Flying wing or wings to fly is the term for an aircraft design that resembled a blend of two wings (Blended-Wing Body). Future aircraft design does not have a main body called the fuselage or tail like on the plane that we know at this time. This airplane is truly unique because it consists only of the wing and it was only needed wings.
Flying Wing shape resembles a boomerang, which basically is a two blade wings are combined into one unit. The design of this kind it is no stranger to design aircraft, but during this form of Blended Wing Body is only used for combat aircraft with stealth technology, which is a plane that could disappear or undetectable by radar. Flying Wing consists of only one unit has several advantages such as passenger capacity and generated a large elevator.
Design of Flying Wing in particular must consider several requirements, among others: 1. Aerodynamic requirements 2. Strength and Stiffness Requirements 3. Weight Requirements 4. Tactics of Technical Requirements 5. Operating Requirements 6. Construction Requirements
he design of the wing (Flying Wing model) must pass through stages by stages that fit in order to get maximum results. Stages in the design is the determination of initial dimensions, the mission profile and making the model structure.
Within the framework of the wing design, Safety Factor should pay attention mainly on the trunk link, spar and connecting beams. - Average Safety Factor on the plane is 1.5. In the design of UAV Wing Flying Wing aircraft was designed large enough Safety Factor for Safety Factor is designed large enough (1.77 2.37 spar and connecting rods) to be safe at the time of landing hard (Hard Landing) and the possibility of fibers of the material is less homogeneous . Safety Factor for the beam connecting large left because of what is needed is a sufficient bonding area.
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