dde9692f10bd2bd98a435c1f0209319efc9cbb8a,trunk/SUAVE/Input_Output/OpenVSP/vsp_read_wing.py,,vsp_read_wing,#Any#Any#,20

Before Change

		x_sec_1_tc_parm        = vsp.GetXSecParm(x_sec_1,"Tip_Chord")
		
		// Calcs
		sweep     = vsp.GetParmVal(x_sec_1_sweep_parm)
		sweep_loc = vsp.GetParmVal(x_sec_1_sweep_loc_parm)
		c_4_sweep = convert_sweep(sweep,sweep_loc,0.25,wing.aspect_ratio,wing.taper)		
		
		// Pull and pack
		wing.dihedral              = vsp.GetParmVal(x_sec_1_dih_parm) * Units.deg
		wing.taper                 = vsp.GetParmVal(x_sec_1_taper_parm)
		wing.chords.root           = vsp.GetParmVal(x_sec_1_rc_parm)* units_factor
		wing.chords.tip            = vsp.GetParmVal(x_sec_1_tc_parm) * units_factor	
		wing.chords.mean_geometric = wing.areas.reference / wing.spans.projected	
		wing.sweeps.quarter_chord  = c_4_sweep

	// Twists
	wing.twists.root      = vsp.GetParmVal(wing_id, "Twist", "XSec_0") * Units.deg

After Change

		x_sec_1_tc_parm        = vsp.GetXSecParm(x_sec_1,"Tip_Chord")
		
		// Calcs
		sweep     = vsp.GetParmVal(x_sec_1_sweep_parm) * Units.deg
		sweep_loc = vsp.GetParmVal(x_sec_1_sweep_loc_parm)
		taper     = vsp.GetParmVal(x_sec_1_taper_parm)
		c_4_sweep = convert_sweep(sweep,sweep_loc,0.25,wing.aspect_ratio,taper)		
		
		// Pull and pack
		wing.sweeps.quarter_chord  = c_4_sweep
		wing.taper                 = taper
		wing.dihedral              = vsp.GetParmVal(x_sec_1_dih_parm) * Units.deg - x_rot
		wing.chords.root           = vsp.GetParmVal(x_sec_1_rc_parm)* units_factor

Instances