032 1.0000 Value27= 11.50 1.021 0.03920 0.0128 0.0030 1.0000 Value28= 12.00 1.031 0.04325 0.0150 0.0026 1.0000 [Set1-Polar3] Re-Nr=600000 ReynoldsNumber=600000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=28 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.258 0.01205 -0.0231 0.7225 0.0104 Value02= -3.50 -0.208 0.01098 -0.0218 0.7160 0.0144 Value03= -3.00 -0.156 0.01021 -0.0208 0.7077 0.0362 Value04= -2.50 -0.103 0.00963 -0.0203 0.7004 0.1024 Value05= -2.00 -0.051 0.00905 -0.0198 0.6933 0.2008 Value06= -1.50 -0.002 0.00828 -0.0189 0.6854 0.3778 Value07= -1.00 0.041 0.00723 -0.0165 0.6789 0.6352 Value08= -0.50 0.097 0.00621 -0.0159 0.6716 0.9354 Value09= 0.00 0.221 0.00667 -0.0302 0.6643 0.9621 Value10= 0.50 0.301 0.00682 -0.0354 0.6571 0.9718 Value11= 1.00 0.373 0.00689 -0.0390 0.6481 0.9812 Value12= 1.50 0.434 0.00681 -0.0402 0.6399 0.9918 Value13= 2.00 0.503 0.00682 -0.0435 0.6292 0.9952 Value14= 2.50 0.574 0.00681 -0.0470 0.6183 0.9990 Value15= 3.00 0.631 0.00683 -0.0476 0.6034 1.0000 Value16= 3.50 0.682 0.00690 -0.0470 0.5862 1.0000 Value17= 4.00 0.734 0.00704 -0.0465 0.5603 1.0000 Value18= 4.50 0.785 0.00728 -0.0460 0.5255 1.0000 Value19= 5.00 0.836 0.00775 -0.0456 0.4759 1.0000 Value20= 5.50 0.883 0.00855 -0.0448 0.4060 1.0000 Value21= 6.00 0.926 0.00979 -0.0435 0.3096 1.0000 Value22= 6.50 0.962 0.01137 -0.0412 0.2032 1.0000 Value23= 9.50 1.039 0.02302 -0.0060 0.0029 1.0000 Value24= 10.00 1.052 0.02597 -0.0032 0.0026 1.0000 Value25= 10.50 1.062 0.02940 -0.0007 0.0024 1.0000 Value26= 11.00 1.070 0.03316 0.0016 0.0022 1.0000 Value27= 11.50 1.078 0.03723 0.0037 0.0020 1.0000 Value28= 12.00 1.086 0.04165 0.0058 0.0019 1.0000 [Set1-Polar4] Re-Nr=1000000 ReynoldsNumber=1000000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=19 ; Alpha Cl Cd Cm T.U. T.L. Value01= 0.00 0.131 0.00511 -0.0111 0.6444 0.8781 Value02= 1.00 0.328 0.00550 -0.0294 0.6275 0.9703 Value03= 1.50 0.402 0.00564 -0.0334 0.6182 0.9767 Value04= 2.00 0.468 0.00567 -0.0357 0.6076 0.9831 Value05= 2.50 0.525 0.00567 -0.0363 0.5939 0.9916 Value06= 3.00 0.597 0.00574 -0.0400 0.5751 0.9941 Value07= 3.50 0.661 0.00586 -0.0423 0.5519 0.9960 Value08= 4.00 0.723 0.00612 -0.0442 0.5141 0.9975 Value09= 4.50 0.783 0.00662 -0.0458 0.4554 0.9988 Value10= 5.00 0.842 0.00715 -0.0473 0.4041 0.9997 Value11= 5.50 0.892 0.00835 -0.0474 0.2931 1.0000 Value12= 6.00 0.935 0.00948 -0.0463 0.2087 1.0000 Value13= 9.00 1.004 0.02016 -0.0092 0.0022 0.9922 Value14= 9.50 1.003 0.02243 -0.0031 0.0020 0.9923 Value15= 10.00 0.997 0.02538 0.0024 0.0018 0.9926 Value16= 10.50 0.993 0.02875 0.0068 0.0016 0.9928 Value17= 11.00 0.986 0.03282 0.0106 0.0015 0.9932 Value18= 11.50 0.994 0.03597 0.0129 0.0016 0.9934 Value19= 12.00 0.987 0.04075 0.0164 0.0014 0.9937 [Set1-Polar5] Re-Nr=2000000 ReynoldsNumber=2000000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=24 ; Alpha Cl Cd Cm T.U. T.L. Value01= -3.00 -0.171 0.00784 -0.0167 0.6573 0.0095 Value02= -2.50 -0.117 0.00748 -0.0164 0.6496 0.0264 Value03= -2.00 -0.063 0.00701 -0.0161 0.6449 0.0833 Value04= -1.50 -0.009 0.00665 -0.0159 0.6380 0.1474 Value05= -1.00 0.046 0.00635 -0.0158 0.6305 0.2155 Value06= -0.50 0.098 0.00581 -0.0154 0.6249 0.3585 Value07= 0.00 0.151 0.00539 -0.0150 0.6161 0.4907 Value08= 0.50 0.200 0.00473 -0.0137 0.6090 0.6922 Value09= 1.00 0.240 0.00400 -0.0104 0.5998 0.9111 Value10= 1.50 0.339 0.00419 -0.0199 0.5891 0.9713 Value11= 2.00 0.415 0.00439 -0.0245 0.5743 0.9751 Value12= 2.50 0.487 0.00459 -0.0281 0.5554 0.9781 Value13= 3.00 0.551 0.00482 -0.0303 0.5194 0.9825 Value14= 3.50 0.609 0.00509 -0.0311 0.4759 0.9900 Value15= 4.00 0.672 0.00546 -0.0332 0.4274 0.9927 Value16= 4.50 0.734 0.00586 -0.0353 0.3852 0.9939 Value17= 5.00 0.794 0.00666 -0.0372 0.2985 0.9952 Value18= 5.50 0.850 0.00770 -0.0388 0.2027 0.9966 Value19= 6.00 0.905 0.00889 -0.0401 0.1135 0.9979 Value20= 6.50 0.957 0.01028 -0.0410 0.0344 0.9990 Value21= 10.50 1.085 0.02450 0.0019 0.0014 1.0000 Value22= 11.00 1.107 0.02820 0.0026 0.0014 1.0000 Value23= 11.50 1.120 0.03192 0.0056 0.0013 1.0000 Value24= 12.00 1.132 0.03607 0.0084 0.0013 1.0000