| 0006 | 0008 | 0010 | 0012 | 0015 | 0018 | 0021 |
| 0008-34 | 0010-34 | 0010-35 | 0010-64 |
| 0010-66 | 0010-66 | 0012-34 | 0012-64 |
| 16-006 | 16-009 | 16-012 | 16-015 | 16-018 | 16-021 |
| 63-006 | 63-008 | 63-009 | 63-010 |
| 63-012 | 63-015 | 63-018 | 63-021 |
| 63A006 | 63A008 | 63A010 | 63A012 | 63A015 |
| 64-006 | 64-008 | 64-009 | 64-010 |
| 64-012 | 64-015 | 64-018 | 64-021 |
| 64A006 | 64A008 | 64A010 | 64A012 | 64A015 |
| 65-006 | 65-008 | 65-009 | 65-010 |
| 65-012 | 65-015 | 65-018 | 65-021 |
| 65A006 | 65A008 | 65A010 | 65A012 | 65A015 |
| 66-006 | 66-008 | 66-009 | 66-010 |
| 66-012 | 66-015 | 66-018 | 66-021 |
| 67-012 | 67-015 |
| NACA 0006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.6107 | 0.5910 |
| 0.7500 | 0.7424 | 0.4749 |
| 1.2500 | 0.9470 | 0.3579 |
| 2.5000 | 1.3074 | 0.2387 |
| 5.0000 | 1.7773 | 0.1514 |
| 7.5000 | 2.1000 | 0.1104 |
| 10.0000 | 2.3414 | 0.0844 |
| 15.0000 | 2.6726 | 0.0509 |
| 20.0000 | 2.8688 | 0.0289 |
| 25.0000 | 2.9706 | 0.0126 |
| 30.0000 | 3.0009 | 0.0000 |
| 35.0000 | 2.9743 | -0.0102 |
| 40.0000 | 2.9015 | -0.0186 |
| 45.0000 | 2.7904 | -0.0256 |
| 50.0000 | 2.6470 | -0.0316 |
| 55.0000 | 2.4762 | -0.0366 |
| 60.0000 | 2.2817 | -0.0411 |
| 65.0000 | 2.0662 | -0.0450 |
| 70.0000 | 1.8320 | -0.0486 |
| 75.0000 | 1.5802 | -0.0521 |
| 80.0000 | 1.3116 | -0.0554 |
| 85.0000 | 1.0263 | -0.0587 |
| 90.0000 | 0.7239 | -0.0623 |
| 95.0000 | 0.4033 | -0.0660 |
| 100.0000 | 0.0630 | -0.0702 |
| L.E. radius = 0.397 percent chord | ||
| NACA 0008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.8142 | 0.7880 |
| 0.7500 | 0.9899 | 0.6332 |
| 1.2500 | 1.2626 | 0.4772 |
| 2.5000 | 1.7431 | 0.3183 |
| 5.0000 | 2.3698 | 0.2019 |
| 7.5000 | 2.7999 | 0.1472 |
| 10.0000 | 3.1218 | 0.1125 |
| 15.0000 | 3.5634 | 0.0679 |
| 20.0000 | 3.8250 | 0.0385 |
| 25.0000 | 3.9608 | 0.0168 |
| 30.0000 | 4.0012 | -0.0001 |
| 35.0000 | 3.9657 | -0.0136 |
| 40.0000 | 3.8687 | -0.0248 |
| 45.0000 | 3.7205 | -0.0342 |
| 50.0000 | 3.5294 | -0.0421 |
| 55.0000 | 3.3016 | -0.0489 |
| 60.0000 | 3.0422 | -0.0548 |
| 65.0000 | 2.7550 | -0.0600 |
| 70.0000 | 2.4426 | -0.0649 |
| 75.0000 | 2.1069 | -0.0694 |
| 80.0000 | 1.7487 | -0.0738 |
| 85.0000 | 1.3684 | -0.0783 |
| 90.0000 | 0.9651 | -0.0830 |
| 95.0000 | 0.5377 | -0.0880 |
| 100.0000 | 0.0840 | -0.0935 |
| L.E. radius = 0.705 percent chord | ||
| NACA 0010 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.0178 | 0.9850 |
| 0.7500 | 1.2374 | 0.7915 |
| 1.2500 | 1.5783 | 0.5966 |
| 2.5000 | 2.1789 | 0.3979 |
| 5.0000 | 2.9622 | 0.2524 |
| 7.5000 | 3.4999 | 0.1840 |
| 10.0000 | 3.9023 | 0.1406 |
| 15.0000 | 4.4543 | 0.0848 |
| 20.0000 | 4.7813 | 0.0481 |
| 25.0000 | 4.9510 | 0.0210 |
| 30.0000 | 5.0014 | -0.0001 |
| 35.0000 | 4.9572 | -0.0171 |
| 40.0000 | 4.8358 | -0.0310 |
| 45.0000 | 4.6506 | -0.0427 |
| 50.0000 | 4.4117 | -0.0526 |
| 55.0000 | 4.1270 | -0.0611 |
| 60.0000 | 3.8028 | -0.0685 |
| 65.0000 | 3.4437 | -0.0750 |
| 70.0000 | 3.0533 | -0.0811 |
| 75.0000 | 2.6336 | -0.0868 |
| 80.0000 | 2.1859 | -0.0923 |
| 85.0000 | 1.7105 | -0.0979 |
| 90.0000 | 1.2064 | -0.1038 |
| 95.0000 | 0.6721 | -0.1100 |
| 100.0000 | 0.1050 | -0.1169 |
| L.E. radius = 1.102 percent chord | ||
| NACA 0012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.2213 | 1.1819 |
| 0.7500 | 1.4849 | 0.9498 |
| 1.2500 | 1.8939 | 0.7159 |
| 2.5000 | 2.6147 | 0.4775 |
| 5.0000 | 3.5547 | 0.3029 |
| 7.5000 | 4.1999 | 0.2208 |
| 10.0000 | 4.6828 | 0.1687 |
| 15.0000 | 5.3452 | 0.1018 |
| 20.0000 | 5.7375 | 0.0577 |
| 25.0000 | 5.9412 | 0.0252 |
| 30.0000 | 6.0017 | -0.0001 |
| 35.0000 | 5.9486 | -0.0205 |
| 40.0000 | 5.8030 | -0.0372 |
| 45.0000 | 5.5807 | -0.0513 |
| 50.0000 | 5.2940 | -0.0631 |
| 55.0000 | 4.9524 | -0.0733 |
| 60.0000 | 4.5634 | -0.0822 |
| 65.0000 | 4.1325 | -0.0901 |
| 70.0000 | 3.6639 | -0.0973 |
| 75.0000 | 3.1603 | -0.1041 |
| 80.0000 | 2.6231 | -0.1108 |
| 85.0000 | 2.0526 | -0.1175 |
| 90.0000 | 1.4477 | -0.1245 |
| 95.0000 | 0.8066 | -0.1321 |
| 100.0000 | 0.1260 | -0.1403 |
| L.E. radius = 1.587 percent chord | ||
| NACA 0015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.5266 | 1.4774 |
| 0.7500 | 1.8561 | 1.1872 |
| 1.2500 | 2.3674 | 0.8948 |
| 2.5000 | 3.2684 | 0.5969 |
| 5.0000 | 4.4434 | 0.3786 |
| 7.5000 | 5.2499 | 0.2760 |
| 10.0000 | 5.8535 | 0.2109 |
| 15.0000 | 6.6815 | 0.1272 |
| 20.0000 | 7.1719 | 0.0721 |
| 25.0000 | 7.4266 | 0.0315 |
| 30.0000 | 7.5022 | -0.0001 |
| 35.0000 | 7.4358 | -0.0256 |
| 40.0000 | 7.2538 | -0.0466 |
| 45.0000 | 6.9759 | -0.0641 |
| 50.0000 | 6.6175 | -0.0789 |
| 55.0000 | 6.1905 | -0.0916 |
| 60.0000 | 5.7042 | -0.1027 |
| 65.0000 | 5.1656 | -0.1126 |
| 70.0000 | 4.5799 | -0.1216 |
| 75.0000 | 3.9504 | -0.1301 |
| 80.0000 | 3.2789 | -0.1385 |
| 85.0000 | 2.5657 | -0.1469 |
| 90.0000 | 1.8096 | -0.1556 |
| 95.0000 | 1.0082 | -0.1651 |
| 100.0000 | 0.1575 | -0.1754 |
| L.E. radius = 2.479 percent chord | ||
| NACA 0018 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.8320 | 1.7729 |
| 0.7500 | 2.2273 | 1.4246 |
| 1.2500 | 2.8409 | 1.0738 |
| 2.5000 | 3.9221 | 0.7162 |
| 5.0000 | 5.3320 | 0.4543 |
| 7.5000 | 6.2999 | 0.3312 |
| 10.0000 | 7.0242 | 0.2531 |
| 15.0000 | 8.0177 | 0.1527 |
| 20.0000 | 8.6063 | 0.0866 |
| 25.0000 | 8.9119 | 0.0379 |
| 30.0000 | 9.0026 | -0.0001 |
| 35.0000 | 8.9229 | -0.0307 |
| 40.0000 | 8.7045 | -0.0559 |
| 45.0000 | 8.3711 | -0.0769 |
| 50.0000 | 7.9410 | -0.0947 |
| 55.0000 | 7.4286 | -0.1099 |
| 60.0000 | 6.8451 | -0.1232 |
| 65.0000 | 6.1987 | -0.1351 |
| 70.0000 | 5.4959 | -0.1459 |
| 75.0000 | 4.7405 | -0.1562 |
| 80.0000 | 3.9347 | -0.1661 |
| 85.0000 | 3.0788 | -0.1762 |
| 90.0000 | 2.1716 | -0.1868 |
| 95.0000 | 1.2098 | -0.1981 |
| 100.0000 | 0.1890 | -0.2105 |
| L.E. radius = 3.570 percent chord | ||
| NACA 0021 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 2.1373 | 2.0684 |
| 0.7500 | 2.5985 | 1.6621 |
| 1.2500 | 3.3143 | 1.2528 |
| 2.5000 | 4.5758 | 0.8356 |
| 5.0000 | 6.2207 | 0.5301 |
| 7.5000 | 7.3498 | 0.3863 |
| 10.0000 | 8.1948 | 0.2953 |
| 15.0000 | 9.3540 | 0.1781 |
