o.name = 'wing' ;

o.CG = [ 0 0 0 ];

o.ref_point = [ 0 0 0 ];

o.wingsym = 1 ;

o.nw = 1 ;

o.apex = [ 0 0 0 ];

o.twst_piv = 0.5 ;

o.np = 1 ;

o.span =    6.03 ;

o.chord = [ 2.1430  0.8572 ];

o.twst = [ 0  3.5 ];

o.di = 0 ;

o.sw = 0 ;

o.sweep_piv = .25 ;

o.foil = { 4416  4412 };

o.nxtype = 1 ;

o.nx = 1 ;

o.nytype = 4 ;

o.ny = 10 ;

o.flap = 0 ; 
                                                                                    cd ..

										Airloads ( o )