Apply the data ( Wing Span, Wing Platform Area, Gross Weight at takeoff, Fuel Capacity, Powerplant, Aspect Ratio etc. )of the Airbus A320 to problems 6.1, 6.2, and 6.3 attached . Additionally, generate a V-n diagram for the Airbus A320. Don''t use the data of the aircraft in the problems. Use the ones of the Airbus A320. Show your work by writing.