67 void SetName(
const char *FileName );
69 int Read(
const char *FileName );
73 int Write(
const char *FileName );
Simple I/O functions class.
Simple output file of Press program: reference values, aerodynamic coefficients, flow parameters.
double B
reference wingspan
double Cxi
induced drag coefficient
int Read(void)
reads the [.sdsa] file defined by SetName function
double Z
Z coordinate fo the origin for moment components.
double Cls
rolling moment coefficient (stability axis system)
void Clean(void)
cleans local variables
double Cxs
drag coefficient (stability axis system - pressure component)
double Cx
drag coefficient (body axis system - pressure component)
double Cl
rolling moment coefficient (body axis system)
double Czi
lift coefficients that relates to induced drag
double Cys
sideforce coefficient (stability axis system)
double X
X coordinate fo the origin for moment components.
double Cns
yawing moment coefficient (stability axis system)
double Beta
sideslip angle [deg]
double Cz
lift coefficient (body axis system)
double Cn
yawing moment coefficient (body axis system)
void SetName(const char *FileName)
set pathname for the [.sdsa] file
double P
roll rate [rad/s]
double Cms
pitching moment coefficient (stability axis system)
double MAC
mean aerodynamic chord
double Q
pitch rate [rad/s]
double Cm
pitching moment coefficient (body axis system)
double Cy
sideforce coefficient (body axis system)
double Czs
lift coefficient (stability axis system)
double Alfa
angle of attack [deg]
int Write(void)
writes the [.sdsa] file defined by SetName function
This file contains some smart I/O functions.