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