; This is a polar exchange file (PEF) ; Comments start with a ';' in column 1, blank lines are allowed ; The 'PolarBrowser' application, a reader and converter is available ; in the software section at: ; http://www.MH-AeroTools.de/airfoils/ [Airfoil] Description1=MH 53 9.43% NumberSets=1 [Set1] Origin=PEFView Description1=XFLR Analysis, M=0.285 Description2=Copyright 2007 Martin Hepperle NumberPolars=5 [Set1-Polar1] ReynoldsNumber=500000 MachNumber=0.285 NumberPoints=50 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.210 0.00669 -0.0013 0.954 0.821 Value02=-1.750 -0.182 0.00670 -0.0005 0.949 0.853 Value03=-1.500 -0.154 0.00673 0.0002 0.944 0.872 Value04=-1.250 -0.126 0.00675 0.0010 0.938 0.886 Value05=-1.000 -0.099 0.00676 0.0019 0.932 0.897 Value06=-0.750 -0.073 0.00676 0.0029 0.926 0.906 Value07=-0.500 -0.046 0.00678 0.0038 0.919 0.915 Value08=-0.250 -0.019 0.00679 0.0047 0.912 0.922 Value09=0.000 0.008 0.00680 0.0056 0.905 0.929 Value10=0.250 0.036 0.00680 0.0063 0.896 0.935 Value11=0.500 0.064 0.00678 0.0068 0.886 0.941 Value12=0.750 0.093 0.00676 0.0072 0.876 0.946 Value13=1.000 0.123 0.00675 0.0072 0.862 0.951 Value14=1.250 0.154 0.00674 0.0070 0.848 0.956 Value15=1.500 0.186 0.00672 0.0064 0.829 0.959 Value16=1.750 0.221 0.00673 0.0054 0.803 0.962 Value17=2.000 0.255 0.00679 0.0045 0.772 0.966 Value18=2.250 0.288 0.00692 0.0038 0.734 0.970 Value19=2.500 0.324 0.00711 0.0023 0.687 0.972 Value20=2.750 0.357 0.00732 0.0013 0.640 0.975 Value21=3.000 0.390 0.00760 0.0003 0.585 0.978 Value22=3.250 0.424 0.00795 -0.0010 0.518 0.981 Value23=3.500 0.458 0.00836 -0.0023 0.444 0.983 Value24=3.750 0.491 0.00887 -0.0036 0.359 0.986 Value25=4.000 0.524 0.00946 -0.0050 0.271 0.989 Value26=4.250 0.557 0.01021 -0.0065 0.172 0.991 Value27=4.500 0.591 0.01092 -0.0080 0.097 0.993 Value28=4.750 0.623 0.01180 -0.0091 0.040 0.995 Value29=5.000 0.655 0.01263 -0.0101 0.024 0.997 Value30=5.250 0.689 0.01342 -0.0112 0.020 0.999 Value31=5.500 0.717 0.01425 -0.0110 0.018 1.000 Value32=5.750 0.736 0.01506 -0.0091 0.016 1.000 Value33=6.000 0.754 0.01586 -0.0072 0.013 1.000 Value34=6.500 0.787 0.01821 -0.0022 0.010 1.000 Value35=6.750 0.802 0.01977 0.0007 0.009 1.000 Value36=7.000 0.815 0.02148 0.0036 0.008 1.000 Value37=7.250 0.824 0.02399 0.0072 0.008 1.000 Value38=7.500 0.829 0.02653 0.0115 0.008 1.000 Value39=7.750 0.828 0.02936 0.0165 0.008 1.000 Value40=8.000 0.822 0.03259 0.0219 0.008 1.000 Value41=8.250 0.814 0.03582 0.0269 0.007 1.000 Value42=8.500 0.804 0.03935 0.0313 0.007 1.000 Value43=8.750 0.792 0.04318 0.0347 0.007 1.000 Value44=9.000 0.777 0.04661 0.0378 0.008 1.000 Value45=9.250 0.760 0.05038 0.0391 0.008 1.000 Value46=9.500 0.744 0.05476 0.0383 0.008 1.000 Value47=9.750 