A struct containing airfoil data. More...

#include <naca.h>

Public Attributes
const char *	name
	4- or 5-digit airfoil code

double	maxor
	the maximum camber

double	posmax
	the location of maximum camber

double	thmax
	the maximum thickness

double	k1
	constant to determine the desired lift coefficient (5-digit serie)

enum series	serie
	type of serie - 4- or 5-digit

int	ireflex
	reflex flag - if ireflex = 1, Cm should be close to 0 (5-digit serie)

int	iTE0
	trailing edge flag, 1 - TE thickness equal to zero

Detailed Description

A struct containing airfoil data.

Definition at line 45 of file naca.h.

The documentation for this struct was generated from the following file:

Public Attributes