| 20.0000 | 10.0407 | 0.1010 |
| 25.0000 | 10.3972 | 0.0442 |
| 30.0000 | 10.5030 | -0.0001 |
| 35.0000 | 10.4101 | -0.0358 |
| 40.0000 | 10.1553 | -0.0652 |
| 45.0000 | 9.7663 | -0.0897 |
| 50.0000 | 9.2645 | -0.1104 |
| 55.0000 | 8.6667 | -0.1282 |
| 60.0000 | 7.9859 | -0.1438 |
| 65.0000 | 7.2319 | -0.1576 |
| 70.0000 | 6.4118 | -0.1703 |
| 75.0000 | 5.5305 | -0.1822 |
| 80.0000 | 4.5905 | -0.1938 |
| 85.0000 | 3.5920 | -0.2056 |
| 90.0000 | 2.5335 | -0.2179 |
| 95.0000 | 1.4115 | -0.2311 |
| 100.0000 | 0.2205 | -0.2455 |
| L.E. radius = 4.859 percent chord | ||
| NACA 0008-34 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.4578 | 0.4946 |
| 0.7500 | 0.5707 | 0.4164 |
| 1.2500 | 0.7566 | 0.3370 |
| 2.5000 | 1.1174 | 0.2538 |
| 5.0000 | 1.6583 | 0.1884 |
| 7.5000 | 2.0830 | 0.1540 |
| 10.0000 | 2.4364 | 0.1298 |
| 15.0000 | 2.9926 | 0.0947 |
| 20.0000 | 3.3969 | 0.0681 |
| 25.0000 | 3.6815 | 0.0464 |
| 30.0000 | 3.8669 | 0.0283 |
| 35.0000 | 3.9687 | 0.0129 |
| 40.0000 | 4.0000 | 0.0000 |
| 45.0000 | 3.9708 | 0.0117 |
| 50.0000 | 3.8838 | 0.0231 |
| 55.0000 | 3.7401 | 0.0343 |
| 60.0000 | 3.5409 | 0.0453 |
| 65.0000 | 3.2873 | 0.0561 |
| 70.0000 | 2.9803 | 0.0667 |
| 75.0000 | 2.6211 | 0.0770 |
| 80.0000 | 2.2107 | 0.0871 |
| 85.0000 | 1.7503 | 0.0970 |
| 90.0000 | 1.2410 | 0.1067 |
| 95.0000 | 0.6839 | 0.1161 |
| 100.0000 | 0.0800 | 0.1254 |
| L.E. radius = 0.176 percent chord | ||
| NACA 0010-34 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.5722 | 0.6182 |
| 0.7500 | 0.7133 | 0.5205 |
| 1.2500 | 0.9457 | 0.4212 |
| 2.5000 | 1.3968 | 0.3173 |
| 5.0000 | 2.0728 | 0.2355 |
| 7.5000 | 2.6038 | 0.1925 |
| 10.0000 | 3.0455 | 0.1623 |
| 15.0000 | 3.7408 | 0.1183 |
| 20.0000 | 4.2461 | 0.0851 |
| 25.0000 | 4.6018 | 0.0580 |
| 30.0000 | 4.8336 | 0.0353 |
| 35.0000 | 4.9609 | 0.0161 |
| 40.0000 | 5.0000 | 0.0000 |
| 45.0000 | 4.9634 | 0.0146 |
| 50.0000 | 4.8547 | 0.0289 |
| 55.0000 | 4.6751 | 0.0429 |
| 60.0000 | 4.4261 | 0.0567 |
| 65.0000 | 4.1091 | 0.0701 |
| 70.0000 | 3.7254 | 0.0833 |
| 75.0000 | 3.2764 | 0.0962 |
| 80.0000 | 2.7634 | 0.1089 |
| 85.0000 | 2.1879 | 0.1213 |
| 90.0000 | 1.5513 | 0.1334 |
| 95.0000 | 0.8548 | 0.1452 |
| 100.0000 | 0.1000 | 0.1567 |
| L.E. radius = 0.275 percent chord | ||
| NACA 0010-35 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.5457 | 0.5660 |
| 0.7500 | 0.6739 | 0.4692 |
| 1.2500 | 0.8810 | 0.3717 |
| 2.5000 | 1.2730 | 0.2722 |
| 5.0000 | 1.8469 | 0.1987 |
| 7.5000 | 2.2960 | 0.1636 |
| 10.0000 | 2.6748 | 0.1408 |
| 15.0000 | 3.2958 | 0.1098 |
| 20.0000 | 3.7870 | 0.0876 |
| 25.0000 | 4.1782 | 0.0694 |
| 30.0000 | 4.4844 | 0.0534 |
| 35.0000 | 4.7148 | 0.0389 |
| 40.0000 | 4.8750 | 0.0253 |
| 45.0000 | 4.9691 | 0.0124 |
| 50.0000 | 5.0000 | 0.0000 |
| 55.0000 | 4.9676 | 0.0133 |
| 60.0000 | 4.8631 | 0.0289 |
| 65.0000 | 4.6753 | 0.0466 |
| 70.0000 | 4.3932 | 0.0666 |
| 75.0000 | 4.0057 | 0.0888 |
| 80.0000 | 3.5018 | 0.1132 |
| 85.0000 | 2.8703 | 0.1398 |
| 90.0000 | 2.1003 | 0.1686 |
| 95.0000 | 1.1805 | 0.1997 |
| 100.0000 | 0.1000 | 0.2329 |
| L.E. radius = 0.275 percent chord | ||
| NACA 0010-64 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.9880 | 0.9266 |
| 0.7500 | 1.1932 | 0.7345 |
| 1.2500 | 1.5062 | 0.5421 |
| 2.5000 | 2.0428 | 0.3497 |
| 5.0000 | 2.7205 | 0.2160 |
| 7.5000 | 3.1808 | 0.1583 |
| 10.0000 | 3.5315 | 0.1247 |
| 15.0000 | 4.0471 | 0.0855 |
| 20.0000 | 4.4115 | 0.0617 |
| 25.0000 | 4.6742 | 0.0440 |
| 30.0000 | 4.8556 | 0.0288 |
| 35.0000 | 4.9637 | 0.0145 |
| 40.0000 | 5.0000 | 0.0000 |
| 45.0000 | 4.9634 | 0.0146 |
| 50.0000 | 4.8547 | 0.0289 |
| 55.0000 | 4.6751 | 0.0429 |
| 60.0000 | 4.4261 | 0.0567 |
| 65.0000 | 4.1091 | 0.0701 |
| 70.0000 | 3.7254 | 0.0833 |
| 75.0000 | 3.2764 | 0.0962 |
| 80.0000 | 2.7634 | 0.1089 |
| 85.0000 | 2.1879 | 0.1213 |
| 90.0000 | 1.5513 | 0.1334 |
| 95.0000 | 0.8548 | 0.1452 |
| 100.0000 | 0.1000 | 0.1567 |
| L.E. radius = 1.102 percent chord | ||
| NACA 0010-65 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.9728 | 0.8967 |
| 0.7500 | 1.1705 | 0.7049 |
| 1.2500 | 1.4690 | 0.5133 |
| 2.5000 | 1.9707 | 0.3229 |
| 5.0000 | 2.5862 | 0.1929 |
| 7.5000 | 2.9935 | 0.1390 |
| 10.0000 | 3.3005 | 0.1091 |
| 15.0000 | 3.7556 | 0.0769 |
| 20.0000 | 4.0938 | 0.0598 |
| 25.0000 | 4.3631 | 0.0485 |
| 30.0000 | 4.5820 | 0.0393 |
| 35.0000 | 4.7569 | 0.0306 |
| 40.0000 | 4.8877 | 0.0215 |
| 45.0000 | 4.9707 | 0.0115 |
| 50.0000 | 5.0000 | 0.0000 |
| 55.0000 | 4.9676 | 0.0133 |
| 60.0000 | 4.8631 | 0.0289 |
| 65.0000 | 4.6753 | 0.0466 |
| 70.0000 | 4.3932 | 0.0666 |
| 75.0000 | 4.0057 | 0.0888 |
| 80.0000 | 3.5018 | 0.1132 |
| 85.0000 | 2.8703 | 0.1398 |
| 90.0000 | 2.1003 | 0.1686 |
| 95.0000 | 1.1805 | 0.1997 |
| 100.0000 | 0.1000 | 0.2329 |
| L.E. radius = 1.102 percent chord | ||
| NACA 0010-66 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.9820 | 0.9147 |
| 0.7500 | 1.1842 | 0.7224 |
| 1.2500 | 1.4912 | 0.5299 |
| 2.5000 | 2.0123 | 0.3372 |
| 5.0000 | 2.6580 | 0.2030 |
| 7.5000 | 3.0855 | 0.1452 |
| 10.0000 | 3.4036 | 0.1119 |
| 15.0000 | 3.8584 | 0.0743 |
| 20.0000 | 4.1735 | 0.0535 |
| 25.0000 | 4.4056 | 0.0402 |
| 30.0000 | 4.5823 | 0.0309 |
| 35.0000 | 4.7186 | 0.0239 |
| 40.0000 | 4.8234 | 0.0182 |
| 45.0000 | 4.9017 | 0.0132 |
| 50.0000 | 4.9565 | 0.0087 |
| 55.0000 | 4.9891 | 0.0044 |
| 60.0000 | 5.0000 | 0.0000 |
| 65.0000 | 4.9808 | 0.0093 |
| 70.0000 | 4.8905 | 0.0285 |
| 75.0000 | 4.6798 | 0.0575 |
| 80.0000 | 4.2996 | 0.0963 |
| 85.0000 | 3.7007 | 0.1449 |
| 90.0000 | 2.8339 | 0.2034 |
| 95.0000 | 1.6501 | 0.2717 |
| 100.0000 | 0.1000 | 0.3499 |
| L.E. radius = 1.102 percent chord | ||
| NACA 0012-34 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.6867 | 0.7418 |
| 0.7500 | 0.8560 | 0.6246 |
| 1.2500 | 1.1348 | 0.5054 |
| 2.5000 | 1.6761 | 0.3807 |
| 5.0000 | 2.4874 | 0.2825 |
| 7.5000 | 3.1245 | 0.2310 |
| 10.0000 | 3.6546 | 0.1948 |
| 15.0000 | 4.4889 | 0.1420 |
| 20.0000 | 5.0953 | 0.1021 |
| 25.0000 | 5.5222 | 0.0696 |
| 30.0000 | 5.8003 | 0.0424 |
| 35.0000 | 5.9530 | 0.0194 |
| 40.0000 | 6.0000 | 0.0000 |
