[Airfoil] Description1=MH 43 NumberSets=1 [Set1] Origin=Calculation: X-Foil Description1=Copyright 1996 Martin Hepperle Description2=Created Mon May 13 09:54:37 1996 NumberPolars=5 [Set1-Polar1] Re-Nr=100000 ReynoldsNumber=100000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=31 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.320 0.01965 -0.0287 1.0000 0.0248 Value02= -3.50 -0.288 0.01770 -0.0258 1.0000 0.0364 Value03= -3.00 -0.219 0.01513 -0.0296 0.9921 0.1192 Value04= -1.50 0.042 0.01229 -0.0453 0.9357 1.0000 Value05= -1.00 0.114 0.01246 -0.0492 0.9019 1.0000 Value06= -0.50 0.174 0.01273 -0.0503 0.8696 1.0000 Value07= 0.00 0.224 0.01308 -0.0492 0.8386 1.0000 Value08= 0.50 0.272 0.01344 -0.0472 0.8095 1.0000 Value09= 1.00 0.319 0.01382 -0.0452 0.7825 1.0000 Value10= 1.50 0.367 0.01416 -0.0430 0.7564 1.0000 Value11= 2.00 0.415 0.01453 -0.0411 0.7303 1.0000 Value12= 2.50 0.464 0.01480 -0.0388 0.7043 1.0000 Value13= 3.00 0.513 0.01509 -0.0368 0.6773 1.0000 Value14= 3.50 0.563 0.01530 -0.0346 0.6490 1.0000 Value15= 4.00 0.612 0.01535 -0.0320 0.6162 1.0000 Value16= 4.50 0.662 0.01536 -0.0294 0.5784 1.0000 Value17= 5.00 0.712 0.01533 -0.0265 0.5289 1.0000 Value18= 5.50 0.758 0.01544 -0.0235 0.4480 1.0000 Value19= 6.00 0.798 0.01670 -0.0212 0.2928 1.0000 Value20= 6.50 0.839 0.01929 -0.0203 0.1283 1.0000 Value21= 7.00 0.875 0.02292 -0.0182 0.0532 1.0000 Value22= 7.50 0.912 0.02618 -0.0161 0.0337 1.0000 Value23= 8.00 0.952 0.02994 -0.0139 0.0247 1.0000 Value24= 8.50 0.992 0.03391 -0.0122 0.0197 1.0000 Value25= 9.00 1.027 0.03938 -0.0105 0.0160 1.0000 Value26= 9.50 1.053 0.04579 -0.0088 0.0140 1.0000 Value27= 10.00 1.065 0.05358 -0.0075 0.0129 1.0000 Value28= 10.50 1.058 0.06275 -0.0072 0.0122 1.0000 Value29= 11.00 1.026 0.07274 -0.0092 0.0121 1.0000 Value30= 11.50 0.978 0.08691 -0.0193 0.0123 1.0000 Value31= 12.00 0.913 0.11482 -0.0428 0.0133 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 -0.275 0.01495 -0.0358 0.9762 0.0140 Value02= -3.50 -0.202 0.01329 -0.0396 0.9517 0.0250 Value03= -3.00 -0.143 0.01161 -0.0401 0.9215 0.1290 Value04= -2.50 -0.094 0.01046 -0.0386 0.8918 0.3747 Value05= -2.00 -0.054 0.00933 -0.0351 0.8643 0.6662 Value06= -1.50 -0.020 0.00875 -0.0280 0.8402 0.8895 Value07= -1.00 0.068 0.00871 -0.0327 0.8223 0.9880 Value08= -0.50 0.142 0.00873 -0.0367 0.8001 1.0000 Value09= 0.00 0.189 0.00886 -0.0350 0.7770 1.0000 Value10= 0.50 0.237 0.00900 -0.0334 0.7541 1.0000 Value11= 1.00 0.287 0.00916 -0.0321 0.7322 1.0000 Value12= 1.50 0.338 0.00931 -0.0308 0.7094 1.0000 Value13= 2.00 0.390 0.00946 -0.0296 0.6858 1.0000 Value14= 2.50 0.443 0.00964 -0.0287 0.6611 1.0000 Value15= 3.00 0.495 0.00979 -0.0276 0.6328 1.0000 Value16= 3.50 0.548 0.00999 -0.0266 0.6015 1.0000 Value17= 4.00 0.600 0.01021 -0.0256 0.5635 1.0000 Value18= 4.50 0.652 0.01054 -0.0246 0.5137 1.0000 Value19= 5.00 0.700 0.01127 -0.0232 