DESIGN AND ANALYSIS OF WING OF AN ULTRALIGHT AIRCRAFT

This paper deals with the structural design and analysis of high wing of an ultralight aircraft. The wing design involves its initial considerations like planform selection, location to the aircraft and the structural design involves the design calculations for the selection of airfoil, area of the wing, wing loading characteristics and weight of the wing. The design is done corresponding to the calculated values with the help of designing software ANSYS FLUENT.