| 45.0000 | 5.9561 | 0.0175 |
| 50.0000 | 5.8256 | 0.0347 |
| 55.0000 | 5.6102 | 0.0515 |
| 60.0000 | 5.3114 | 0.0680 |
| 65.0000 | 4.9309 | 0.0841 |
| 70.0000 | 4.4704 | 0.1000 |
| 75.0000 | 3.9316 | 0.1155 |
| 80.0000 | 3.3161 | 0.1307 |
| 85.0000 | 2.6255 | 0.1455 |
| 90.0000 | 1.8615 | 0.1600 |
| 95.0000 | 1.0258 | 0.1742 |
| 100.0000 | 0.1200 | 0.1881 |
| L.E. radius = 0.397 percent chord | ||
| NACA 0012-64 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.1855 | 1.1120 |
| 0.7500 | 1.4318 | 0.8813 |
| 1.2500 | 1.8074 | 0.6506 |
| 2.5000 | 2.4513 | 0.4197 |
| 5.0000 | 3.2647 | 0.2592 |
| 7.5000 | 3.8170 | 0.1900 |
| 10.0000 | 4.2378 | 0.1497 |
| 15.0000 | 4.8565 | 0.1027 |
| 20.0000 | 5.2938 | 0.0741 |
| 25.0000 | 5.6091 | 0.0528 |
| 30.0000 | 5.8267 | 0.0346 |
| 35.0000 | 5.9564 | 0.0173 |
| 40.0000 | 6.0000 | 0.0000 |
| 45.0000 | 5.9561 | 0.0175 |
| 50.0000 | 5.8256 | 0.0347 |
| 55.0000 | 5.6102 | 0.0515 |
| 60.0000 | 5.3114 | 0.0680 |
| 65.0000 | 4.9309 | 0.0841 |
| 70.0000 | 4.4704 | 0.1000 |
| 75.0000 | 3.9316 | 0.1155 |
| 80.0000 | 3.3161 | 0.1307 |
| 85.0000 | 2.6255 | 0.1455 |
| 90.0000 | 1.8615 | 0.1600 |
| 95.0000 | 1.0258 | 0.1742 |
| 100.0000 | 0.1200 | 0.1881 |
| L.E. radius = 1.587 percent chord | ||
| NACA 16-006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.4128 | 0.4057 |
| 0.7500 | 0.5037 | 0.3287 |
| 1.2500 | 0.6462 | 0.2514 |
| 2.5000 | 0.9034 | 0.1734 |
| 5.0000 | 1.2560 | 0.1181 |
| 7.5000 | 1.5171 | 0.0932 |
| 10.0000 | 1.7300 | 0.0781 |
| 15.0000 | 2.0694 | 0.0593 |
| 20.0000 | 2.3336 | 0.0470 |
| 25.0000 | 2.5439 | 0.0374 |
| 30.0000 | 2.7102 | 0.0292 |
| 35.0000 | 2.8373 | 0.0217 |
| 40.0000 | 2.9276 | 0.0144 |
| 45.0000 | 2.9818 | 0.0073 |
| 50.0000 | 3.0000 | 0.0000 |
| 55.0000 | 2.9806 | 0.0080 |
| 60.0000 | 2.9178 | 0.0173 |
| 65.0000 | 2.8052 | 0.0280 |
| 70.0000 | 2.6359 | 0.0400 |
| 75.0000 | 2.4034 | 0.0533 |
| 80.0000 | 2.1011 | 0.0679 |
| 85.0000 | 1.7222 | 0.0839 |
| 90.0000 | 1.2602 | 0.1012 |
| 95.0000 | 0.7083 | 0.1198 |
| 100.0000 | 0.0600 | 0.1398 |
| L.E. radius = 0.176 percent chord | ||
| NACA 16-009 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.6192 | 0.6086 |
| 0.7500 | 0.7555 | 0.4930 |
| 1.2500 | 0.9693 | 0.3770 |
| 2.5000 | 1.3550 | 0.2602 |
| 5.0000 | 1.8840 | 0.1771 |
| 7.5000 | 2.2756 | 0.1399 |
| 10.0000 | 2.5950 | 0.1172 |
| 15.0000 | 3.1042 | 0.0890 |
| 20.0000 | 3.5004 | 0.0705 |
| 25.0000 | 3.8158 | 0.0562 |
| 30.0000 | 4.0653 | 0.0438 |
| 35.0000 | 4.2559 | 0.0325 |
| 40.0000 | 4.3913 | 0.0217 |
| 45.0000 | 4.4727 | 0.0109 |
| 50.0000 | 4.5000 | 0.0000 |
| 55.0000 | 4.4709 | 0.0120 |
| 60.0000 | 4.3768 | 0.0260 |
| 65.0000 | 4.2078 | 0.0420 |
| 70.0000 | 3.9539 | 0.0599 |
| 75.0000 | 3.6052 | 0.0799 |
| 80.0000 | 3.1516 | 0.1019 |
| 85.0000 | 2.5833 | 0.1258 |
| 90.0000 | 1.8902 | 0.1518 |
| 95.0000 | 1.0625 | 0.1797 |
| 100.0000 | 0.0900 | 0.2096 |
| L.E. radius = 0.397 percent chord | ||
| NACA 16-012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 0.8256 | 0.8115 |
| 0.7500 | 1.0073 | 0.6573 |
| 1.2500 | 1.2924 | 0.5027 |
| 2.5000 | 1.8067 | 0.3469 |
| 5.0000 | 2.5120 | 0.2362 |
| 7.5000 | 3.0342 | 0.1865 |
| 10.0000 | 3.4600 | 0.1562 |
| 15.0000 | 4.1389 | 0.1186 |
| 20.0000 | 4.6671 | 0.0940 |
| 25.0000 | 5.0877 | 0.0749 |
| 30.0000 | 5.4203 | 0.0585 |
| 35.0000 | 5.6746 | 0.0434 |
| 40.0000 | 5.8551 | 0.0289 |
| 45.0000 | 5.9636 | 0.0145 |
| 50.0000 | 6.0000 | 0.0000 |
| 55.0000 | 5.9611 | 0.0160 |
| 60.0000 | 5.8357 | 0.0346 |
| 65.0000 | 5.6103 | 0.0559 |
| 70.0000 | 5.2718 | 0.0799 |
| 75.0000 | 4.8069 | 0.1065 |
| 80.0000 | 4.2022 | 0.1358 |
| 85.0000 | 3.4444 | 0.1677 |
| 90.0000 | 2.5203 | 0.2023 |
| 95.0000 | 1.4166 | 0.2396 |
| 100.0000 | 0.1200 | 0.2795 |
| L.E. radius = 0.705 percent chord | ||
| NACA 16-015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.0321 | 1.0144 |
| 0.7500 | 1.2591 | 0.8217 |
| 1.2500 | 1.6155 | 0.6284 |
| 2.5000 | 2.2584 | 0.4336 |
| 5.0000 | 3.1400 | 0.2952 |
| 7.5000 | 3.7927 | 0.2331 |
| 10.0000 | 4.3250 | 0.1953 |
| 15.0000 | 5.1736 | 0.1483 |
| 20.0000 | 5.8339 | 0.1175 |
| 25.0000 | 6.3597 | 0.0936 |
| 30.0000 | 6.7754 | 0.0731 |
| 35.0000 | 7.0932 | 0.0542 |
| 40.0000 | 7.3189 | 0.0361 |
| 45.0000 | 7.4545 | 0.0181 |
| 50.0000 | 7.5000 | 0.0000 |
| 55.0000 | 7.4514 | 0.0200 |
| 60.0000 | 7.2946 | 0.0433 |
| 65.0000 | 7.0129 | 0.0699 |
| 70.0000 | 6.5898 | 0.0999 |
| 75.0000 | 6.0086 | 0.1332 |
| 80.0000 | 5.2527 | 0.1698 |
| 85.0000 | 4.3055 | 0.2097 |
| 90.0000 | 3.1504 | 0.2529 |
| 95.0000 | 1.7708 | 0.2995 |
| 100.0000 | 0.1500 | 0.3494 |
| L.E. radius = 1.102 percent chord | ||
| NACA 16-018 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.2385 | 1.2172 |
| 0.7500 | 1.5110 | 0.9860 |
| 1.2500 | 1.9386 | 0.7541 |
| 2.5000 | 2.7101 | 0.5203 |
| 5.0000 | 3.7680 | 0.3542 |
| 7.5000 | 4.5513 | 0.2797 |
| 10.0000 | 5.1900 | 0.2343 |
| 15.0000 | 6.2083 | 0.1780 |
| 20.0000 | 7.0007 | 0.1410 |
| 25.0000 | 7.6316 | 0.1123 |
| 30.0000 | 8.1305 | 0.0877 |
| 35.0000 | 8.5119 | 0.0651 |
| 40.0000 | 8.7827 | 0.0433 |
| 45.0000 | 8.9454 | 0.0218 |
| 50.0000 | 9.0000 | 0.0000 |
| 55.0000 | 8.9417 | 0.0240 |
| 60.0000 | 8.7535 | 0.0520 |
| 65.0000 | 8.4155 | 0.0839 |
| 70.0000 | 7.9078 | 0.1199 |
| 75.0000 | 7.2103 | 0.1598 |
| 80.0000 | 6.3033 | 0.2037 |
| 85.0000 | 5.1666 | 0.2516 |
| 90.0000 | 3.7805 | 0.3035 |
| 95.0000 | 2.1249 | 0.3594 |
| 100.0000 | 0.1800 | 0.4193 |
| L.E. radius = 1.587 percent chord | ||
| NACA 16-021 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | ******** |
| 0.5000 | 1.4449 | 1.4201 |
| 0.7500 | 1.7628 | 1.1503 |
| 1.2500 | 2.2617 | 0.8797 |
| 2.5000 | 3.1618 | 0.6070 |
| 5.0000 | 4.3960 | 0.4133 |
| 7.5000 | 5.3098 | 0.3263 |
| 10.0000 | 6.0550 | 0.2734 |
| 15.0000 | 7.2430 | 0.2076 |
| 20.0000 | 8.1675 | 0.1645 |
| 25.0000 | 8.9036 | 0.1310 |
| 30.0000 | 9.4856 | 0.1023 |
| 35.0000 | 9.9305 | 0.0759 |
| 40.0000 | 10.2464 | 0.0505 |
| 45.0000 | 10.4363 | 0.0254 |
| 50.0000 | 10.5000 | 0.0000 |
| 55.0000 | 10.4320 | 0.0280 |
| 60.0000 | 10.2124 | 0.0606 |
| 65.0000 | 9.8181 | 0.0979 |
