The present invention “Aircraft Wing with Tiplet” reflects a wing with two distinct sections including inner section for maximized lift production with long chords, high taper, and ultra-thin airfoils for substantial profile drag reduction, as well as a “tiplet” section with minimized area and maximized span to minimize aspect ratio penalty from the standpoint of increased induced drag mitigation due to large inner section lifting area. Long chords and large area of inner section are feasible from the standpoint of flight safety with the application of airfoils with forward center of pressure that provide for dynamic stability of aircraft in flight.