; This is a polar exchange file ; Comments start with a ';' in column 1 [Airfoil] Airfoilname=MH 46 11.35% NumberSets=1 [Set1] Origin=Eppler PROFIL (calculation) Description1=Copyright 1996 Martin Hepperle Description2=Created Sat Jun 17 21:50:48 1995 NumberPolars=5 [Set1-Polar1] ; the following line for compatibility with older versions Re-Nr=100000 ; future versions should use the following line ReynoldsNumber=100000 MachNumber=0.00 Description1= NumberPoints=18 ;---- Alpha Cl Cd Cm Value01=-2.00 -0.22 0.0137 0.0335 Value02=-1.50 -0.17 0.0131 0.0332 Value03=-1.00 -0.11 0.0124 0.0328 Value04=-0.50 -0.05 0.0112 0.0322 Value05=0.00 0.00 0.0114 0.0318 Value06=0.50 0.06 0.0115 0.0315 Value07=1.00 0.11 0.0117 0.0311 Value08=1.50 0.16 0.0119 0.0309 Value09=2.00 0.21 0.0121 0.0317 Value10=3.00 0.30 0.0127 0.0332 Value11=4.00 0.39 0.0134 0.0347 Value12=5.00 0.48 0.0145 0.0360 Value13=6.00 0.58 0.0163 0.0371 Value14=7.00 0.66 0.0184 0.0384 Value15=8.00 0.75 0.0208 0.0397 Value16=9.00 0.83 0.0235 0.0408 Value17=10.00 0.90 0.0263 0.0418 Value18=11.00 0.97 0.0297 0.0425 [Set1-Polar2] ; the following line for compatibility with older versions Re-Nr=200000 ; future versions should use the following line ReynoldsNumber=200000 MachNumber=0.00 Description1= NumberPoints=18 ;---- Alpha Cl Cd Cm Value01=-2.00 -0.22 0.0115 0.0335 Value02=-1.50 -0.17 0.0105 0.0332 Value03=-1.00 -0.11 0.0097 0.0328 Value04=-0.50 -0.05 0.0083 0.0321 Value05=0.00 0.00 0.0084 0.0318 Value06=0.50 0.06 0.0085 0.0314 Value07=1.00 0.11 0.0087 0.0310 Value08=1.50 0.16 0.0088 0.0308 Value09=2.00 0.21 0.0090 0.0315 Value10=3.00 0.31 0.0095 0.0328 Value11=4.00 0.40 0.0101 0.0339 Value12=5.00 0.50 0.0111 0.0351 Value13=6.00 0.59 0.0127 0.0364 Value14=7.00 0.68 0.0147 0.0380 Value15=8.00 0.76 0.0170 0.0394 Value16=9.00 0.84 0.0194 0.0407 Value17=10.00 0.92 0.0219 0.0418 Value18=11.00 0.99 0.0251 0.0427 [Set1-Polar3] ; the following line for compatibility with older versions Re-Nr=400000 ; future versions should use the following line ReynoldsNumber=400000 MachNumber=0.00 Description1= NumberPoints=18 ;---- Alpha Cl Cd Cm Value01=-2.00 -0.22 0.0095 0.0335 Value02=-1.50 -0.17 0.0089 0.0332 Value03=-1.00 -0.11 0.0081 0.0328 Value04=-0.50 -0.05 0.0065 0.0320 Value05=0.00 0.00 0.0066 0.0316 Value06=0.50 0.06 0.0067 0.0313 Value07=1.00 0.11 0.0068 0.0309 Value08=1.50 0.17 0.0069 0.0306 Value09=2.00 0.22 0.0070 0.0301 Value10=3.00 0.33 0.0074 0.0292 Value11=4.00 0.44 0.0080 0.0282 Value12=5.00 0.55 0.0089 0.0270 Value13=6.00 0.61 0.0102 0.0351 Value14=7.00 0.69 0.0120 0.0371 Value15=8.00 0.77 0.0141 0.0389 Value16=9.00 0.85 0.0163 0.0404 Value17=10.00 0.93 0.0185 0.0417 Value18=11.00 1.00 0.0215 0.0428 [Set1-Polar4] ; the following line for compatibility with older versions Re-Nr=600000 ; future versions should use the following line ReynoldsNumber=600000 MachNumber=0.00 Description1= NumberPoints=18 ;---- Alpha Cl Cd Cm Value01=-2.00 -0.22 0.0086 0.0335 Value02=-1.50 -0.17 0.0080 0.0332 Value03=-1.00 -0.11 0.0073 0.0328 Value04=-0.50 -0.06 0.0062 0.0325 Value05=0.00 0.00 0.0057 0.0317 Value06=0.50 0.06 0.0057 0.0313 Value07=1.00 0.11 0.0058 0.0310 Value08=1.50 0.17 0.0059 0.0306 Value09=2.00 0.22 0.0061 0.0302 Value10=3.00 0.33 0.0064 0.0292 Value11=4.00 0.44 0.0069 0.0282 Value12=5.00 0.55 0.0077 0.0270 Value13=6.00 0.63 0.0091 0.0324 Value14=7.00 0.70 0.0108 0.0365 Value15=8.00 0.78 0.0127 0.0385 Value16=9.00 0.86 0.0148 0.0401 Value17=10.00 0.94 0.0169 0.0415 Value18=11.00 1.01 0.0197 0.0427 [Set1-Polar5] ; the following line for compatibility with older versions Re-Nr=1000000 ; future versions should use the following line ReynoldsNumber=1000000 MachNumber=0.00 Description1= NumberPoints=18 ;---- Alpha Cl Cd Cm Value01=-2.00 -0.22 0.0077 0.0335 Value02=-1.50 -0.17 0.0073 0.0332 Value03=-1.00 -0.11 0.0069 0.0328 Value04=-0.50 -0.06 0.0065 0.0325 Value05=0.00 0.00 0.0060 0.0321 Value06=0.50 0.06 0.0051 0.0317 Value07=1.00 0.11 0.0050 0.0311 Value08=1.50 0.17 0.0051 0.0307 Value09=2.00 0.22 0.0052 0.0302 Value10=3.00 0.33 0.0055 0.0293 Value11=4.00 0.44 0.0061 0.0282 Value12=5.00 0.55 0.0068 0.0270 Value13=6.00 0.66 0.0080 0.0258 Value14=7.00 0.71 0.0094 0.0353 Value15=8.00 0.79 0.0113 0.0378 Value16=9.00 0.87 0.0132 0.0397 Value17=10.00 0.95 0.0151 0.0412 Value18=11.00 1.02 0.0177 0.0426