| 70.0000 | 9.2257 | 0.1398 |
| 75.0000 | 8.4120 | 0.1864 |
| 80.0000 | 7.3538 | 0.2377 |
| 85.0000 | 6.0277 | 0.2935 |
| 90.0000 | 4.4106 | 0.3541 |
| 95.0000 | 2.4791 | 0.4193 |
| 100.0000 | 0.2100 | 0.4891 |
| L.E. radius = 2.160 percent chord | ||
| NACA 63-006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.5032 | 0.4769 |
| 0.7500 | 0.6084 | 0.3784 |
| 1.2500 | 0.7710 | 0.2808 |
| 2.5000 | 1.0565 | 0.1946 |
| 5.0000 | 1.4624 | 0.1383 |
| 7.5000 | 1.7668 | 0.1077 |
| 10.0000 | 2.0105 | 0.0891 |
| 15.0000 | 2.3869 | 0.0638 |
| 20.0000 | 2.6573 | 0.0451 |
| 25.0000 | 2.8424 | 0.0294 |
| 30.0000 | 2.9558 | 0.0154 |
| 35.0000 | 2.9990 | 0.0013 |
| 40.0000 | 2.9712 | -0.0124 |
| 45.0000 | 2.8764 | -0.0253 |
| 50.0000 | 2.7218 | -0.0364 |
| 55.0000 | 2.5160 | -0.0456 |
| 60.0000 | 2.2679 | -0.0536 |
| 65.0000 | 1.9844 | -0.0599 |
| 70.0000 | 1.6726 | -0.0646 |
| 75.0000 | 1.3431 | -0.0672 |
| 80.0000 | 1.0076 | -0.0671 |
| 85.0000 | 0.6804 | -0.0633 |
| 90.0000 | 0.3821 | -0.0555 |
| 95.0000 | 0.1371 | -0.0405 |
| 100.0000 | 0.0000 | -0.0016 |
| L.E. radius = 0.267 percent chord | ||
| NACA 63-008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6669 | 0.6355 |
| 0.7500 | 0.8105 | 0.5022 |
| 1.2500 | 1.0250 | 0.3752 |
| 2.5000 | 1.4068 | 0.2610 |
| 5.0000 | 1.9520 | 0.1853 |
| 7.5000 | 2.3587 | 0.1442 |
| 10.0000 | 2.6859 | 0.1191 |
| 15.0000 | 3.1894 | 0.0852 |
| 20.0000 | 3.5499 | 0.0599 |
| 25.0000 | 3.7965 | 0.0391 |
| 30.0000 | 3.9458 | 0.0200 |
| 35.0000 | 3.9998 | 0.0007 |
| 40.0000 | 3.9577 | -0.0176 |
| 45.0000 | 3.8253 | -0.0351 |
| 50.0000 | 3.6131 | -0.0498 |
| 55.0000 | 3.3336 | -0.0618 |
| 60.0000 | 2.9982 | -0.0722 |
| 65.0000 | 2.6174 | -0.0802 |
| 70.0000 | 2.2000 | -0.0858 |
| 75.0000 | 1.7615 | -0.0891 |
| 80.0000 | 1.3175 | -0.0882 |
| 85.0000 | 0.8871 | -0.0830 |
| 90.0000 | 0.4961 | -0.0725 |
| 95.0000 | 0.1776 | -0.0529 |
| 100.0000 | 0.0000 | -0.0021 |
| L.E. radius = 0.471 percent chord | ||
| NACA 63-009 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.7502 | 0.7111 |
| 0.7500 | 0.9067 | 0.5667 |
| 1.2500 | 1.1503 | 0.4228 |
| 2.5000 | 1.5804 | 0.2946 |
| 5.0000 | 2.1955 | 0.2092 |
| 7.5000 | 2.6552 | 0.1627 |
| 10.0000 | 3.0239 | 0.1342 |
| 15.0000 | 3.5914 | 0.0959 |
| 20.0000 | 3.9972 | 0.0674 |
| 25.0000 | 4.2743 | 0.0439 |
| 30.0000 | 4.4413 | 0.0225 |
| 35.0000 | 4.5001 | 0.0005 |
| 40.0000 | 4.4499 | -0.0204 |
| 45.0000 | 4.2973 | -0.0401 |
| 50.0000 | 4.0557 | -0.0565 |
| 55.0000 | 3.7381 | -0.0701 |
| 60.0000 | 3.3589 | -0.0811 |
| 65.0000 | 2.9282 | -0.0904 |
| 70.0000 | 2.4587 | -0.0966 |
| 75.0000 | 1.9652 | -0.0997 |
| 80.0000 | 1.4671 | -0.0985 |
| 85.0000 | 0.9871 | -0.0925 |
| 90.0000 | 0.5511 | -0.0806 |
| 95.0000 | 0.1972 | -0.0589 |
| 100.0000 | 0.0000 | -0.0023 |
| L.E. radius = 0.590 percent chord | ||
| NACA 63-010 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.8281 | 0.7910 |
| 0.7500 | 1.0017 | 0.6311 |
| 1.2500 | 1.2748 | 0.4702 |
| 2.5000 | 1.7559 | 0.3279 |
| 5.0000 | 2.4400 | 0.2331 |
| 7.5000 | 2.9508 | 0.1812 |
| 10.0000 | 3.3614 | 0.1495 |
| 15.0000 | 3.9949 | 0.1065 |
| 20.0000 | 4.4452 | 0.0748 |
| 25.0000 | 4.7528 | 0.0488 |
| 30.0000 | 4.9374 | 0.0249 |
| 35.0000 | 5.0003 | 0.0003 |
| 40.0000 | 4.9414 | -0.0233 |
| 45.0000 | 4.7683 | -0.0452 |
| 50.0000 | 4.4960 | -0.0634 |
| 55.0000 | 4.1403 | -0.0784 |
| 60.0000 | 3.7158 | -0.0903 |
| 65.0000 | 3.2359 | -0.1007 |
| 70.0000 | 2.7129 | -0.1074 |
| 75.0000 | 2.1659 | -0.1101 |
| 80.0000 | 1.6144 | -0.1088 |
| 85.0000 | 1.0845 | -0.1018 |
| 90.0000 | 0.6045 | -0.0884 |
| 95.0000 | 0.2161 | -0.0648 |
| 100.0000 | 0.0000 | -0.0025 |
| L.E. radius = 0.721 percent chord | ||
| NACA 63-012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.9806 | 0.9487 |
| 0.7500 | 1.1943 | 0.7544 |
| 1.2500 | 1.5189 | 0.5659 |
| 2.5000 | 2.0981 | 0.3964 |
| 5.0000 | 2.9250 | 0.2818 |
| 7.5000 | 3.5436 | 0.2186 |
| 10.0000 | 4.0384 | 0.1800 |
| 15.0000 | 4.8003 | 0.1280 |
| 20.0000 | 5.3432 | 0.0899 |
| 25.0000 | 5.7115 | 0.0585 |
| 30.0000 | 5.9304 | 0.0295 |
| 35.0000 | 6.0005 | -0.0008 |
| 40.0000 | 5.9220 | -0.0299 |
| 45.0000 | 5.7051 | -0.0557 |
| 50.0000 | 5.3697 | -0.0777 |
| 55.0000 | 4.9353 | -0.0957 |
| 60.0000 | 4.4204 | -0.1100 |
| 65.0000 | 3.8400 | -0.1220 |
| 70.0000 | 3.2115 | -0.1294 |
| 75.0000 | 2.5568 | -0.1319 |
| 80.0000 | 1.9004 | -0.1298 |
| 85.0000 | 1.2721 | -0.1201 |
| 90.0000 | 0.7077 | -0.1038 |
| 95.0000 | 0.2521 | -0.0759 |
| 100.0000 | 0.0000 | -0.0030 |
| L.E. radius = 1.004 percent chord | ||
| NACA 63-015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.2048 | 1.1720 |
| 0.7500 | 1.4663 | 0.9408 |
| 1.2500 | 1.8722 | 0.7103 |
| 2.5000 | 2.6035 | 0.5007 |
| 5.0000 | 3.6493 | 0.3560 |
| 7.5000 | 4.4282 | 0.2758 |
| 10.0000 | 5.0528 | 0.2267 |
| 15.0000 | 6.0118 | 0.1606 |
| 20.0000 | 6.6936 | 0.1128 |
| 25.0000 | 7.1534 | 0.0727 |
| 30.0000 | 7.4223 | 0.0348 |
| 35.0000 | 7.4992 | -0.0039 |
| 40.0000 | 7.3859 | -0.0416 |
| 45.0000 | 7.0988 | -0.0733 |
| 50.0000 | 6.6640 | -0.0996 |
| 55.0000 | 6.1071 | -0.1219 |
| 60.0000 | 5.4526 | -0.1398 |
| 65.0000 | 4.7197 | -0.1530 |
| 70.0000 | 3.9318 | -0.1606 |
| 75.0000 | 3.1176 | -0.1636 |
| 80.0000 | 2.3075 | -0.1597 |
| 85.0000 | 1.5386 | -0.1474 |
| 90.0000 | 0.8525 | -0.1262 |
| 95.0000 | 0.3028 | -0.0912 |
| 100.0000 | 0.0000 | -0.0037 |
| L.E. radius = 1.473 percent chord | ||
| NACA 63-018 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.4062 | 1.3916 |
| 0.7500 | 1.7179 | 1.1250 |
| 1.2500 | 2.2055 | 0.8557 |
| 2.5000 | 3.0877 | 0.6087 |
| 5.0000 | 4.3623 | 0.4329 |
| 7.5000 | 5.3085 | 0.3344 |
| 10.0000 | 6.0653 | 0.2744 |
| 15.0000 | 7.2264 | 0.1941 |
| 20.0000 | 8.0473 | 0.1360 |
| 25.0000 | 8.5989 | 0.0864 |
| 30.0000 | 8.9163 | 0.0397 |
| 35.0000 | 8.9961 | -0.0075 |
| 40.0000 | 8.8421 | -0.0525 |
| 45.0000 | 8.4784 | -0.0910 |
| 50.0000 | 7.9384 | -0.1241 |
| 55.0000 | 7.2544 | -0.1488 |
| 60.0000 | 6.4567 | -0.1693 |
| 65.0000 | 5.5686 | -0.1843 |
| 70.0000 | 4.6229 | -0.1935 |
| 75.0000 | 3.6506 | -0.1945 |
| 80.0000 | 2.6912 | -0.1873 |
