; This is a polar exchange file
; Comments start with a ';' in column 1
[Airfoil]
; obsolete:
Airfoilname=MH 32
; new:
Description1=MH 32
NumberSets=1

[Set1]
Origin=Eppler PROFIL (calculation)
Description1=Copyright 1996 Martin Hepperle
Description2=Created Mon May 13 15:03:20 1996

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=12
;----  Alpha      Cl        Cd         Cm
Value01=-0.50   -0.06   0.0138   -0.0550
Value02=0.00   -0.00   0.0127   -0.0554
Value03=0.50   0.05   0.0118   -0.0557
Value04=1.00   0.11   0.0115   -0.0563
Value05=2.00   0.21   0.0113   -0.0574
Value06=3.00   0.33   0.0115   -0.0593
Value07=4.00   0.44   0.0121   -0.0606
Value08=5.00   0.55   0.0128   -0.0613
Value09=6.00   0.65   0.0140   -0.0618
Value10=7.00   0.76   0.0157   -0.0616
Value11=8.00   0.85   0.0178   -0.0600
Value12=9.00   0.94   0.0204   -0.0566

[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=13
;----  Alpha      Cl        Cd         Cm
Value01=-1.00   -0.11   0.0116   -0.0551
Value02=-0.50   -0.06   0.0114   -0.0557
Value03=0.00   0.00   0.0099   -0.0563
Value04=0.50   0.06   0.0090   -0.0569
Value05=1.00   0.11   0.0086   -0.0575
Value06=2.00   0.22   0.0084   -0.0587
Value07=3.00   0.33   0.0086   -0.0599
Value08=4.00   0.44   0.0091   -0.0611
Value09=5.00   0.55   0.0098   -0.0623
Value10=6.00   0.66   0.0109   -0.0633
Value11=7.00   0.77   0.0125   -0.0637
Value12=8.00   0.87   0.0145   -0.0628
Value13=9.00   0.96   0.0175   -0.0594

[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=14
;----  Alpha      Cl        Cd         Cm
Value01=-2.00   -0.22   0.0103   -0.0540
Value02=-1.00   -0.11   0.0098   -0.0551
Value03=-0.50   -0.06   0.0096   -0.0557
Value04=0.00   0.00   0.0080   -0.0563
Value05=0.50   0.06   0.0071   -0.0569
Value06=1.00   0.11   0.0067   -0.0575
Value07=2.00   0.22   0.0064   -0.0587
Value08=3.00   0.33   0.0066   -0.0599
Value09=4.00   0.44   0.0071   -0.0611
Value10=5.00   0.55   0.0077   -0.0623
Value11=6.00   0.66   0.0086   -0.0635
Value12=7.00   0.77   0.0102   -0.0646
Value13=8.00   0.87   0.0120   -0.0647
Value14=9.00   0.97   0.0152   -0.0620

[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=14
;----  Alpha      Cl        Cd         Cm
Value01=-2.00   -0.22   0.0095   -0.0540
Value02=-1.00   -0.11   0.0090   -0.0551
Value03=-0.50   -0.06   0.0088   -0.0557
Value04=0.00   0.00   0.0072   -0.0563
Value05=0.50   0.06   0.0063   -0.0569
Value06=1.00   0.11   0.0060   -0.0575
Value07=2.00   0.22   0.0058   -0.0587
Value08=3.00   0.33   0.0060   -0.0599
Value09=4.00   0.44   0.0063   -0.0611
Value10=5.00   0.55   0.0068   -0.0623
Value11=6.00   0.66   0.0077   -0.0635
Value12=7.00   0.77   0.0090   -0.0647
Value13=8.00   0.88   0.0108   -0.0654
Value14=9.00   0.97   0.0140   -0.0632

[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=14
;----  Alpha      Cl        Cd         Cm
Value01=-2.00   -0.22   0.0086   -0.0540
Value02=-1.00   -0.11   0.0082   -0.0551
Value03=-0.50   -0.06   0.0080   -0.0557
Value04=0.00   0.00   0.0065   -0.0563
Value05=0.50   0.06   0.0060   -0.0569
Value06=1.00   0.11   0.0057   -0.0575
Value07=2.00   0.22   0.0056   -0.0587
Value08=3.00   0.33   0.0056   -0.0599
Value09=4.00   0.44   0.0058   -0.0611
Value10=5.00   0.55   0.0063   -0.0623
Value11=6.00   0.66   0.0069   -0.0635
Value12=7.00   0.77   0.0080   -0.0647
Value13=8.00   0.88   0.0096   -0.0658
Value14=9.00   0.98   0.0127   -0.0647