0.728 0.06016 0.0348 0.008 1.000 Value48=10.000 0.715 0.06716 0.0284 0.008 1.000 Value49=10.250 0.706 0.07560 0.0208 0.008 1.000 Value50=10.500 0.700 0.08292 0.0158 0.008 1.000 [Set1-Polar2] ReynoldsNumber=750000 MachNumber=0.285 NumberPoints=49 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.206 0.00551 -0.0009 0.934 0.729 Value02=-1.750 -0.184 0.00527 0.0009 0.929 0.791 Value03=-1.500 -0.159 0.00516 0.0022 0.923 0.827 Value04=-1.250 -0.133 0.00510 0.0033 0.916 0.851 Value05=-1.000 -0.107 0.00507 0.0041 0.910 0.867 Value06=-0.750 -0.080 0.00504 0.0049 0.904 0.881 Value07=-0.500 -0.053 0.00502 0.0055 0.897 0.891 Value08=-0.250 -0.026 0.00501 0.0062 0.889 0.900 Value09=0.000 0.001 0.00500 0.0068 0.880 0.909 Value10=0.250 0.028 0.00501 0.0075 0.869 0.917 Value11=0.500 0.056 0.00502 0.0081 0.856 0.924 Value12=0.750 0.083 0.00504 0.0087 0.842 0.930 Value13=1.000 0.110 0.00508 0.0093 0.824 0.935 Value14=1.250 0.137 0.00515 0.0100 0.800 0.941 Value15=1.500 0.164 0.00527 0.0107 0.769 0.946 Value16=1.750 0.190 0.00542 0.0114 0.739 0.950 Value17=2.000 0.217 0.00559 0.0120 0.705 0.955 Value18=2.250 0.245 0.00581 0.0123 0.665 0.959 Value19=2.500 0.274 0.00604 0.0123 0.623 0.963 Value20=2.750 0.303 0.00627 0.0123 0.581 0.966 Value21=3.000 0.332 0.00655 0.0122 0.530 0.970 Value22=3.250 0.364 0.00690 0.0113 0.470 0.972 Value23=3.750 0.427 0.00773 0.0096 0.338 0.978 Value24=4.000 0.461 0.00826 0.0080 0.259 0.979 Value25=4.250 0.492 0.00885 0.0072 0.182 0.982 Value26=4.500 0.526 0.00944 0.0056 0.118 0.983 Value27=4.750 0.558 0.01005 0.0045 0.065 0.985 Value28=5.000 0.590 0.01073 0.0035 0.028 0.987 Value29=5.250 0.623 0.01135 0.0027 0.018 0.989 Value30=5.750 0.689 0.01266 0.0008 0.013 0.993 Value31=6.000 0.722 0.01328 -0.0002 0.010 0.994 Value32=6.250 0.754 0.01405 -0.0009 0.008 0.996 Value33=6.750 0.812 0.01710 -0.0013 0.006 0.999 Value34=7.000 0.837 0.01879 -0.0004 0.005 1.000 Value35=7.250 0.851 0.01981 0.0022 0.005 1.000 Value36=7.500 0.858 0.02202 0.0062 0.005 1.000 Value37=7.750 0.860 0.02462 0.0109 0.004 1.000 Value38=8.000 0.856 0.02761 0.0164 0.004 1.000 Value39=8.250 0.846 0.03074 0.0223 0.004 1.000 Value40=8.500 0.834 0.03407 0.0278 0.004 1.000 Value41=8.750 0.821 0.03797 0.0322 0.004 1.000 Value42=9.000 0.806 0.04179 0.0359 0.004 1.000 Value43=9.250 0.789 0.04556 0.0383 0.004 1.000 Value44=9.500 0.772 0.04980 0.0386 0.004 1.000 Value45=9.750 0.755 0.05482 0.0364 0.004 1.000 Value46=10.000 0.741 0.06114 0.0312 0.004 1.000 Value47=10.250 0.729 0.06965 0.0230 0.004 1.000 Value48=10.500 0.721 0.07970 0.0161 0.005 1.000 Value49=10.750 0.712 0.08700 0.0116 0.005 1.000 [Set1-Polar3] ReynoldsNumber=1000000 MachNumber=0.285 NumberPoints=53 