0.4001 1.0000 Value20= 5.50 0.748 0.01258 -0.0227 0.2662 1.0000 Value21= 6.00 0.796 0.01422 -0.0223 0.1363 1.0000 Value22= 6.50 0.840 0.01657 -0.0212 0.0386 1.0000 Value23= 7.00 0.885 0.01868 -0.0200 0.0224 1.0000 Value24= 7.50 0.925 0.02128 -0.0184 0.0164 1.0000 Value25= 8.00 0.965 0.02382 -0.0168 0.0137 1.0000 Value26= 8.50 1.004 0.02736 -0.0148 0.0120 1.0000 Value27= 9.00 1.039 0.03293 -0.0124 0.0108 1.0000 Value28= 9.50 1.069 0.03824 -0.0106 0.0094 1.0000 Value29= 10.00 1.090 0.04481 -0.0088 0.0083 1.0000 Value30= 10.50 1.095 0.05268 -0.0075 0.0077 1.0000 Value31= 11.00 1.078 0.06119 -0.0066 0.0074 1.0000 Value32= 11.50 1.043 0.07169 -0.0106 0.0073 1.0000 Value33= 12.00 0.995 0.08714 -0.0224 0.0075 1.0000 [Set1-Polar3] Re-Nr=400000 ReynoldsNumber=400000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=31 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.274 0.01279 -0.0322 0.8950 0.0075 Value02= -3.50 -0.225 0.01130 -0.0302 0.8677 0.0113 Value03= -3.00 -0.174 0.01042 -0.0290 0.8441 0.0177 Value04= -2.50 -0.122 0.00930 -0.0282 0.8230 0.1480 Value05= -2.00 -0.070 0.00845 -0.0277 0.8023 0.3320 Value06= -1.50 -0.021 0.00741 -0.0266 0.7815 0.5926 Value07= -0.50 0.070 0.00633 -0.0201 0.7422 0.9461 Value08= 0.50 0.223 0.00645 -0.0286 0.7012 1.0000 Value09= 1.00 0.274 0.00655 -0.0276 0.6792 1.0000 Value10= 1.50 0.327 0.00668 -0.0269 0.6573 1.0000 Value11= 2.00 0.380 0.00683 -0.0262 0.6337 1.0000 Value12= 2.50 0.434 0.00701 -0.0257 0.6047 1.0000 Value13= 3.00 0.488 0.00722 -0.0252 0.5740 1.0000 Value14= 3.50 0.541 0.00748 -0.0248 0.5371 1.0000 Value15= 4.00 0.595 0.00788 -0.0243 0.4833 1.0000 Value16= 4.50 0.646 0.00873 -0.0239 0.3721 1.0000 Value17= 5.00 0.697 0.00981 -0.0237 0.2602 1.0000 Value18= 5.50 0.746 0.01117 -0.0235 0.1376 1.0000 Value19= 6.00 0.794 0.01290 -0.0230 0.0278 1.0000 Value20= 6.50 0.844 0.01428 -0.0224 0.0150 1.0000 Value21= 7.00 0.891 0.01588 -0.0215 0.0121 1.0000 Value22= 7.50 0.933 0.01836 -0.0199 0.0106 1.0000 Value23= 8.00 0.977 0.02028 -0.0187 0.0095 1.0000 Value24= 8.50 1.018 0.02271 -0.0172 0.0085 1.0000 Value25= 9.00 1.056 0.02587 -0.0154 0.0076 1.0000 Value26= 9.50 1.087 0.03107 -0.0129 0.0066 1.0000 Value27= 10.00 1.107 0.03957 -0.0101 0.0061 1.0000 Value28= 10.50 1.113 0.04861 -0.0082 0.0060 1.0000 Value29= 11.00 1.099 0.05749 -0.0065 0.0059 1.0000 Value30= 11.50 1.068 0.06710 -0.0086 0.0059 1.0000 Value31= 12.00 1.027 0.07966 -0.0169 0.0059 1.0000 [Set1-Polar4] Re-Nr=600000 ReynoldsNumber=600000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=33 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.288 0.01241 -0.0285 0.8506 0.0053 Value02= -3.50 -0.236 0.01035 -0.0269 0.8295 0.0083 Value03= -3.00 -0.182 0.00960 -0.0262 0.8088 0.0116 Value04= -2.50 -0.128 0.00900 -0.0256 0.7889 0.0232 Value05= -2.00 -0.075 0.00790 -0.0254 0.7697 0.2319 Value06= -1.50 -0.022 0.00717 -0.0252 0.7498 