| 85.0000 | 1.7872 | -0.1713 |
| 90.0000 | 0.9864 | -0.1464 |
| 95.0000 | 0.3489 | -0.1049 |
| 100.0000 | 0.0000 | -0.0044 |
| L.E. radius = 1.950 percent chord | ||
| NACA 63-021 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.5833 | 1.6008 |
| 0.7500 | 1.9443 | 1.3052 |
| 1.2500 | 2.5137 | 1.0015 |
| 2.5000 | 3.5542 | 0.7193 |
| 5.0000 | 5.0623 | 0.5128 |
| 7.5000 | 6.1804 | 0.3949 |
| 10.0000 | 7.0749 | 0.3234 |
| 15.0000 | 8.4405 | 0.2288 |
| 20.0000 | 9.4054 | 0.1594 |
| 25.0000 | 10.0498 | 0.1000 |
| 30.0000 | 10.4129 | 0.0450 |
| 35.0000 | 10.4911 | -0.0136 |
| 40.0000 | 10.2904 | -0.0657 |
| 45.0000 | 9.8440 | -0.1114 |
| 50.0000 | 9.1920 | -0.1479 |
| 55.0000 | 8.3774 | -0.1766 |
| 60.0000 | 7.4334 | -0.1995 |
| 65.0000 | 6.3891 | -0.2162 |
| 70.0000 | 5.2836 | -0.2240 |
| 75.0000 | 4.1573 | -0.2241 |
| 80.0000 | 3.0531 | -0.2151 |
| 85.0000 | 2.0219 | -0.1959 |
| 90.0000 | 1.1111 | -0.1658 |
| 95.0000 | 0.3922 | -0.1178 |
| 100.0000 | 0.0000 | -0.0050 |
| L.E. radius = 2.399 percent chord | ||
| NACA 63A006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.5051 | 0.4636 |
| 0.7500 | 0.6087 | 0.3639 |
| 1.2500 | 0.7666 | 0.2794 |
| 2.5000 | 1.0533 | 0.1951 |
| 5.0000 | 1.4540 | 0.1354 |
| 7.5000 | 1.7531 | 0.1067 |
| 10.0000 | 1.9943 | 0.0882 |
| 15.0000 | 2.3662 | 0.0625 |
| 20.0000 | 2.6344 | 0.0448 |
| 25.0000 | 2.8224 | 0.0310 |
| 30.0000 | 2.9433 | 0.0178 |
| 35.0000 | 2.9956 | 0.0038 |
| 40.0000 | 2.9838 | -0.0090 |
| 45.0000 | 2.9102 | -0.0207 |
| 50.0000 | 2.7817 | -0.0306 |
| 55.0000 | 2.6048 | -0.0399 |
| 60.0000 | 2.3871 | -0.0470 |
| 65.0000 | 2.1340 | -0.0531 |
| 70.0000 | 1.8528 | -0.0588 |
| 75.0000 | 1.5522 | -0.0613 |
| 80.0000 | 1.2455 | -0.0618 |
| 85.0000 | 0.9383 | -0.0614 |
| 90.0000 | 0.6309 | -0.0623 |
| 95.0000 | 0.3187 | -0.0573 |
| 100.0000 | 0.0091 | -0.8441 |
| L.E. radius = 0.278 percent chord | ||
| NACA 63A008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6687 | 0.6119 |
| 0.7500 | 0.8056 | 0.4843 |
| 1.2500 | 1.0144 | 0.3751 |
| 2.5000 | 1.4012 | 0.2617 |
| 5.0000 | 1.9372 | 0.1816 |
| 7.5000 | 2.3398 | 0.1428 |
| 10.0000 | 2.6620 | 0.1180 |
| 15.0000 | 3.1592 | 0.0836 |
| 20.0000 | 3.5174 | 0.0598 |
| 25.0000 | 3.7684 | 0.0409 |
| 30.0000 | 3.9287 | 0.0231 |
| 35.0000 | 3.9957 | 0.0049 |
| 40.0000 | 3.9765 | -0.0121 |
| 45.0000 | 3.8744 | -0.0282 |
| 50.0000 | 3.6988 | -0.0422 |
| 55.0000 | 3.4592 | -0.0539 |
| 60.0000 | 3.1662 | -0.0639 |
| 65.0000 | 2.8272 | -0.0718 |
| 70.0000 | 2.4511 | -0.0782 |
| 75.0000 | 2.0515 | -0.0815 |
| 80.0000 | 1.6453 | -0.0812 |
| 85.0000 | 1.2391 | -0.0811 |
| 90.0000 | 0.8328 | -0.0827 |
| 95.0000 | 0.4216 | -0.0748 |
| 100.0000 | 0.0123 | -1.0407 |
| L.E. radius = 0.483 percent chord | ||
| NACA 63A010 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.8246 | 0.7590 |
| 0.7500 | 0.9943 | 0.6051 |
| 1.2500 | 1.2581 | 0.4712 |
| 2.5000 | 1.7425 | 0.3298 |
| 5.0000 | 2.4185 | 0.2284 |
| 7.5000 | 2.9234 | 0.1795 |
| 10.0000 | 3.3290 | 0.1482 |
| 15.0000 | 3.9534 | 0.1051 |
| 20.0000 | 4.4026 | 0.0750 |
| 25.0000 | 4.7162 | 0.0508 |
| 30.0000 | 4.9153 | 0.0279 |
| 35.0000 | 4.9963 | 0.0054 |
| 40.0000 | 4.9683 | -0.0158 |
| 45.0000 | 4.8355 | -0.0363 |
| 50.0000 | 4.6110 | -0.0533 |
| 55.0000 | 4.3072 | -0.0678 |
| 60.0000 | 3.9373 | -0.0805 |
| 65.0000 | 3.5108 | -0.0908 |
| 70.0000 | 3.0402 | -0.0970 |
| 75.0000 | 2.5422 | -0.1009 |
| 80.0000 | 2.0383 | -0.1006 |
| 85.0000 | 1.5346 | -0.1005 |
| 90.0000 | 1.0300 | -0.1032 |
| 95.0000 | 0.5234 | -0.0916 |
| 100.0000 | 0.0155 | -1.2272 |
| L.E. radius = 0.724 percent chord | ||
| NACA 63A012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.9698 | 0.9052 |
| 0.7500 | 1.1718 | 0.7263 |
| 1.2500 | 1.4916 | 0.5694 |
| 2.5000 | 2.0770 | 0.3993 |
| 5.0000 | 2.8956 | 0.2760 |
| 7.5000 | 3.5048 | 0.2168 |
| 10.0000 | 3.9953 | 0.1786 |
| 15.0000 | 4.7491 | 0.1270 |
| 20.0000 | 5.2891 | 0.0903 |
| 25.0000 | 5.6657 | 0.0609 |
| 30.0000 | 5.9033 | 0.0322 |
| 35.0000 | 5.9971 | 0.0052 |
| 40.0000 | 5.9587 | -0.0204 |
| 45.0000 | 5.7933 | -0.0447 |
| 50.0000 | 5.5184 | -0.0645 |
| 55.0000 | 5.1487 | -0.0820 |
| 60.0000 | 4.7004 | -0.0968 |
| 65.0000 | 4.1862 | -0.1084 |
| 70.0000 | 3.6214 | -0.1167 |
| 75.0000 | 3.0259 | -0.1197 |
| 80.0000 | 2.4255 | -0.1200 |
| 85.0000 | 1.8251 | -0.1197 |
| 90.0000 | 1.2249 | -0.1235 |
| 95.0000 | 0.6238 | -0.1077 |
| 100.0000 | 0.0189 | -1.4097 |
| L.E. radius = 0.990 percent chord | ||
| NACA 63A015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.1717 | 1.1115 |
| 0.7500 | 1.4206 | 0.9013 |
| 1.2500 | 1.8245 | 0.7188 |
| 2.5000 | 2.5662 | 0.5061 |
| 5.0000 | 3.6024 | 0.3493 |
| 7.5000 | 4.3724 | 0.2738 |
| 10.0000 | 4.9920 | 0.2249 |
| 15.0000 | 5.9403 | 0.1606 |
| 20.0000 | 6.6193 | 0.1138 |
| 25.0000 | 7.0925 | 0.0771 |
| 30.0000 | 7.3867 | 0.0391 |
| 35.0000 | 7.4983 | 0.0050 |
| 40.0000 | 7.4418 | -0.0279 |
| 45.0000 | 7.2244 | -0.0577 |
| 50.0000 | 6.8701 | -0.0838 |
| 55.0000 | 6.3995 | -0.1044 |
| 60.0000 | 5.8321 | -0.1214 |
| 65.0000 | 5.1842 | -0.1363 |
| 70.0000 | 4.4774 | -0.1460 |
| 75.0000 | 3.7378 | -0.1487 |
| 80.0000 | 2.9944 | -0.1491 |
| 85.0000 | 2.2530 | -0.1479 |
| 90.0000 | 1.5085 | -0.1531 |
| 95.0000 | 0.7732 | -0.1309 |
| 100.0000 | 0.0242 | -1.6838 |
| L.E. radius = 1.406 percent chord | ||
| NACA 64-006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.4924 | 0.4687 |
| 0.7500 | 0.5956 | 0.3687 |
| 1.2500 | 0.7511 | 0.2696 |
| 2.5000 | 1.0213 | 0.1822 |
| 5.0000 | 1.4025 | 0.1300 |
| 7.5000 | 1.6897 | 0.1024 |
| 10.0000 | 1.9236 | 0.0860 |
| 15.0000 | 2.2932 | 0.0635 |
| 20.0000 | 2.5675 | 0.0471 |
| 25.0000 | 2.7675 | 0.0332 |
| 30.0000 | 2.9019 | 0.0207 |
| 35.0000 | 2.9762 | 0.0090 |
| 40.0000 | 2.9855 | -0.0061 |
| 45.0000 | 2.9133 | -0.0223 |
| 50.0000 | 2.7686 | -0.0348 |
| 55.0000 | 2.5689 | -0.0448 |
| 60.0000 | 2.3246 | -0.0527 |
| 65.0000 | 2.0439 | -0.0593 |
| 70.0000 | 1.7359 | -0.0640 |
| 75.0000 | 1.4078 | -0.0671 |
| 80.0000 | 1.0699 | -0.0678 |
| 85.0000 | 0.7353 | -0.0654 |
| 90.0000 | 0.4224 | -0.0589 |
