aircraftFuelConsumptionModel.h File Reference

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Classes
class	DtAircraftFuelConsumptionModel
	Implements the Breguet range equation V(L/D) Range = ---—*ln(Wi/Wf) g*SFC V = Velocity L/D = Lift/Drag ratio (aerodynamic efficiency) SFC = Specific fuel consumption (engine efficiency) Wi = initial weight Wf = final weight. More...
class	DtNoFuelUsageAircraftFuelConsumptionModel
	Uses no fuel. More...
class	DtConstantAircraftFuelConsumptionModel
	Uses a single efficiency number (i.e. doesn't do any interpolation). More...
class	DtBilinearInterpolationAircraftFuelConsumptionModel
	Uses bilinear interpolation to interpolate an efficiency. More...