0.4060 Value07= -1.00 0.030 0.00629 -0.0245 0.7311 0.6462 Value08= -0.50 0.078 0.00564 -0.0224 0.7113 0.8393 Value09= 0.00 0.125 0.00542 -0.0195 0.6924 0.9439 Value10= 0.50 0.208 0.00547 -0.0251 0.6707 0.9971 Value11= 1.00 0.272 0.00558 -0.0269 0.6468 1.0000 Value12= 1.50 0.324 0.00571 -0.0262 0.6242 1.0000 Value13= 2.00 0.377 0.00586 -0.0256 0.5974 1.0000 Value14= 2.50 0.431 0.00606 -0.0251 0.5678 1.0000 Value15= 3.00 0.485 0.00630 -0.0248 0.5333 1.0000 Value16= 3.50 0.539 0.00663 -0.0245 0.4855 1.0000 Value17= 4.00 0.592 0.00729 -0.0243 0.3940 1.0000 Value18= 4.50 0.644 0.00823 -0.0242 0.2848 1.0000 Value19= 5.00 0.695 0.00935 -0.0241 0.1754 1.0000 Value20= 5.50 0.745 0.01080 -0.0239 0.0559 1.0000 Value21= 6.00 0.795 0.01208 -0.0234 0.0140 1.0000 Value22= 6.50 0.845 0.01359 -0.0226 0.0107 1.0000 Value23= 7.00 0.895 0.01465 -0.0221 0.0095 1.0000 Value24= 7.50 0.943 0.01606 -0.0214 0.0087 1.0000 Value25= 8.00 0.988 0.01777 -0.0203 0.0079 1.0000 Value26= 8.50 1.029 0.02002 -0.0188 0.0073 1.0000 Value27= 9.00 1.064 0.02404 -0.0162 0.0064 1.0000 Value28= 9.50 1.089 0.03220 -0.0126 0.0059 1.0000 Value29= 10.00 1.114 0.03823 -0.0107 0.0053 1.0000 Value30= 10.50 1.129 0.04466 -0.0090 0.0048 1.0000 Value31= 11.00 1.127 0.05187 -0.0071 0.0045 1.0000 Value32= 11.50 1.103 0.06005 -0.0071 0.0044 1.0000 Value33= 12.00 1.067 0.07106 -0.0125 0.0043 1.0000 [Set1-Polar5] Re-Nr=1000000 ReynoldsNumber=1000000 Description1=Copyright © 1995-1996 Martin Hepperle NumberPoints=27 ; Alpha Cl Cd Cm T.U. T.L. Value01= -4.00 -0.297 0.01085 -0.0259 0.8061 0.0038 Value02= -3.50 -0.243 0.00976 -0.0252 0.7873 0.0048 Value03= -0.50 0.083 0.00526 -0.0234 0.6735 0.6924 Value04= 0.00 0.135 0.00492 -0.0225 0.6526 0.8165 Value05= 0.50 0.185 0.00468 -0.0208 0.6326 0.9171 Value06= 1.50 0.323 0.00481 -0.0261 0.5829 1.0000 Value07= 2.00 0.376 0.00499 -0.0254 0.5505 1.0000 Value08= 2.50 0.430 0.00520 -0.0251 0.5184 1.0000 Value09= 3.00 0.484 0.00558 -0.0248 0.4591 1.0000 Value10= 3.50 0.538 0.00602 -0.0246 0.3972 1.0000 Value11= 4.00 0.591 0.00683 -0.0245 0.2941 1.0000 Value12= 4.50 0.643 0.00774 -0.0245 0.1932 1.0000 Value13= 5.00 0.694 0.00886 -0.0244 0.0899 1.0000 Value14= 5.50 0.745 0.01036 -0.0240 0.0106 1.0000 Value15= 6.00 0.798 0.01101 -0.0238 0.0093 1.0000 Value16= 6.50 0.851 0.01180 -0.0235 0.0082 1.0000 Value17= 7.00 0.902 0.01278 -0.0231 0.0075 1.0000 Value18= 7.50 0.951 0.01404 -0.0224 0.0071 1.0000 Value19= 8.00 0.997 0.01574 -0.0214 0.0067 1.0000 Value20= 8.50 1.037 0.01852 -0.0195 0.0062 1.0000 Value21= 9.00 1.068 0.02398 -0.0162 0.0052 1.0000 Value22= 9.50 1.105 0.02703 -0.0147 0.0046 1.0000 Value23= 10.00 1.138 0.03096 -0.0131 0.0041 1.0000 Value24= 10.50 1.162 0.03591 -0.0112 0.0037 1.0000 Value25= 11.00 1.174 0.04185 -0.0093 0.0035 1.0000 Value26= 11.50 1.164 0.04840 -0.0067 0.0034 1.0000 Value27= 12.00 1.139 0.05682 -0.0078 0.0033 1.0000