Mover Creator Standard Airfoil Templates

Mover Creator provides a set of predefined standard airfoil templates that can be used for any Surfaces (fixed or controlled) defined in the Geometry page.

	BAC 300 series Used for the wing of the E-HJ-41A-1 max thickness 9% at 40% chord max camber 1.8% at 30% chord 12.0 deg -8.0 deg 1.20 -0.51 0.185 0.01065 -0.02814
	BAC 400 series Used for the wing of the P-MJ-21A-1 max thickness 12.5% at 29.7% chord max camber 0.8% at 10% chord 15.75 deg -15.75 deg 1.56 -1.287 0.130 0.0063 -0.0088
	NACA 0008 Not currently used in any vehicle template max thickness 8% at 30% chord max camber 0% at 0% chord 11.5 deg -11.5 deg 1.1 -1.1 0.0 0.004 0.0
	NACA 0012 Used for fins on all Weapon templates max thickness 12% at 30% chord max camber 0% at 0% chord 15.5 deg -15.5 deg 1.37 -1.37 0.0 0.0053 0.0
	NACA 6716 Used for the wing of the A-M4-22A-1 max thickness 16% at 30% chord max camber 6% at 70% chord 19.0 deg -15.0 deg 1.83 -0.61 0.906 0.0075 -0.254
	NACA 63A409 Used for the wing of the R-MJ-11A-1 max thickness 8.7% at 35.5% chord max camber 2.8% at 52.5% chord 13.0 deg -9 deg 1.365 -0.442 0.365 0.0047 -0.0825
	NACA 64(1)-012 Used for all non-wing surfaces for Aircraft templates max thickness 12% at 40% chord max camber 0% at 0% chord 13.0 deg -13.0 deg 1.15 -1.15 0.0 0.0054 0.0
	NACA 64-206 Used for the wings of all Fighter and Drone templates max thickness 6% at 40% chord max camber 1.1% at 50% chord 7.75 deg -7.75 deg 0.8275 -0.527 0.145 0.0037 -0.042
	NACA 63(3)-218 Used for the wing of the B-H3-81A-1 template max thickness 18% at 34% chord max camber 1.1% at 25% chord 19.0 deg -18.5 deg 1.35 -1.16 0.15 0.0074 -0.0346
	NACA 65(3)-018 Used for the wing of the B-H1-80W-1 and B-H4-40W-1 templates max thickness 18% at 40% chord max camber 0% at 0% chord 18.0 deg -18.0 deg 1.14 -1.14 0.0 0.0068 0.0
	NASA SC(2)-0412 Used for the wing of the K-MJ-21A-1 and C-HJ-41A-1 templates max thickness 12% at 37% chord max camber 1.3% at 83% chord 15.5 deg -16.5 deg 1.6412 -1.3565 0.255 0.006 -0.08