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.209 0.00514 0.0007 0.920 0.637 Value02=-1.750 -0.186 0.00478 0.0022 0.914 0.715 Value03=-1.500 -0.163 0.00451 0.0036 0.908 0.778 Value04=-1.250 -0.137 0.00438 0.0045 0.902 0.815 Value05=-1.000 -0.110 0.00431 0.0051 0.896 0.840 Value06=-0.750 -0.083 0.00427 0.0056 0.889 0.858 Value07=-0.500 -0.055 0.00424 0.0061 0.881 0.871 Value08=-0.250 -0.027 0.00421 0.0064 0.872 0.883 Value09=0.000 0.001 0.00420 0.0068 0.860 0.892 Value10=0.250 0.029 0.00420 0.0072 0.846 0.901 Value11=0.500 0.056 0.00422 0.0076 0.830 0.909 Value12=0.750 0.084 0.00427 0.0081 0.809 0.916 Value13=1.000 0.111 0.00436 0.0087 0.782 0.922 Value14=1.250 0.137 0.00450 0.0094 0.750 0.928 Value15=1.500 0.163 0.00466 0.0101 0.718 0.934 Value16=1.750 0.189 0.00483 0.0108 0.685 0.939 Value17=2.000 0.215 0.00503 0.0115 0.646 0.944 Value18=2.250 0.241 0.00524 0.0122 0.608 0.949 Value19=2.500 0.267 0.00547 0.0129 0.568 0.953 Value20=2.750 0.293 0.00572 0.0136 0.525 0.957 Value21=3.000 0.318 0.00600 0.0142 0.474 0.962 Value22=3.250 0.344 0.00631 0.0148 0.421 0.966 Value23=3.500 0.370 0.00665 0.0153 0.364 0.970 Value24=3.750 0.399 0.00705 0.0151 0.304 0.973 Value25=4.000 0.427 0.00751 0.0149 0.237 0.975 Value26=4.250 0.456 0.00800 0.0146 0.176 0.978 Value27=4.500 0.487 0.00852 0.0138 0.118 0.980 Value28=4.750 0.519 0.00904 0.0128 0.071 0.982 Value29=5.000 0.553 0.00960 0.0115 0.035 0.984 Value30=5.250 0.585 0.01017 0.0107 0.018 0.985 Value31=5.500 0.619 0.01066 0.0096 0.014 0.986 Value32=5.750 0.652 0.01113 0.0087 0.011 0.988 Value33=6.000 0.685 0.01170 0.0077 0.010 0.990 Value34=6.250 0.717 0.01235 0.0069 0.008 0.991 Value35=6.500 0.748 0.01323 0.0064 0.006 0.993 Value36=6.750 0.780 0.01420 0.0058 0.005 0.994 Value37=7.000 0.809 0.01547 0.0056 0.004 0.996 Value38=7.250 0.838 0.01689 0.0054 0.004 0.997 Value39=7.500 0.866 0.01858 0.0052 0.003 0.999 Value40=7.750 0.886 0.02157 0.0063 0.003 1.000 Value41=8.000 0.885 0.02431 0.0116 0.003 1.000 Value42=8.250 0.876 0.02745 0.0178 0.003 1.000 Value43=8.500 0.861 0.03074 0.0242 0.003 1.000 Value44=8.750 0.846 0.03443 0.0298 0.003 1.000 Value45=9.000 0.831 0.03872 0.0338 0.003 1.000 Value46=9.250 0.813 0.04256 0.0372 0.003 1.000 Value47=9.500 0.795 0.04674 0.0386 0.003 1.000 Value48=9.750 0.777 0.05152 0.0376 0.003 1.000 Value49=10.000 0.761 0.05735 0.0337 0.003 1.000 Value50=10.250 0.747 0.06498 0.0266 0.003 1.000 Value51=10.500 0.738 0.07587 0.0181 0.003 1.000 Value52=10.750 0.728 0.08419 0.0129 0.003 1.000 Value53=11.000 0.718 0.09140 0.0087 0.003 1.000 [Set1-Polar4] ReynoldsNumber=1500000 MachNumber=0.285 NumberPoints=57 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.210 0.00506 0.0020 0.901 0.469 Value02=-1.750 -0.187 0.00450 0.0031 