Airfoil: W1015-20 fp30 Builder: S. Cassidy Comment: Clean, Cf/C = 20%, Flap = 30° Number of Reynolds #'s: 3 Average Reynolds #: 99588.7 Number of angles of attack: 53 alpha / Cl / Cm -10.32 -0.31 -0.1355 -9.30 -0.18 -0.1414 -8.26 -0.07 -0.1514 -7.16 0.04 -0.1512 -6.31 0.11 -0.1514 -5.07 0.21 -0.1390 -4.10 0.27 -0.1298 -3.19 0.35 -0.1271 -2.06 0.46 -0.1288 -1.02 0.57 -0.1333 -0.14 0.67 -0.1384 1.02 0.78 -0.1342 1.97 0.86 -0.1326 3.07 0.96 -0.1311 4.10 1.05 -0.1288 4.98 1.12 -0.1257 6.05 1.21 -0.1259 7.16 1.30 -0.1248 8.20 1.38 -0.1236 9.25 1.46 -0.1224 10.24 1.52 -0.1201 11.22 1.56 -0.1189 11.90 1.14 -0.2480 12.92 1.13 -0.2492 13.95 1.11 -0.2523 15.01 1.16 -0.2663 15.93 1.14 -0.2689 15.58 1.14 -0.2531 14.59 1.13 -0.2442 13.63 1.15 -0.2391 12.63 1.13 -0.2326 11.66 1.07 -0.2242 10.59 1.04 -0.2126 9.73 1.05 -0.2037 8.66 1.05 -0.1919 7.88 1.37 -0.1172 6.81 1.29 -0.1176 5.77 1.21 -0.1190 4.68 1.11 -0.1203 3.59 1.03 -0.1215 2.67 0.94 -0.1237 1.80 0.87 -0.1254 0.67 0.78 -0.1303 -0.29 0.65 -0.1262 -1.44 0.55 -0.1227 -2.45 0.45 -0.1194 -3.39 0.36 -0.1204 -4.56 0.27 -0.1244 -5.54 0.21 -0.1358 -6.36 0.15 -0.1425 -7.53 0.05 -0.1464 -8.57 -0.07 -0.1417 -9.58 -0.19 -0.1359 Tabulated from data in file 07002gw.dat & reduced using program C10.20 Average Reynolds #: 199372.7 Number of angles of attack: 53 alpha / Cl / Cm -10.36 -0.21 -0.1646 -9.34 -0.10 -0.1689 -8.21 0.02 -0.1739 -7.26 0.12 -0.1754 -6.17 0.24 -0.1780 -5.14 0.35 -0.1803 -4.06 0.46 -0.1797 -3.11 0.55 -0.1795 -2.11 0.63 -0.1774 -1.12 0.68 -0.1673 -0.10 0.76 -0.1598 0.88 0.83 -0.1534 2.00 0.93 -0.1498 3.04 1.01 -0.1445 3.98 1.10 -0.1415 5.02 1.19 -0.1399 6.13 1.28 -0.1376 7.15 1.36 -0.1358 8.15 1.45 -0.1341 9.12 1.52 -0.1310 10.23 1.60 -0.1283 11.29 1.65 -0.1271 12.14 1.69 -0.1274 13.22 1.58 -0.1414 14.06 1.53 -0.1507 14.89 1.21 -0.2666 15.84 1.21 -0.2744 15.63 1.17 -0.2618 14.77 1.20 -0.2601 13.64 1.19 -0.2547 12.72 1.19 -0.2484 11.62 1.13 -0.2380 10.79 1.13 -0.2323 9.99 1.58 -0.1247 8.82 1.50 -0.1262 7.76 1.41 -0.1281 6.75 1.34 -0.1316 5.87 1.27 -0.1344 4.68 1.16 -0.1356 3.64 1.08 -0.1386 2.72 1.00 -0.1414 1.68 0.90 -0.1452 0.63 0.82 -0.1504 -0.43 0.74 -0.1573 -1.28 0.68 -0.1635 -2.42 0.61 -0.1732 -3.48 0.51 -0.1732 -4.40 0.42 -0.1738 -5.43 0.32 -0.1733 -6.55 0.20 -0.1710 -7.57 0.09 -0.1694 -8.44 -0.00 -0.1658 -9.52 -0.12 -0.1623 Tabulated from data in file 07004gw.dat & reduced using program C10.20 Average Reynolds #: 398440.4 Number of angles of attack: 51 alpha / Cl / Cm -10.45 -0.19 -0.1718 -9.24 -0.06 -0.1752 -8.39 0.02 -0.1787 -7.27 0.14 -0.1806 -6.32 0.24 -0.1818 -5.29 0.35 -0.1836 -4.17 0.45 -0.1820 -3.16 0.54 -0.1784 -2.18 0.63 -0.1747 -1.13 0.72 -0.1715 -0.20 0.81 -0.1704 0.94 0.91 -0.1671 1.99 1.00 -0.1632 2.92 1.08 -0.1601 3.91 1.17 -0.1566 5.01 1.26 -0.1530 6.14 1.36 -0.1480 7.04 1.43 -0.1439 8.05 1.51 -0.1388 9.12 1.60 -0.1357 10.28 1.70 -0.1329 11.30 1.77 -0.1301 12.17 1.78 -0.1302 13.12 1.60 -0.1531 14.06 1.52 -0.1633 15.04 1.52 -0.1727 14.87 1.50 -0.1690 13.94 1.54 -0.1629 12.85 1.60 -0.1472 11.89 1.80 -0.1288 10.88 1.74 -0.1297 9.94 1.67 -0.1320 8.86 1.58 -0.1350 7.85 1.51 -0.1398 6.82 1.42 -0.1437 5.90 1.34 -0.1468 4.88 1.25 -0.1512 3.82 1.17 -0.1559 2.69 1.07 -0.1601 1.65 0.98 -0.1643 0.78 0.90 -0.1661 -0.23 0.80 -0.1674 -1.25 0.71 -0.1702 -2.40 0.60 -0.1720 -3.43 0.52 -0.1791 -4.49 0.42 -0.1798 -5.47 0.32 -0.1799 -6.46 0.22 -0.1800 -7.57 0.11 -0.1766 -8.62 -0.00 -0.1746 -9.60 -0.11 -0.1718 Tabulated from data in file 07006gw.dat & reduced using program C10.20 File w1015-20_fp30_lift.dat created using program clcm dist V1.1 on 30-Mar-2012 09:46:58