354944ced54ac838377c5c60e20439b26cf692cd,trunk/SUAVE/Methods/Aerodynamics/AVL/create_avl_datastructure.py,,populate_wing_sections,#Any#Any#,158

Before Change

                        
                if avl_wing.vertical:
                        temp                  = tip_section.origin[2]
                        tip_section.origin[2] = tip_section.origin[1]
                        tip_section.origin[1] = temp

                avl_wing.append_section(root_section)
                avl_wing.append_section(tip_section)

After Change

             
                // assign location of wing tip         
                if avl_wing.vertical:
                        tip_section.origin    = [origin[0]+semispan*np.tan(sweep),origin[1]+semispan*np.tan(dihedral),origin[1]+semispan]
                else: 
                        tip_section.origin    = [origin[0]+semispan*np.tan(sweep),origin[1]+semispan,origin[2]+semispan*np.tan(dihedral)]
                

Instances