Search results
Results From The WOW.Com Content Network
The aircraft design process is a loosely defined method used to balance many competing and demanding ... The wing of a fixed-wing aircraft provides the lift necessary ...
A tandem wing design has two wings, one behind the other: see Tailplanes and foreplanes below. Some early types had tandem stacks of multiple planes, such as the nine-wing Caproni Ca.60 flying boat with three triplane stacks in tandem. A cruciform wing is a set of four individual wings arranged in the shape of a cross. The cross may take either ...
This process can also be extended to explore single wing-body aircraft designs. Wing-body styled aircraft can scale up their cargo much easier than the traditional ‘tube and plank’ design. Airbus utilized this approach to explore design choices in future large aircraft in 2002. [5]
Washout is a characteristic of aircraft wing design which deliberately reduces the lift distribution across the span of an aircraft’s wing. The wing is designed so that the angle of incidence is greater at the wing roots and decreases across the span, becoming lowest at the wing tip .
The Junkers all-metal corrugated-covered wing / multiple tubular wing spar design format was emulated after World War I by American aviation designer William Stout for his 1920s-era Ford Trimotor airliner series, and by Russian aerospace designer Andrei Tupolev for such aircraft as his Tupolev ANT-2 of 1922, upwards in size to the then-gigantic ...
Blended wing body aircraft have a flattened and airfoil shaped body, which produces most of the lift to keep itself aloft, and distinct and separate wing structures, though the wings are smoothly blended in with the body. Thus blended wing bodied aircraft incorporate design features from both a futuristic fuselage and flying wing design.
Back in January, Boeing flew its fancy new widebody aircraft for the first time. The wings are longer than the ones on previous versions of that airplane—a design change that helps increase the ...
Angle of incidence of an airplane wing on an airplane. On fixed-wing aircraft, the angle of incidence (sometimes referred to as the mounting angle [1] or setting angle) is the angle between the chord line of the wing where the wing is mounted to the fuselage, and a reference axis along the fuselage (often the direction of minimum drag, or where applicable, the longitudinal axis).