| 95.0000 | 0.1568 | -0.0458 |
| 100.0000 | 0.0000 | -0.0018 |
| L.E. radius = 0.249 percent chord | ||
| NACA 64-008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6544 | 0.6250 |
| 0.7500 | 0.7912 | 0.4919 |
| 1.2500 | 0.9999 | 0.3594 |
| 2.5000 | 1.3623 | 0.2439 |
| 5.0000 | 1.8723 | 0.1743 |
| 7.5000 | 2.2575 | 0.1372 |
| 10.0000 | 2.5706 | 0.1152 |
| 15.0000 | 3.0655 | 0.0850 |
| 20.0000 | 3.4323 | 0.0630 |
| 25.0000 | 3.6996 | 0.0443 |
| 30.0000 | 3.8782 | 0.0271 |
| 35.0000 | 3.9754 | 0.0114 |
| 40.0000 | 3.9831 | -0.0091 |
| 45.0000 | 3.8796 | -0.0313 |
| 50.0000 | 3.6797 | -0.0475 |
| 55.0000 | 3.4076 | -0.0606 |
| 60.0000 | 3.0774 | -0.0710 |
| 65.0000 | 2.7002 | -0.0793 |
| 70.0000 | 2.2874 | -0.0854 |
| 75.0000 | 1.8501 | -0.0888 |
| 80.0000 | 1.4014 | -0.0898 |
| 85.0000 | 0.9598 | -0.0861 |
| 90.0000 | 0.5496 | -0.0773 |
| 95.0000 | 0.2034 | -0.0597 |
| 100.0000 | 0.0000 | -0.0023 |
| L.E. radius = 0.446 percent chord | ||
| NACA 64-009 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.7372 | 0.6997 |
| 0.7500 | 0.8906 | 0.5511 |
| 1.2500 | 1.1249 | 0.4035 |
| 2.5000 | 1.5307 | 0.2752 |
| 5.0000 | 2.1063 | 0.1967 |
| 7.5000 | 2.5411 | 0.1547 |
| 10.0000 | 2.8944 | 0.1299 |
| 15.0000 | 3.4527 | 0.0958 |
| 20.0000 | 3.8662 | 0.0709 |
| 25.0000 | 4.1666 | 0.0498 |
| 30.0000 | 4.3672 | 0.0304 |
| 35.0000 | 4.4758 | 0.0125 |
| 40.0000 | 4.4817 | -0.0110 |
| 45.0000 | 4.3608 | -0.0361 |
| 50.0000 | 4.1324 | -0.0542 |
| 55.0000 | 3.8235 | -0.0687 |
| 60.0000 | 3.4492 | -0.0804 |
| 65.0000 | 3.0232 | -0.0893 |
| 70.0000 | 2.5581 | -0.0961 |
| 75.0000 | 2.0660 | -0.0999 |
| 80.0000 | 1.5628 | -0.1006 |
| 85.0000 | 1.0689 | -0.0962 |
| 90.0000 | 0.6112 | -0.0861 |
| 95.0000 | 0.2256 | -0.0664 |
| 100.0000 | 0.0000 | -0.0025 |
| L.E. radius = 0.566 percent chord | ||
| NACA 64-010 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.8149 | 0.7791 |
| 0.7500 | 0.9900 | 0.6094 |
| 1.2500 | 1.2474 | 0.4482 |
| 2.5000 | 1.6985 | 0.3066 |
| 5.0000 | 2.3402 | 0.2192 |
| 7.5000 | 2.8249 | 0.1723 |
| 10.0000 | 3.2185 | 0.1446 |
| 15.0000 | 3.8397 | 0.1067 |
| 20.0000 | 4.3002 | 0.0790 |
| 25.0000 | 4.6347 | 0.0553 |
| 30.0000 | 4.8571 | 0.0337 |
| 35.0000 | 4.9766 | 0.0135 |
| 40.0000 | 4.9800 | -0.0133 |
| 45.0000 | 4.8409 | -0.0410 |
| 50.0000 | 4.5834 | -0.0610 |
| 55.0000 | 4.2367 | -0.0771 |
| 60.0000 | 3.8182 | -0.0899 |
| 65.0000 | 3.3427 | -0.0994 |
| 70.0000 | 2.8252 | -0.1068 |
| 75.0000 | 2.2789 | -0.1112 |
| 80.0000 | 1.7214 | -0.1112 |
| 85.0000 | 1.1754 | -0.1061 |
| 90.0000 | 0.6711 | -0.0945 |
| 95.0000 | 0.2470 | -0.0728 |
| 100.0000 | 0.0000 | -0.0028 |
| L.E. radius = 0.701 percent chord | ||
| NACA 64-012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.9738 | 0.9297 |
| 0.7500 | 1.1797 | 0.7300 |
| 1.2500 | 1.4906 | 0.5367 |
| 2.5000 | 2.0325 | 0.3696 |
| 5.0000 | 2.8074 | 0.2645 |
| 7.5000 | 3.3913 | 0.2079 |
| 10.0000 | 3.8652 | 0.1745 |
| 15.0000 | 4.6170 | 0.1284 |
| 20.0000 | 5.1708 | 0.0950 |
| 25.0000 | 5.5721 | 0.0664 |
| 30.0000 | 5.8380 | 0.0407 |
| 35.0000 | 5.9789 | 0.0151 |
| 40.0000 | 5.9752 | -0.0186 |
| 45.0000 | 5.7973 | -0.0511 |
| 50.0000 | 5.4786 | -0.0752 |
| 55.0000 | 5.0548 | -0.0942 |
| 60.0000 | 4.5464 | -0.1092 |
| 65.0000 | 3.9722 | -0.1202 |
| 70.0000 | 3.3489 | -0.1284 |
| 75.0000 | 2.6935 | -0.1331 |
| 80.0000 | 2.0289 | -0.1323 |
| 85.0000 | 1.3818 | -0.1254 |
| 90.0000 | 0.7861 | -0.1110 |
| 95.0000 | 0.2879 | -0.0850 |
| 100.0000 | 0.0000 | -0.0033 |
| L.E. radius = 1.004 percent chord | ||
| NACA 64-015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.2087 | 1.1457 |
| 0.7500 | 1.4600 | 0.9036 |
| 1.2500 | 1.8470 | 0.6676 |
| 2.5000 | 2.5253 | 0.4649 |
| 5.0000 | 3.5013 | 0.3338 |
| 7.5000 | 4.2379 | 0.2621 |
| 10.0000 | 4.8372 | 0.2195 |
| 15.0000 | 5.7802 | 0.1616 |
| 20.0000 | 6.4783 | 0.1192 |
| 25.0000 | 6.9812 | 0.0831 |
| 30.0000 | 7.3126 | 0.0505 |
| 35.0000 | 7.4831 | 0.0171 |
| 40.0000 | 7.4629 | -0.0275 |
| 45.0000 | 7.2201 | -0.0682 |
| 50.0000 | 6.8052 | -0.0971 |
| 55.0000 | 6.2609 | -0.1195 |
| 60.0000 | 5.6148 | -0.1376 |
| 65.0000 | 4.8902 | -0.1513 |
| 70.0000 | 4.1077 | -0.1608 |
| 75.0000 | 3.2915 | -0.1647 |
| 80.0000 | 2.4688 | -0.1633 |
| 85.0000 | 1.6745 | -0.1536 |
| 90.0000 | 0.9479 | -0.1353 |
| 95.0000 | 0.3458 | -0.1022 |
| 100.0000 | 0.0000 | -0.0041 |
| L.E. radius = 1.556 percent chord | ||
| NACA 64-018 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.4302 | 1.3565 |
| 0.7500 | 1.7292 | 1.0702 |
| 1.2500 | 2.1876 | 0.7968 |
| 2.5000 | 3.0027 | 0.5615 |
| 5.0000 | 4.1865 | 0.4046 |
| 7.5000 | 5.0784 | 0.3174 |
| 10.0000 | 5.8041 | 0.2656 |
| 15.0000 | 6.9450 | 0.1953 |
| 20.0000 | 7.7867 | 0.1436 |
| 25.0000 | 8.3928 | 0.0998 |
| 30.0000 | 8.7889 | 0.0591 |
| 35.0000 | 8.9873 | 0.0182 |
| 40.0000 | 8.9433 | -0.0372 |
| 45.0000 | 8.6277 | -0.0862 |
| 50.0000 | 8.1109 | -0.1195 |
| 55.0000 | 7.4417 | -0.1463 |
| 60.0000 | 6.6543 | -0.1674 |
| 65.0000 | 5.7769 | -0.1831 |
| 70.0000 | 4.8367 | -0.1924 |
| 75.0000 | 3.8611 | -0.1964 |
| 80.0000 | 2.8838 | -0.1926 |
| 85.0000 | 1.9480 | -0.1802 |
| 90.0000 | 1.0988 | -0.1572 |
| 95.0000 | 0.3989 | -0.1186 |
| 100.0000 | 0.0000 | -0.0048 |
| L.E. radius = 2.206 percent chord | ||
| NACA 64-021 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.6389 | 1.5566 |
| 0.7500 | 1.9848 | 1.2282 |
| 1.2500 | 2.5126 | 0.9217 |
| 2.5000 | 3.4600 | 0.6594 |
| 5.0000 | 4.8583 | 0.4775 |
| 7.5000 | 5.9088 | 0.3742 |
| 10.0000 | 6.7654 | 0.3127 |
| 15.0000 | 8.1075 | 0.2296 |
| 20.0000 | 9.0976 | 0.1683 |
| 25.0000 | 9.8068 | 0.1163 |
| 30.0000 | 10.2669 | 0.0680 |
| 35.0000 | 10.4903 | 0.0180 |
| 40.0000 | 10.4156 | -0.0487 |
| 45.0000 | 10.0199 | -0.1044 |
| 50.0000 | 9.3950 | -0.1436 |
| 55.0000 | 8.5974 | -0.1745 |
| 60.0000 | 7.6644 | -0.1972 |
| 65.0000 | 6.6330 | -0.2140 |
| 70.0000 | 5.5356 | -0.2243 |
| 75.0000 | 4.4023 | -0.2274 |
| 80.0000 | 3.2766 | -0.2217 |
| 85.0000 | 2.2039 | -0.2054 |
| 90.0000 | 1.2392 | -0.1783 |
| 95.0000 | 0.4473 | -0.1335 |
| 100.0000 | 0.0000 | -0.0055 |
| L.E. radius = 2.937 percent chord | ||
