Recent airfoil data for both flight and windtunnel tests have been collected and correlated insofar as possible. Computer program to obtain ordinates for naca airfoils. Symmetric airfoils in the 4digitseries family are designated by a 4digit number of the form naca 00xx. Enter the airfoil thickness, camber and camber postion to generate a 4 digit naca. Detail data necessary for the application of naca 6serles airfoils to wing design are presented in supplementary figures, together with recent data for the naca 24, 44, and 230series airfoils. Recent airfoil data for both flight and windtunnel tests hare. Online search of naca 4 digit airfoils aerofoil in the databases filtering by name, thickness and camber. This methodology began to change in the early 1930s with the publishing of a naca report entitled. The characteristics of 78 related airfoil sections from tests.
Theory of wing sections including a summary of airfoil data. Summary of lowspeed airfoil data uiuc applied aerodynamics. The naca airfoil series the early naca airfoil series, the 4digit, 5digit, and modified 45digit, were generated using analytical equations that describe the camber curvature of the meanline geometric centerline of the airfoil section as well as the sections thickness distribution along the length of the airfoil. New data are presented that permit the rapid calculation of the approximate pressure distributions for the older naca fourdigit. Parser naca2412 il naca 2412 naca 2412 airfoil max thickness 12% at 30% chord. Naca 65series 10percentthick airfoil sections, for which cascade data were available. A more complete discussion of porouswall cascades can be found in. There are many sources of airfoil data or the sections can be generated using tools. Recent information on the aerodynamic characteristics of.
The cascade data were obtained in porous wall cascades which closely approximate twodimensionalflow conditions by removing the boundary layer from the walls enclosing the blade row. Airfoil database search naca 4 digit search the 1636 airfoils available in the databases filtering by name, thickness and camber. Its mathematically simple shape and age have meant that it is one of the first choices for validating cfd programs, as there is a wealth of data on this particular airfoil. The naca 0012 airfoil was one of the earliest airfoils created. Max camber 2% at 40% chord source uiuc airfoil coordinates database source dat file. Summary of lowspeed airfoil data is only the first in what should be a series of volumes that. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of reynolds numbers. Though the naca 0012 airfoil is not in general use. Naca 4 digit airfoil database search airfoil tools. Search the 1636 airfoils available in the databases filtering by name, thickness and camber. Currently the airfoils are only stored in your browser session and will need to be added when the browser is reopened naca 4 digit airfoil generator.
1577 514 491 628 1605 736 1454 1604 1355 51 21 1342 1042 1059 1398 1192 1145 600 1476 241 1420 915 860 916 178 353 753 78 1548 1411 481 1609 222 228 534 951 1385 1037 1307