FAR-APP-2.cfg

@PART[straightslat]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.351
		MidChordSweep = 0
		maxdeflect = 45
		b_2 = 1.828
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = straight
	}
}

@PART[spoilerflap]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.478
		MidChordSweep = 0
		maxdeflect = 45
		b_2 = 3.53
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = surface
	}
}

@PART[kruegerflap]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.326
		MidChordSweep = 0
		maxdeflect = 30
		b_2 = 1.66
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = flap
	}
}

@PART[doublefowlerflap]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.9
		MidChordSweep = 0
		maxdeflect = 30
		b_2 = 3.51
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = slata
	}
	MODULE
	{
		name = FARControllableSurface
		MAC = 0.47
		MidChordSweep = 0
		maxdeflect = 30
		b_2 = 3.51
		TaperRatio = 1
		ctrlSurfFrac = 1
        transformName = slatb
	}
}

@PART[migwing]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 1.706
		MidChordSweep = 50
		maxdeflect = 25
		b_2 = 2.08
		TaperRatio = 0.196
		ctrlSurfFrac = 0.155
        transformName = obj_ctrlSrf
	}
}

@PART[warhawkfin]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARControllableSurface
		MAC = 2.19
		MidChordSweep = 30
		maxdeflect = 20
		b_2 = 2.45
		TaperRatio = 0.43
		ctrlSurfFrac = 0.465
        transformName = obj_ctrlSrf
	}
}

@PART[wing4]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 1.06
		MidChordSweep = 14
		b_2 = 1.9
		TaperRatio = 0.64
		nonSideAttach = 0
	}
}

@PART[wingtip]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.9
		MidChordSweep = -15
		b_2 = 0.51
		TaperRatio = 0.15
		nonSideAttach = 0
	}
}

@PART[hanglel]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.26
		MidChordSweep = 3.5
		b_2 = 1.89
		TaperRatio = 0.54
		nonSideAttach = 1
	}
}

@PART[hangles]:NEEDS[FerramAerospaceResearch] // redo
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.27
		MidChordSweep = 9
		b_2 = 0.93
		TaperRatio = 0.54
		nonSideAttach = 1
	}
}

@PART[vanglel]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.12
		MidChordSweep = 4.3
		b_2 = 0.94
		TaperRatio = 0.44
		nonSideAttach = 1
	}
}

@PART[vangles]:NEEDS[FerramAerospaceResearch]
{
	@module = Part
	@maximum_drag = 0
	@minimum_drag = 0
	@angularDrag = 0
	@dragCoeff = 0
	@deflectionLiftCoeff = 0
    !MODULE[ModuleLiftingSurface] {}
	MODULE
	{
		name = FARWingAerodynamicModel
		MAC = 0.10
		MidChordSweep = 4
		b_2 = 0.47
		TaperRatio = 0.59
		nonSideAttach = 1
	}
}