; This is a polar exchange file
; Comments start with a ';' in column 1
[Airfoil]
; obsolete:
Airfoilname=MH 18
; new:
Description1=MH 18
NumberSets=1

[Set1]
Origin=Eppler PROFIL (calculation)
Description1=Copyright 1996 Martin Hepperle
Description2=Created Mon May 13 11:15:52 1996

NumberPolars=3

[Set1-Polar1]
; the following line for compatibility with older versions
Re-Nr=500000
; future versions should use the following line
ReynoldsNumber=500000
MachNumber=0.00
Description1=
NumberPoints=11
;----  Alpha      Cl        Cd         Cm
Value01=-1.50   -0.17   0.0105   -0.0014
Value02=0.00   0.01   0.0061   -0.0065
Value03=1.00   0.12   0.0062   -0.0078
Value04=2.00   0.23   0.0063   -0.0093
Value05=3.00   0.34   0.0064   -0.0109
Value06=4.00   0.43   0.0066   -0.0098
Value07=5.00   0.53   0.0070   -0.0098
Value08=6.00   0.63   0.0080   -0.0098
Value09=7.00   0.72   0.0094   -0.0086
Value10=8.00   0.79   0.0148   -0.0035
Value11=9.00   0.88   0.0163   -0.0024

[Set1-Polar2]
; the following line for compatibility with older versions
Re-Nr=700000
; future versions should use the following line
ReynoldsNumber=700000
MachNumber=0.00
Description1=
NumberPoints=12
;----  Alpha      Cl        Cd         Cm
Value01=-2.00   -0.22   0.0101   -0.0007
Value02=-1.50   -0.17   0.0098   -0.0014
Value03=0.00   0.01   0.0054   -0.0062
Value04=1.00   0.12   0.0055   -0.0076
Value05=2.00   0.23   0.0056   -0.0091
Value06=3.00   0.34   0.0057   -0.0108
Value07=4.00   0.44   0.0059   -0.0126
Value08=5.00   0.55   0.0063   -0.0145
Value09=6.00   0.64   0.0073   -0.0115
Value10=7.00   0.73   0.0085   -0.0099
Value11=8.00   0.80   0.0138   -0.0043
Value12=9.00   0.88   0.0153   -0.0033

[Set1-Polar3]
; 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=12
;----  Alpha      Cl        Cd         Cm
Value01=-2.00   -0.22   0.0095   -0.0007
Value02=-1.50   -0.17   0.0092   -0.0014
Value03=0.00   0.00   0.0049   -0.0045
Value04=1.00   0.12   0.0049   -0.0072
Value05=2.00   0.23   0.0050   -0.0088
Value06=3.00   0.33   0.0051   -0.0105
Value07=4.00   0.44   0.0054   -0.0124
Value08=5.00   0.55   0.0059   -0.0143
Value09=6.00   0.65   0.0069   -0.0125
Value10=7.00   0.74   0.0080   -0.0108
Value11=8.00   0.80   0.0129   -0.0052
Value12=9.00   0.89   0.0143   -0.0042