0.894 0.594 Value03=-1.500 -0.162 0.00418 0.0038 0.889 0.667 Value04=-1.250 -0.137 0.00388 0.0048 0.882 0.737 Value05=-1.000 -0.111 0.00371 0.0054 0.875 0.779 Value06=-0.750 -0.083 0.00360 0.0059 0.865 0.810 Value07=-0.500 -0.056 0.00354 0.0063 0.853 0.833 Value08=-0.250 -0.028 0.00351 0.0066 0.838 0.851 Value09=0.000 0.000 0.00352 0.0069 0.820 0.864 Value10=0.250 0.028 0.00356 0.0072 0.798 0.875 Value11=0.500 0.056 0.00364 0.0076 0.770 0.885 Value12=0.750 0.083 0.00375 0.0080 0.739 0.893 Value13=1.000 0.110 0.00389 0.0083 0.705 0.902 Value14=1.250 0.137 0.00403 0.0087 0.673 0.909 Value15=1.500 0.165 0.00419 0.0090 0.637 0.915 Value16=1.750 0.192 0.00437 0.0094 0.599 0.921 Value17=2.000 0.219 0.00455 0.0097 0.563 0.926 Value18=2.250 0.246 0.00476 0.0101 0.521 0.932 Value19=2.500 0.272 0.00499 0.0105 0.478 0.936 Value20=2.750 0.299 0.00525 0.0110 0.429 0.941 Value21=3.000 0.325 0.00553 0.0115 0.381 0.945 Value22=3.250 0.350 0.00585 0.0121 0.329 0.950 Value23=3.500 0.376 0.00617 0.0127 0.280 0.954 Value24=3.750 0.401 0.00656 0.0134 0.222 0.958 Value25=4.000 0.426 0.00692 0.0141 0.176 0.962 Value26=4.250 0.450 0.00732 0.0150 0.127 0.966 Value27=4.500 0.475 0.00771 0.0158 0.088 0.970 Value28=4.750 0.500 0.00807 0.0166 0.059 0.974 Value29=5.000 0.526 0.00845 0.0171 0.033 0.977 Value30=5.250 0.553 0.00888 0.0174 0.016 0.980 Value31=5.500 0.582 0.00924 0.0174 0.012 0.983 Value32=5.750 0.612 0.00959 0.0172 0.010 0.985 Value33=6.000 0.644 0.00999 0.0165 0.008 0.986 Value34=6.250 0.676 0.01040 0.0159 0.007 0.988 Value35=6.500 0.710 0.01095 0.0149 0.006 0.989 Value36=6.750 0.742 0.01158 0.0142 0.004 0.991 Value37=7.000 0.774 0.01233 0.0134 0.003 0.991 Value38=7.250 0.805 0.01325 0.0129 0.003 0.993 Value39=7.500 0.836 0.01436 0.0125 0.002 0.994 Value40=7.750 0.865 0.01554 0.0122 0.002 0.995 Value41=8.000 0.890 0.01783 0.0126 0.002 0.997 Value42=8.250 0.909 0.02159 0.0135 0.002 0.999 Value43=8.500 0.907 0.02669 0.0174 0.002 1.000 Value44=8.750 0.887 0.03009 0.0248 0.002 1.000 Value45=9.000 0.866 0.03431 0.0309 0.002 1.000 Value46=9.250 0.847 0.03902 0.0349 0.002 1.000 Value47=9.500 0.827 0.04321 0.0378 0.002 1.000 Value48=9.750 0.807 0.04774 0.0385 0.002 1.000 Value49=10.000 0.789 0.05293 0.0366 0.002 1.000 Value50=10.250 0.773 0.05930 0.0317 0.002 1.000 Value51=10.500 0.760 0.06769 0.0239 0.002 1.000 Value52=10.750 0.751 0.07884 0.0158 0.002 1.000 Value53=11.000 0.740 0.08693 0.0109 0.002 1.000 Value54=11.250 0.729 0.09435 0.0068 0.002 1.000 Value55=11.500 0.718 0.10154 0.0031 0.002 1.000 Value56=11.750 0.708 0.10856 -0.0003 0.002 1.000 Value57=12.000 0.699 0.11540 -0.0034 0.002 1.000 [Set1-Polar5] ReynoldsNumber=2000000 MachNumber=0.285 NumberPoints=57 Values=Alpha Cl Cd Cm