; This is a polar exchange file
; Comments start with a ';' in column 1
[Airfoil]
Airfoilname=MH 116  9.84%  
NumberSets=1

[Set1]
Origin=Eppler PROFIL (calculation)
Description1=Copyright 1997 Martin Hepperle
Description2=Created Mon Mar 10 20:23:53 1997
Description3=Smooth Surface

NumberPolars=3

[Set1-Polar1]
; the following line for compatibility with older versions
Re-Nr=300000
; future versions should use the following line
ReynoldsNumber=300000
MachNumber=0.5
Description1=
NumberPoints=13
;----  Alpha      Cl        Cd         Cm
Value01=-5.00   -0.11   0.0126   -0.1353
Value02=-4.00   0.03   0.0117   -0.1373
Value03=-3.00   0.18   0.0112   -0.1397
Value04=-2.00   0.32   0.0107   -0.1421
Value05=-1.00   0.46   0.0102   -0.1445
Value06=0.00   0.61   0.0095   -0.1469
Value07=1.00   0.75   0.0098   -0.1494
Value08=2.00   0.89   0.0105   -0.1514
Value09=3.00   1.02   0.0114   -0.1534
Value10=4.00   1.16   0.0131   -0.1551
Value11=5.00   1.28   0.0165   -0.1542
Value12=6.00   1.37   0.0211   -0.1476
Value13=7.00   1.45   0.0258   -0.1407

[Set1-Polar2]
; the following line for compatibility with older versions
Re-Nr=500000
; future versions should use the following line
ReynoldsNumber=500000
MachNumber=0.5
Description1=
NumberPoints=13
;----  Alpha      Cl        Cd         Cm
Value01=-5.00   -0.11   0.0111   -0.1348
Value02=-4.00   0.03   0.0103   -0.1374
Value03=-3.00   0.18   0.0098   -0.1401
Value04=-2.00   0.32   0.0093   -0.1427
Value05=-1.00   0.47   0.0088   -0.1453
Value06=0.00   0.61   0.0080   -0.1479
Value07=1.00   0.75   0.0082   -0.1504
Value08=2.00   0.89   0.0088   -0.1528
Value09=3.00   1.03   0.0096   -0.1551
Value10=4.00   1.17   0.0111   -0.1569
Value11=5.00   1.29   0.0143   -0.1567
Value12=6.00   1.40   0.0186   -0.1523
Value13=7.00   1.48   0.0230   -0.1451

[Set1-Polar3]
; the following line for compatibility with older versions
Re-Nr=700000
; future versions should use the following line
ReynoldsNumber=700000
MachNumber=0.5
Description1=
NumberPoints=13
;----  Alpha      Cl        Cd         Cm
Value01=-5.00   -0.11   0.0104   -0.1348
Value02=-4.00   0.03   0.0096   -0.1374
Value03=-3.00   0.18   0.0091   -0.1401
Value04=-2.00   0.32   0.0085   -0.1429
Value05=-1.00   0.47   0.0081   -0.1456
Value06=0.00   0.61   0.0074   -0.1483
Value07=1.00   0.75   0.0076   -0.1509
Value08=2.00   0.90   0.0081   -0.1534
Value09=3.00   1.04   0.0088   -0.1558
Value10=4.00   1.17   0.0104   -0.1577
Value11=5.00   1.30   0.0131   -0.1583
Value12=6.00   1.41   0.0172   -0.1550
Value13=7.00   1.49   0.0214   -0.1480