NACA_AIRFOIL_DATA Struct Reference

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.

Member Data Documentation

ireflex

int NACA_AIRFOIL_DATA::ireflex

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

Definition at line 53 of file naca.h.

iTE0

int NACA_AIRFOIL_DATA::iTE0

trailing edge flag, 1 - TE thickness equal to zero

Definition at line 54 of file naca.h.

Referenced by NACA_PROFILE::setTE0().

k1

double NACA_AIRFOIL_DATA::k1

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

Definition at line 51 of file naca.h.

maxor

double NACA_AIRFOIL_DATA::maxor

the maximum camber

Definition at line 48 of file naca.h.

Referenced by NACA_PROFILE::generate_naca().

name

const char* NACA_AIRFOIL_DATA::name

4- or 5-digit airfoil code

Definition at line 47 of file naca.h.

Referenced by NACA_PROFILE::generate_naca().

posmax

double NACA_AIRFOIL_DATA::posmax

the location of maximum camber

Definition at line 49 of file naca.h.

Referenced by NACA_PROFILE::generate_naca().

serie

enum series NACA_AIRFOIL_DATA::serie

type of serie - 4- or 5-digit

Definition at line 52 of file naca.h.

Referenced by NACA_PROFILE::generate_naca().

thmax

double NACA_AIRFOIL_DATA::thmax

the maximum thickness

Definition at line 50 of file naca.h.

Referenced by NACA_PROFILE::generate_naca().

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

• naca.h