DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
-#define ID_PROPELLER "$Id: FGPropeller.h,v 1.19 2011/09/24 14:26:46 jentron Exp $"
+#define ID_PROPELLER "$Id: FGPropeller.h,v 1.20 2011/10/31 14:54:41 bcoconni Exp $"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FORWARD DECLARATIONS
<li>Various NACA Technical Notes and Reports</li>
</ul>
@author Jon S. Berndt
- @version $Id: FGPropeller.h,v 1.19 2011/09/24 14:26:46 jentron Exp $
+ @version $Id: FGPropeller.h,v 1.20 2011/10/31 14:54:41 bcoconni Exp $
@see FGEngine
@see FGThruster
*/
void SetEngineRPM(double rpm) {RPM = rpm/GearRatio;}
/// Returns true of this propeller is variable pitch
- bool IsVPitch(void) {return MaxPitch != MinPitch;}
+ bool IsVPitch(void) const {return MaxPitch != MinPitch;}
/** This commands the pitch of the blade to change to the value supplied.
This call is meant to be issued either from the cockpit or by the flight
void SetSense(double s) { Sense = s;}
/// Retrieves the pitch of the propeller in degrees.
- double GetPitch(void) { return Pitch; }
+ double GetPitch(void) const { return Pitch; }
/// Retrieves the RPMs of the propeller
- double GetRPM(void) const { return RPM; }
+ double GetRPM(void) const { return RPM; }
/// Calculates the RPMs of the engine based on gear ratio
- double GetEngineRPM(void) const { return RPM * GearRatio; }
+ double GetEngineRPM(void) const { return RPM * GearRatio; }
/// Retrieves the propeller moment of inertia
- double GetIxx(void) { return Ixx; }
+ double GetIxx(void) const { return Ixx; }
/// Retrieves the coefficient of thrust multiplier
- double GetCtFactor(void) { return CtFactor; }
+ double GetCtFactor(void) const { return CtFactor; }
/// Retrieves the coefficient of power multiplier
- double GetCpFactor(void) { return CpFactor; }
+ double GetCpFactor(void) const { return CpFactor; }
/// Retrieves the propeller diameter
- double GetDiameter(void) { return Diameter; }
+ double GetDiameter(void) const { return Diameter; }
/// Retrieves propeller thrust table
FGTable* GetCThrustTable(void) const { return cThrust;}
FGTable* GetCpMachTable(void) const { return CpMach; }
/// Retrieves the Torque in foot-pounds (Don't you love the English system?)
- double GetTorque(void) { return vTorque(eX); }
+ double GetTorque(void) const { return vTorque(eX); }
/** Retrieves the power required (or "absorbed") by the propeller -
i.e. the power required to keep spinning the propeller at the current
would be slowed.
@return the thrust in pounds */
double Calculate(double EnginePower);
- FGColumnVector3 GetPFactor(void);
- string GetThrusterLabels(int id, string delimeter);
- string GetThrusterValues(int id, string delimeter);
+ FGColumnVector3 GetPFactor(void) const;
+ string GetThrusterLabels(int id, const string& delimeter);
+ string GetThrusterValues(int id, const string& delimeter);
void SetReverseCoef (double c) { Reverse_coef = c; }
- double GetReverseCoef (void) { return Reverse_coef; }
+ double GetReverseCoef (void) const { return Reverse_coef; }
void SetReverse (bool r) { Reversed = r; }
- bool GetReverse (void) { return Reversed; }
+ bool GetReverse (void) const { return Reversed; }
void SetFeather (bool f) { Feathered = f; }
- bool GetFeather (void) { return Feathered; }
+ bool GetFeather (void) const { return Feathered; }
double GetThrustCoefficient(void) const {return ThrustCoeff;}
double GetHelicalTipMach(void) const {return HelicalTipMach;}
int GetConstantSpeed(void) const {return ConstantSpeed;}