| NACA 64A006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.5016 | 0.4569 |
| 0.7500 | 0.6006 | 0.3579 |
| 1.2500 | 0.7544 | 0.2660 |
| 2.5000 | 1.0264 | 0.1844 |
| 5.0000 | 1.4042 | 0.1273 |
| 7.5000 | 1.6871 | 0.1018 |
| 10.0000 | 1.9210 | 0.0858 |
| 15.0000 | 2.2861 | 0.0627 |
| 20.0000 | 2.5593 | 0.0469 |
| 25.0000 | 2.7592 | 0.0333 |
| 30.0000 | 2.8967 | 0.0214 |
| 35.0000 | 2.9768 | 0.0103 |
| 40.0000 | 2.9978 | -0.0027 |
| 45.0000 | 2.9439 | -0.0179 |
| 50.0000 | 2.8244 | -0.0295 |
| 55.0000 | 2.6521 | -0.0391 |
| 60.0000 | 2.4371 | -0.0470 |
| 65.0000 | 2.1858 | -0.0537 |
| 70.0000 | 1.9035 | -0.0592 |
| 75.0000 | 1.5998 | -0.0621 |
| 80.0000 | 1.2851 | -0.0632 |
| 85.0000 | 0.9679 | -0.0629 |
| 90.0000 | 0.6511 | -0.0650 |
| 95.0000 | 0.3289 | -0.0595 |
| 100.0000 | 0.0091 | -0.8442 |
| L.E. radius = 0.277 percent chord | ||
| NACA 64A008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6629 | 0.6037 |
| 0.7500 | 0.7934 | 0.4757 |
| 1.2500 | 0.9984 | 0.3559 |
| 2.5000 | 1.3632 | 0.2471 |
| 5.0000 | 1.8693 | 0.1706 |
| 7.5000 | 2.2480 | 0.1364 |
| 10.0000 | 2.5619 | 0.1148 |
| 15.0000 | 3.0507 | 0.0839 |
| 20.0000 | 3.4160 | 0.0628 |
| 25.0000 | 3.6826 | 0.0443 |
| 30.0000 | 3.8656 | 0.0288 |
| 35.0000 | 3.9715 | 0.0139 |
| 40.0000 | 3.9966 | -0.0046 |
| 45.0000 | 3.9194 | -0.0249 |
| 50.0000 | 3.7558 | -0.0399 |
| 55.0000 | 3.5223 | -0.0528 |
| 60.0000 | 3.2323 | -0.0630 |
| 65.0000 | 2.8955 | -0.0719 |
| 70.0000 | 2.5177 | -0.0787 |
| 75.0000 | 2.1136 | -0.0825 |
| 80.0000 | 1.6965 | -0.0840 |
| 85.0000 | 1.2776 | -0.0831 |
| 90.0000 | 0.8587 | -0.0858 |
| 95.0000 | 0.4349 | -0.0777 |
| 100.0000 | 0.0123 | -1.0408 |
| L.E. radius = 0.485 percent chord | ||
| NACA 64A010 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.8159 | 0.7495 |
| 0.7500 | 0.9823 | 0.5905 |
| 1.2500 | 1.2361 | 0.4463 |
| 2.5000 | 1.6928 | 0.3112 |
| 5.0000 | 2.3306 | 0.2145 |
| 7.5000 | 2.8060 | 0.1715 |
| 10.0000 | 3.2008 | 0.1441 |
| 15.0000 | 3.8156 | 0.1052 |
| 20.0000 | 4.2730 | 0.0789 |
| 25.0000 | 4.6074 | 0.0554 |
| 30.0000 | 4.8362 | 0.0361 |
| 35.0000 | 4.9672 | 0.0172 |
| 40.0000 | 4.9946 | -0.0073 |
| 45.0000 | 4.8920 | -0.0321 |
| 50.0000 | 4.6821 | -0.0509 |
| 55.0000 | 4.3855 | -0.0664 |
| 60.0000 | 4.0196 | -0.0792 |
| 65.0000 | 3.5956 | -0.0903 |
| 70.0000 | 3.1226 | -0.0982 |
| 75.0000 | 2.6192 | -0.1027 |
| 80.0000 | 2.1011 | -0.1042 |
| 85.0000 | 1.5813 | -0.1040 |
| 90.0000 | 1.0623 | -0.1061 |
| 95.0000 | 0.5395 | -0.0951 |
| 100.0000 | 0.0156 | -1.2262 |
| L.E. radius = 0.735 percent chord | ||
| NACA 64A012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.9578 | 0.8948 |
| 0.7500 | 1.1556 | 0.7089 |
| 1.2500 | 1.4633 | 0.5383 |
| 2.5000 | 2.0177 | 0.3760 |
| 5.0000 | 2.7879 | 0.2591 |
| 7.5000 | 3.3638 | 0.2068 |
| 10.0000 | 3.8380 | 0.1738 |
| 15.0000 | 4.5792 | 0.1269 |
| 20.0000 | 5.1311 | 0.0950 |
| 25.0000 | 5.5328 | 0.0667 |
| 30.0000 | 5.8076 | 0.0435 |
| 35.0000 | 5.9638 | 0.0201 |
| 40.0000 | 5.9916 | -0.0106 |
| 45.0000 | 5.8616 | -0.0399 |
| 50.0000 | 5.6035 | -0.0627 |
| 55.0000 | 5.2423 | -0.0808 |
| 60.0000 | 4.7995 | -0.0956 |
| 65.0000 | 4.2869 | -0.1089 |
| 70.0000 | 3.7193 | -0.1176 |
| 75.0000 | 3.1166 | -0.1230 |
| 80.0000 | 2.4985 | -0.1240 |
| 85.0000 | 1.8805 | -0.1237 |
| 90.0000 | 1.2608 | -0.1263 |
| 95.0000 | 0.6426 | -0.1117 |
| 100.0000 | 0.0189 | -1.4070 |
| L.E. radius = 1.021 percent chord | ||
| NACA 64A015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.1613 | 1.0917 |
| 0.7500 | 1.4010 | 0.8779 |
| 1.2500 | 1.7858 | 0.6767 |
| 2.5000 | 2.4841 | 0.4766 |
| 5.0000 | 3.4608 | 0.3279 |
| 7.5000 | 4.1886 | 0.2613 |
| 10.0000 | 4.7887 | 0.2192 |
| 15.0000 | 5.7217 | 0.1600 |
| 20.0000 | 6.4178 | 0.1193 |
| 25.0000 | 6.9224 | 0.0840 |
| 30.0000 | 7.2668 | 0.0542 |
| 35.0000 | 7.4596 | 0.0235 |
| 40.0000 | 7.4852 | -0.0161 |
| 45.0000 | 7.3099 | -0.0527 |
| 50.0000 | 6.9760 | -0.0806 |
| 55.0000 | 6.5157 | -0.1028 |
| 60.0000 | 5.9545 | -0.1214 |
| 65.0000 | 5.3090 | -0.1356 |
| 70.0000 | 4.5978 | -0.1470 |
| 75.0000 | 3.8479 | -0.1525 |
| 80.0000 | 3.0826 | -0.1531 |
| 85.0000 | 2.3195 | -0.1510 |
| 90.0000 | 1.5529 | -0.1567 |
| 95.0000 | 0.7949 | -0.1356 |
| 100.0000 | 0.0242 | -1.6779 |
| L.E. radius = 1.481 percent chord | ||
| NACA 65-006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.4692 | 0.4359 |
| 0.7500 | 0.5645 | 0.3380 |
| 1.2500 | 0.7048 | 0.2422 |
| 2.5000 | 0.9521 | 0.1691 |
| 5.0000 | 1.3113 | 0.1245 |
| 7.5000 | 1.5903 | 0.1013 |
| 10.0000 | 1.8242 | 0.0862 |
| 15.0000 | 2.1975 | 0.0646 |
| 20.0000 | 2.4816 | 0.0494 |
| 25.0000 | 2.6957 | 0.0368 |
| 30.0000 | 2.8510 | 0.0255 |
| 35.0000 | 2.9505 | 0.0145 |
| 40.0000 | 2.9971 | 0.0035 |
| 45.0000 | 2.9819 | -0.0099 |
| 50.0000 | 2.8978 | -0.0238 |
| 55.0000 | 2.7414 | -0.0383 |
| 60.0000 | 2.5199 | -0.0498 |
| 65.0000 | 2.2475 | -0.0585 |
| 70.0000 | 1.9344 | -0.0665 |
| 75.0000 | 1.5920 | -0.0704 |
| 80.0000 | 1.2312 | -0.0734 |
| 85.0000 | 0.8636 | -0.0729 |
| 90.0000 | 0.5068 | -0.0686 |
| 95.0000 | 0.1891 | -0.0558 |
| 100.0000 | 0.0000 | -0.0021 |
| L.E. radius = 0.230 percent chord | ||
| NACA 65-008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6220 | 0.5785 |
| 0.7500 | 0.7480 | 0.4489 |
| 1.2500 | 0.9347 | 0.3228 |
| 2.5000 | 1.2646 | 0.2266 |
| 5.0000 | 1.7462 | 0.1668 |
| 7.5000 | 2.1206 | 0.1355 |
| 10.0000 | 2.4336 | 0.1153 |
| 15.0000 | 2.9330 | 0.0863 |
| 20.0000 | 3.3121 | 0.0660 |
| 25.0000 | 3.5982 | 0.0492 |
| 30.0000 | 3.8050 | 0.0337 |
| 35.0000 | 3.9370 | 0.0192 |
| 40.0000 | 3.9975 | 0.0042 |
| 45.0000 | 3.9733 | -0.0140 |
| 50.0000 | 3.8556 | -0.0332 |
| 55.0000 | 3.6402 | -0.0524 |
| 60.0000 | 3.3388 | -0.0671 |
| 65.0000 | 2.9714 | -0.0792 |
| 70.0000 | 2.5506 | -0.0882 |
| 75.0000 | 2.0942 | -0.0937 |
| 80.0000 | 1.6150 | -0.0974 |
| 85.0000 | 1.1284 | -0.0962 |
| 90.0000 | 0.6605 | -0.0902 |
| 95.0000 | 0.2461 | -0.0723 |
| 100.0000 | 0.0000 | -0.0028 |
| L.E. radius = 0.406 percent chord | ||
| NACA 65-009 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6955 | 0.6511 |
