Technical Characteristics of a Glider - Assignment Example

The glider fuselage has a rounded nose and is sleek thus allowing an 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 the 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 a planform exhibiting a high aspect ratio and variable and tapered aerofoil shape. The wing allows for a straight model of sweeping by entailing wing motion through the right angles to the anticipated line of flight.

The selection of the type of glider wing focuses on allowing for low-speed design. The wings provide essential lift force and therefore the most imperative lift-producing element of the glider (Yechout & Morris, 2003). The four spars mainly provide 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 the 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 them.

The empennage has a 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 include the vertical stabilizer otherwise called the fin on which the rudder is normally attached. There is another segment called the 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 glider. The attached rudder and elevators permit the pilot to amply manage and control the yawing and pitching motions of the glider (Yechout & Morris, 2003). The provided wings have further attached rear sections adjacent to the fuselage commonly called flaps. The entailing of the flaps facilitates the deployment of downward while takeoff and landing thus increasing the quantity of force derived. At some point, a front segment of the wing will deflect.