The 'PolarBrowser' application, a polar file converter is available
in the software section at:
http://www.MH-AeroTools.de/airfoils/
MH 116 9.84%
smooth surface
Copyright 2000-2004 Martin Hepperle
polar
300000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-5.000
-0.110
0.01260
-0.1353
-99.999
-99.999
-99.999
-99.999
-4.000
0.030
0.01170
-0.1373
-99.999
-99.999
-99.999
-99.999
-3.000
0.180
0.01120
-0.1397
-99.999
-99.999
-99.999
-99.999
-2.000
0.320
0.01070
-0.1421
-99.999
-99.999
-99.999
-99.999
-1.000
0.460
0.01020
-0.1445
-99.999
-99.999
-99.999
-99.999
0.000
0.610
0.00950
-0.1469
-99.999
-99.999
-99.999
-99.999
1.000
0.750
0.00980
-0.1494
-99.999
-99.999
-99.999
-99.999
2.000
0.890
0.01050
-0.1514
-99.999
-99.999
-99.999
-99.999
3.001
1.020
0.01140
-0.1534
-99.999
-99.999
-99.999
-99.999
4.001
1.160
0.01310
-0.1551
-99.999
-99.999
-99.999
-99.999
5.001
1.280
0.01650
-0.1542
-99.999
-99.999
-99.999
-99.999
6.001
1.370
0.02110
-0.1476
-99.999
-99.999
-99.999
-99.999
7.001
1.450
0.02580
-0.1407
-99.999
-99.999
-99.999
-99.999
polar
500000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-5.000
-0.110
0.01110
-0.1348
-99.999
-99.999
-99.999
-99.999
-4.000
0.030
0.01030
-0.1374
-99.999
-99.999
-99.999
-99.999
-3.000
0.180
0.00980
-0.1401
-99.999
-99.999
-99.999
-99.999
-2.000
0.320
0.00930
-0.1427
-99.999
-99.999
-99.999
-99.999
-1.000
0.470
0.00880
-0.1453
-99.999
-99.999
-99.999
-99.999
0.000
0.610
0.00800
-0.1479
-99.999
-99.999
-99.999
-99.999
1.000
0.750
0.00820
-0.1504
-99.999
-99.999
-99.999
-99.999
2.000
0.890
0.00880
-0.1528
-99.999
-99.999
-99.999
-99.999
3.001
1.030
0.00960
-0.1551
-99.999
-99.999
-99.999
-99.999
4.001
1.170
0.01110
-0.1569
-99.999
-99.999
-99.999
-99.999
5.001
1.290
0.01430
-0.1567
-99.999
-99.999
-99.999
-99.999
6.001
1.400
0.01860
-0.1523
-99.999
-99.999
-99.999
-99.999
7.001
1.480
0.02300
-0.1451
-99.999
-99.999
-99.999
-99.999
polar
700000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-5.000
-0.110
0.01040
-0.1348
-99.999
-99.999
-99.999
-99.999
-4.000
0.030
0.00960
-0.1374
-99.999
-99.999
-99.999
-99.999
-3.000
0.180
0.00910
-0.1401
-99.999
-99.999
-99.999
-99.999
-2.000
0.320
0.00850
-0.1429
-99.999
-99.999
-99.999
-99.999
-1.000
0.470
0.00810
-0.1456
-99.999
-99.999
-99.999
-99.999
0.000
0.610
0.00740
-0.1483
-99.999
-99.999
-99.999
-99.999
1.000
0.750
0.00760
-0.1509
-99.999
-99.999
-99.999
-99.999
2.000
0.900
0.00810
-0.1534
-99.999
-99.999
-99.999
-99.999
3.001
1.040
0.00880
-0.1558
-99.999
-99.999
-99.999
-99.999
4.001
1.170
0.01040
-0.1577
-99.999
-99.999
-99.999
-99.999
5.001
1.300
0.01310
-0.1583
-99.999
-99.999
-99.999
-99.999
6.001
1.410
0.01720
-0.1550
-99.999
-99.999