TU TL Value01=-2.000 -0.208 0.00524 0.0024 0.887 0.329 Value02=-1.750 -0.186 0.00451 0.0033 0.881 0.488 Value03=-1.500 -0.161 0.00409 0.0040 0.875 0.585 Value04=-1.250 -0.135 0.00380 0.0046 0.866 0.655 Value05=-1.000 -0.109 0.00354 0.0053 0.855 0.722 Value06=-0.750 -0.082 0.00340 0.0058 0.841 0.761 Value07=-0.500 -0.055 0.00332 0.0062 0.822 0.792 Value08=-0.250 -0.028 0.00329 0.0067 0.800 0.817 Value09=0.000 -0.001 0.00332 0.0071 0.775 0.838 Value10=0.250 0.027 0.00339 0.0074 0.747 0.853 Value11=0.500 0.054 0.00348 0.0076 0.716 0.865 Value12=0.750 0.082 0.00361 0.0079 0.680 0.875 Value13=1.000 0.110 0.00373 0.0081 0.648 0.885 Value14=1.250 0.137 0.00387 0.0083 0.613 0.893 Value15=1.500 0.165 0.00402 0.0085 0.576 0.900 Value16=1.750 0.193 0.00418 0.0087 0.540 0.907 Value17=2.000 0.220 0.00437 0.0089 0.500 0.913 Value18=2.250 0.248 0.00457 0.0091 0.458 0.919 Value19=2.500 0.275 0.00481 0.0093 0.413 0.924 Value20=2.750 0.302 0.00505 0.0096 0.367 0.929 Value21=3.000 0.329 0.00534 0.0099 0.318 0.933 Value22=3.250 0.356 0.00561 0.0102 0.274 0.938 Value23=3.500 0.382 0.00596 0.0106 0.220 0.943 Value24=3.750 0.408 0.00628 0.0111 0.177 0.946 Value25=4.000 0.434 0.00666 0.0115 0.128 0.950 Value26=4.250 0.460 0.00701 0.0120 0.092 0.954 Value27=4.500 0.486 0.00734 0.0126 0.063 0.958 Value28=4.750 0.512 0.00767 0.0133 0.040 0.961 Value29=5.000 0.538 0.00803 0.0140 0.021 0.965 Value30=5.250 0.563 0.00835 0.0147 0.012 0.969 Value31=5.500 0.589 0.00862 0.0155 0.009 0.972 Value32=5.750 0.615 0.00891 0.0164 0.008 0.976 Value33=6.000 0.641 0.00918 0.0171 0.007 0.979 Value34=6.250 0.667 0.00956 0.0178 0.006 0.982 Value35=6.500 0.696 0.00984 0.0180 0.005 0.985 Value36=6.750 0.725 0.01023 0.0180 0.004 0.988 Value37=7.000 0.756 0.01079 0.0176 0.003 0.989 Value38=7.250 0.787 0.01135 0.0172 0.002 0.991 Value39=7.500 0.819 0.01224 0.0166 0.002 0.992 Value40=7.750 0.849 0.01326 0.0163 0.002 0.993 Value41=8.000 0.879 0.01461 0.0160 0.002 0.994 Value42=8.250 0.906 0.01632 0.0161 0.001 0.996 Value43=8.500 0.929 0.01881 0.0166 0.001 0.997 Value44=8.750 0.941 0.02327 0.0178 0.001 0.999 Value45=9.000 0.929 0.02790 0.0231 0.001 1.000 Value46=9.250 0.907 0.03192 0.0297 0.001 1.000 Value47=9.500 0.884 0.03718 0.0342 0.001 1.000 Value48=9.750 0.861 0.04152 0.0374 0.001 1.000 Value49=10.000 0.841 0.04610 0.0384 0.001 1.000 Value50=10.250 0.822 0.05123 0.0369 0.001 1.000 Value51=10.500 0.805 0.05738 0.0325 0.001 1.000 Value52=10.750 0.792 0.06509 0.0254 0.001 1.000 Value53=11.000 0.781 0.07636 0.0169 0.001 1.000 Value54=11.250 0.765 0.08602 0.0110 0.001 1.000 Value55=11.500 0.746 0.09528 0.0059 0.001 1.000 Value56=11.750 0.726 0.10460 0.0013 0.001 1.000 Value57=12.000 0.708 0.11362 -0.0028 0.001 1.000