| 0.7500 | 0.8367 | 0.5053 |
| 1.2500 | 1.0487 | 0.3628 |
| 2.5000 | 1.4200 | 0.2555 |
| 5.0000 | 1.9631 | 0.1881 |
| 7.5000 | 2.3849 | 0.1528 |
| 10.0000 | 2.7380 | 0.1299 |
| 15.0000 | 3.3005 | 0.0973 |
| 20.0000 | 3.7279 | 0.0743 |
| 25.0000 | 4.0500 | 0.0554 |
| 30.0000 | 4.2827 | 0.0378 |
| 35.0000 | 4.4307 | 0.0216 |
| 40.0000 | 4.4978 | 0.0045 |
| 45.0000 | 4.4684 | -0.0162 |
| 50.0000 | 4.3329 | -0.0381 |
| 55.0000 | 4.0863 | -0.0596 |
| 60.0000 | 3.7441 | -0.0761 |
| 65.0000 | 3.3283 | -0.0897 |
| 70.0000 | 2.8537 | -0.0989 |
| 75.0000 | 2.3401 | -0.1053 |
| 80.0000 | 1.8017 | -0.1094 |
| 85.0000 | 1.2574 | -0.1078 |
| 90.0000 | 0.7338 | -0.1005 |
| 95.0000 | 0.2740 | -0.0802 |
| 100.0000 | 0.0000 | -0.0031 |
| L.E. radius = 0.510 percent chord | ||
| NACA 65-010 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.7680 | 0.7230 |
| 0.7500 | 0.9290 | 0.5571 |
| 1.2500 | 1.1621 | 0.4024 |
| 2.5000 | 1.5747 | 0.2844 |
| 5.0000 | 2.1798 | 0.2095 |
| 7.5000 | 2.6489 | 0.1701 |
| 10.0000 | 3.0415 | 0.1446 |
| 15.0000 | 3.6681 | 0.1083 |
| 20.0000 | 4.1433 | 0.0827 |
| 25.0000 | 4.5019 | 0.0616 |
| 30.0000 | 4.7604 | 0.0418 |
| 35.0000 | 4.9247 | 0.0240 |
| 40.0000 | 4.9981 | 0.0047 |
| 45.0000 | 4.9631 | -0.0185 |
| 50.0000 | 4.8088 | -0.0434 |
| 55.0000 | 4.5308 | -0.0670 |
| 60.0000 | 4.1471 | -0.0853 |
| 65.0000 | 3.6824 | -0.1000 |
| 70.0000 | 3.1538 | -0.1102 |
| 75.0000 | 2.5830 | -0.1172 |
| 80.0000 | 1.9849 | -0.1212 |
| 85.0000 | 1.3835 | -0.1191 |
| 90.0000 | 0.8068 | -0.1105 |
| 95.0000 | 0.3007 | -0.0878 |
| 100.0000 | 0.0000 | -0.0034 |
| L.E. radius = 0.624 percent chord | ||
| NACA 65-012 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.9159 | 0.8575 |
| 0.7500 | 1.1020 | 0.6664 |
| 1.2500 | 1.3815 | 0.4827 |
| 2.5000 | 1.8796 | 0.3429 |
| 5.0000 | 2.6096 | 0.2529 |
| 7.5000 | 3.1751 | 0.2052 |
| 10.0000 | 3.6491 | 0.1742 |
| 15.0000 | 4.4038 | 0.1304 |
| 20.0000 | 4.9758 | 0.0995 |
| 25.0000 | 5.4069 | 0.0741 |
| 30.0000 | 5.7174 | 0.0500 |
| 35.0000 | 5.9135 | 0.0287 |
| 40.0000 | 5.9990 | 0.0048 |
| 45.0000 | 5.9513 | -0.0235 |
| 50.0000 | 5.7573 | -0.0545 |
| 55.0000 | 5.4141 | -0.0821 |
| 60.0000 | 4.9447 | -0.1044 |
| 65.0000 | 4.3808 | -0.1207 |
| 70.0000 | 3.7429 | -0.1342 |
| 75.0000 | 3.0579 | -0.1408 |
| 80.0000 | 2.3436 | -0.1441 |
| 85.0000 | 1.6288 | -0.1411 |
| 90.0000 | 0.9466 | -0.1298 |
| 95.0000 | 0.3533 | -0.1025 |
| 100.0000 | 0.0000 | -0.0041 |
| L.E. radius = 0.876 percent chord | ||
| NACA 65-015 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.1232 | 1.0580 |
| 0.7500 | 1.3531 | 0.8237 |
| 1.2500 | 1.7025 | 0.6001 |
| 2.5000 | 2.3226 | 0.4326 |
| 5.0000 | 3.2452 | 0.3192 |
| 7.5000 | 3.9597 | 0.2586 |
| 10.0000 | 4.5562 | 0.2194 |
| 15.0000 | 5.5058 | 0.1640 |
| 20.0000 | 6.2252 | 0.1249 |
| 25.0000 | 6.7662 | 0.0928 |
| 30.0000 | 7.1542 | 0.0626 |
| 35.0000 | 7.3985 | 0.0352 |
| 40.0000 | 7.5004 | 0.0041 |
| 45.0000 | 7.4294 | -0.0333 |
| 50.0000 | 7.1705 | -0.0709 |
| 55.0000 | 6.7223 | -0.1065 |
| 60.0000 | 6.1200 | -0.1335 |
| 65.0000 | 5.4048 | -0.1531 |
| 70.0000 | 4.6011 | -0.1664 |
| 75.0000 | 3.7457 | -0.1752 |
| 80.0000 | 2.8590 | -0.1780 |
| 85.0000 | 1.9785 | -0.1733 |
| 90.0000 | 1.1449 | -0.1576 |
| 95.0000 | 0.4283 | -0.1237 |
| 100.0000 | 0.0000 | -0.0050 |
| L.E. radius = 1.299 percent chord | ||
| NACA 65-018 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.3133 | 1.2517 |
| 0.7500 | 1.5902 | 0.9733 |
| 1.2500 | 2.0015 | 0.7166 |
| 2.5000 | 2.7505 | 0.5234 |
| 5.0000 | 3.8679 | 0.3873 |
| 7.5000 | 4.7348 | 0.3133 |
| 10.0000 | 5.4576 | 0.2654 |
| 15.0000 | 6.6051 | 0.1983 |
| 20.0000 | 7.4739 | 0.1508 |
| 25.0000 | 8.1262 | 0.1117 |
| 30.0000 | 8.5935 | 0.0756 |
| 35.0000 | 8.8854 | 0.0416 |
| 40.0000 | 9.0016 | 0.0028 |
| 45.0000 | 8.9024 | -0.0429 |
| 50.0000 | 8.5724 | -0.0897 |
| 55.0000 | 8.0120 | -0.1323 |
| 60.0000 | 7.2711 | -0.1622 |
| 65.0000 | 6.4009 | -0.1846 |
| 70.0000 | 5.4313 | -0.1999 |
| 75.0000 | 4.4043 | -0.2097 |
| 80.0000 | 3.3489 | -0.2107 |
| 85.0000 | 2.3079 | -0.2043 |
| 90.0000 | 1.3298 | -0.1838 |
| 95.0000 | 0.4989 | -0.1440 |
| 100.0000 | 0.0000 | -0.0059 |
| L.E. radius = 1.753 percent chord | ||
| NACA 65-021 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 1.4920 | 1.4266 |
| 0.7500 | 1.8064 | 1.1172 |
| 1.2500 | 2.2817 | 0.8286 |
| 2.5000 | 3.1568 | 0.6158 |
| 5.0000 | 4.4743 | 0.4576 |
| 7.5000 | 5.4976 | 0.3695 |
| 10.0000 | 6.3494 | 0.3127 |
| 15.0000 | 7.7002 | 0.2333 |
| 20.0000 | 8.7210 | 0.1771 |
| 25.0000 | 9.4888 | 0.1306 |
| 30.0000 | 10.0343 | 0.0884 |
| 35.0000 | 10.3741 | 0.0480 |
| 40.0000 | 10.5025 | 0.0008 |
| 45.0000 | 10.3712 | -0.0524 |
| 50.0000 | 9.9611 | -0.1119 |
| 55.0000 | 9.2826 | -0.1578 |
| 60.0000 | 8.3987 | -0.1915 |
| 65.0000 | 7.3699 | -0.2198 |
| 70.0000 | 6.2327 | -0.2360 |
| 75.0000 | 5.0378 | -0.2428 |
| 80.0000 | 3.8169 | -0.2435 |
| 85.0000 | 2.6187 | -0.2339 |
| 90.0000 | 1.5058 | -0.2083 |
| 95.0000 | 0.5651 | -0.1630 |
| 100.0000 | 0.0000 | -0.0069 |
| L.E. radius = 2.210 percent chord | ||
| NACA 65A006 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.4774 | 0.4397 |
| 0.7500 | 0.5760 | 0.3507 |
| 1.2500 | 0.7273 | 0.2663 |
| 2.5000 | 0.9895 | 0.1675 |
| 5.0000 | 1.3199 | 0.1156 |
| 7.5000 | 1.5960 | 0.1025 |
| 10.0000 | 1.8282 | 0.0852 |
| 15.0000 | 2.1965 | 0.0636 |
| 20.0000 | 2.4756 | 0.0484 |
| 25.0000 | 2.6871 | 0.0362 |
| 30.0000 | 2.8414 | 0.0259 |
| 35.0000 | 2.9439 | 0.0157 |
| 40.0000 | 2.9949 | 0.0049 |
| 45.0000 | 2.9908 | -0.0064 |
| 50.0000 | 2.9247 | -0.0196 |
| 55.0000 | 2.7930 | -0.0326 |
| 60.0000 | 2.6015 | -0.0437 |
| 65.0000 | 2.3632 | -0.0519 |
| 70.0000 | 2.0858 | -0.0591 |
| 75.0000 | 1.7753 | -0.0651 |
| 80.0000 | 1.4390 | -0.0692 |
| 85.0000 | 1.0856 | -0.0713 |
| 90.0000 | 0.7309 | -0.0720 |
| 95.0000 | 0.3691 | -0.0677 |
| 100.0000 | 0.0091 | -0.8448 |
| L.E. radius = 0.253 percent chord | ||
| NACA 65A008 | ||
|---|---|---|
|
(Stations and ordinates given in per cent of airfoil chord) | ||
| x | y | dy/dx |
| 0.0000 | 0.0000 | 0.0000 |
| 0.5000 | 0.6311 | 0.5814 |