Definition of Cutting Planes for JSM case, Version 2 (Preliminary)

Note that the pressure taps on the model's wing are aligned on all 3 elements
only when the configuration is stowed (however, note that G-G on the flap is not
aligned even when stowed).  When in the deployed position, you must make a
separate "cut" on each of the elements according to the following formula
(for each of the 7 span stations):

		AX + BY + CZ = D			

	Section	A       	B       	C	        D
Main-wing					
	A-A	0.000000 	-0.998630 	0.052336 	359.90289 
	B-B	0.000000 	-0.998630 	0.052336 	555.75009 
	C-C	0.000000 	-0.998630 	0.052336 	751.66612 
	D-D	0.000000 	-0.998630 	0.052336 	927.25733 
	E-E	0.000000 	-0.998630 	0.052336 	1281.26013 
	G-G	0.000000 	-0.998630 	0.052336 	1764.85985 
	H-H	0.000000 	-0.998630 	0.052336 	2041.23862 
Slat (Ds=25)					
	A-A	0.041617 	-0.979370 	-0.197741 	487.65615 
	B-B	0.041617 	-0.979370 	-0.197741 	683.50335 
	D-D	0.055020 	-0.976978 	-0.206122 	1083.27700 
	E-E	0.055020 	-0.976978 	-0.206122 	1437.27981 
	G-G	0.055020 	-0.976978 	-0.206122 	1920.87952 
	H-H	0.055020 	-0.976978 	-0.206122 	2197.25829 
Flap (Df=30)					
	A-A	0.022513 	0.997400 	-0.068458 	-296.75275 
	B-B	0.022513 	0.997400 	-0.068458 	-492.59995 
	C-C	0.022513 	0.997400 	-0.068458 	-688.51598 
	D-D	0.029388 	-0.956670 	0.289688 	941.18126 
	E-E	0.029388 	-0.956670 	0.289688 	1295.18406 
	G-G	0.029388 	-0.956670 	0.289688 	1758.78378 


* Note: the planes for the main wing were also slightly inclined due to the
dihedral angle of the wing (nearly 3 deg).  This is why the cuts for the main
wing are not at perfectly y=constant planes.