Naca airfoil data pdf

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. Airfoil database search naca 4 digit search the 1636 airfoils available in the databases filtering by name, thickness and camber. There are many sources of airfoil data or the sections can be generated using tools. 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. Summary of lowspeed airfoil data uiuc applied aerodynamics. Naca 65series 10percentthick airfoil sections, for which cascade data were available. Naca 4 digit airfoil database search airfoil tools. Max camber 2% at 40% chord source uiuc airfoil coordinates database source dat file. Naca airfoil database pdf naca airfoil database pdf naca airfoil.

Paste the dat file data into a form and the airfoil will be available to use in the drop down menus. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of reynolds numbers. 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. Computer program to obtain ordinates for naca airfoils. Recent airfoil data for both flight and windtunnel tests hare. A more complete discussion of porouswall cascades can be found in. The naca 0012 airfoil was one of the earliest airfoils created. Summary of lowspeed airfoil data is only the first in what should be a series of volumes that. Parser naca2412 il naca 2412 naca 2412 airfoil max thickness 12% at 30% chord. Theory of wing sections including a summary of airfoil data. The characteristics of 78 related airfoil sections from tests. 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. Symmetric airfoils in the 4digitseries family are designated by a 4digit number of the form naca 00xx.