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The glider fuselage has a rounded nose and sleek thus allowing easy flow of air can flow efficiently around it. The feature is also enhanced by the presence of the tapered body of the fuselage (Yechout & Morris, 2003).
The wing design for the glider represents intrinsic part of the glider. It has various arrangements of braces, ribs, edges and many other parts designed to strengthen the wing part of the glider. The glider wing has planform exhibiting high aspect ratio, variable and tapered aerofoil shape. The wing allows for straight model of sweeping by entailing wing motion through the right angles to anticipated line of flight.
The selection of the type of the glider wing focuses on allowing of low-speed design. The wings provide essential lift force, and therefore is most imperative lift-producing element of the glider (Yechout & Morris, 2003). The four spars mainly provide the lateral strength for the wing. Ribs are attached to the spars to complete the structural parts. There is a rising angle is called the dihedral which aids in keeping the airplane from rolling suddenly while on flight. AOI or the angle at which the wing is linked to the fuselage is mainly 5o. The wings have variable b and c features on it.
The empennage has rudder, vertical stabilizer, engine pylon, elevator and horizontal adjustable stabilizer as the main typical parts. There is well designed to provide stability and enhanced control for the glider. The main two parts entailing the empennage includes vertical stabilizer otherwise called fin on which the rudder is normally attached. There is another segment called horizontal stabilizer on which the elevators are conventionally attached.
The typical stabilizers facilitate proper pointing of the glider to the wind as normally, when the tail section of the glider swing to any side, the wind thrust against the tail sides and surfaces. This action maintains the proper place of the
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