-99.999
-99.999
7.001
1.490
0.02140
-0.1480
-99.999
-99.999
-99.999
-99.999
rough surface (r=3)
Copyright 2000-2004 Martin Hepperle
polar
300000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-5.000
-0.110
0.01290
-0.1353
-99.999
-99.999
-99.999
-99.999
-4.000
0.030
0.01220
-0.1374
-99.999
-99.999
-99.999
-99.999
-3.000
0.180
0.01170
-0.1399
-99.999
-99.999
-99.999
-99.999
-2.000
0.320
0.01130
-0.1423
-99.999
-99.999
-99.999
-99.999
-1.000
0.470
0.01110
-0.1447
-99.999
-99.999
-99.999
-99.999
0.000
0.610
0.01120
-0.1471
-99.999
-99.999
-99.999
-99.999
1.000
0.750
0.01140
-0.1494
-99.999
-99.999
-99.999
-99.999
2.000
0.890
0.01210
-0.1514
-99.999
-99.999
-99.999
-99.999
3.001
1.020
0.01380
-0.1529
-99.999
-99.999
-99.999
-99.999
4.001
1.150
0.01600
-0.1533
-99.999
-99.999
-99.999
-99.999
5.001
1.270
0.01880
-0.1512
-99.999
-99.999
-99.999
-99.999
6.001
1.360
0.02230
-0.1457
-99.999
-99.999
-99.999
-99.999
7.001
1.440
0.02630
-0.1401
-99.999
-99.999
-99.999
-99.999
polar
500000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-5.000
-0.110
0.01180
-0.1348
-99.999
-99.999
-99.999
-99.999
-4.000
0.030
0.01100
-0.1374
-99.999
-99.999
-99.999
-99.999
-3.000
0.180
0.01060
-0.1401
-99.999
-99.999
-99.999
-99.999
-2.000
0.320
0.01020
-0.1427
-99.999
-99.999
-99.999
-99.999
-1.000
0.470
0.01020
-0.1452
-99.999
-99.999
-99.999
-99.999
0.000
0.610
0.01030
-0.1477
-99.999
-99.999
-99.999
-99.999
1.000
0.750
0.01070
-0.1500
-99.999
-99.999
-99.999
-99.999
2.000
0.890
0.01170
-0.1520
-99.999
-99.999
-99.999
-99.999
3.001
1.030
0.01310
-0.1536
-99.999
-99.999
-99.999
-99.999
4.001
1.160
0.01500
-0.1546
-99.999
-99.999
-99.999
-99.999
5.001
1.280
0.01750
-0.1538
-99.999
-99.999
-99.999
-99.999
6.001
1.380
0.02040
-0.1492
-99.999
-99.999
-99.999
-99.999
7.001
1.470
0.02390
-0.1437
-99.999
-99.999
-99.999
-99.999
polar
700000.0
0.00000
Alpha
Cl
Cd
Cm
TU
TL
SU
SL
-5.000
-0.110
0.01120
-0.1348
-99.999
-99.999
-99.999
-99.999
-4.000
0.030
0.01050
-0.1374
-99.999
-99.999
-99.999
-99.999
-3.000
0.180
0.01000
-0.1401
-99.999
-99.999
-99.999
-99.999
-2.000
0.320
0.00980
-0.1428
-99.999
-99.999
-99.999
-99.999
-1.000
0.470
0.00970
-0.1454
-99.999
-99.999
-99.999
-99.999
0.000
0.610
0.00990
-0.1479
-99.999
-99.999
-99.999
-99.999
1.000
0.750
0.01060
-0.1502
-99.999
-99.999
-99.999
-99.999
2.000
0.890
0.01160
-0.1524
-99.999
-99.999
-99.999
-99.999
3.001
1.030
0.01290
-0.1540
-99.999
-99.999
-99.999
-99.999
4.001
1.160
0.01460
-0.1553
-99.999
-99.999
-99.999
-99.999
5.001
1.280
0.01680
-0.1548
-99.999
-99.999
-99.999
-99.999
6.001
1.390
0.01950
-0.1514
-99.999
-99.999
-99.999
-99.999
7.001
1.480
0.02260
-0.1460
-99.999
-99.999
-99.999
-99.999