public interface Aero3DOF
Modified by: Joseph A. Huwaldt
Modifier and Type | Method and Description |
---|---|
float |
getCA()
Method that returns the body axis axial force coefficient.
|
float |
getCD()
Method that returns the wind axis drag coefficient.
|
float |
getCL()
Returns the wind axis lift coefficient.
|
float |
getCM()
Method that returns the wind axis pitching moment coefficient.
|
float |
getCMb()
Method that returns the body axis pitching moment coefficient.
|
float |
getCN()
Returns the body axis normal force coefficient.
|
void |
setAOA(float AOA)
Method that sets the angle of attack in degrees.
|
void |
setHOB(float hob)
Sets the height above ground level (for ground effect modeling).
|
void |
setMach(float Mach)
Method that sets the Mach number.
|
void setAOA(float AOA)
AOA
- Angle of attack in degrees.void setMach(float Mach)
Mach
- The Mach number.void setHOB(float hob)
hob
- The height to the aero reference point divided by the reference span "bref".float getCL()
float getCD()
float getCM()
float getCN()
float getCA()
float getCMb()