jburkardt

NACA\ NACA Airfoils {#naca-naca-airfoils align=”center”} =============


NACA is a C++ library which can take the parameters of certain NACA airfoils and return the coordinates of a sequence of points that outline the wing shape. The data can be displayed with gnuplot.

Licensing: {#licensing align=”center”}

The computer code and data files described and made available on this web page are distributed under the GNU LGPL license.

Languages: {#languages align=”center”}

NACA is available in a C version and a C++ version and a FORTRAN77 version and a FORTRAN90 version and a MATLAB version.

GNUPLOT, C++ programs which illustrate how a program can write data and command files so that gnuplot can create plots of the program results.

Reference: {#reference align=”center”}

  1. Eastman Jacobs, Kenneth Ward, Robert Pinkerton,\ “The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel”,\ NACA Report 460, 1933.

Source Code: {#source-code align=”center”}

Examples and Tests: {#examples-and-tests align=”center”}

List of Routines: {#list-of-routines align=”center”}

You can go up one level to the C++ source codes.


Last revised on 22 May 2014.