Structure for storing the low speed aero data.
#include <sc_aero.h>
|
|
double | length |
| | The characteristic length.
|
| |
|
double | oswaldEff |
| | The Oswald efficiency factor.
|
| |
|
double | aspectRatio |
| | The wing aspect ratio.
|
| |
|
double | thickness |
| | The thickness ratio.
|
| |
|
double | s |
| | The surface area.
|
| |
|
double | zetaTrans |
| | The transonic transition factor.
|
| |
|
double | cP |
| | The parasitic drag coefficient.
|
| |
|
double | alpha0 |
| | Zero lift angle.
|
| |
|
ml_matrix | axis |
| | Axis of rotation.
|
| |
|
ml_matrix | r_surf |
| | Location of hinge.
|
| |
|
ml_matrix | q_body_to_hinge |
| | q body to hinge axis
|
| |
