They're usually attached to the fuselage by strong bolts. These bolts are normally hidden from view - and accessed by a small panel.
A fixed-wing aircraft is an aircraft which has wings that are attached to the aircraft and do not move. The term is used to differentiate airplanes from other types of flying vehicles such as lifting-body aircraft (balloons and blimps) or rotary aircraft such as helicopters and auto gyros. All airplanes are considered fixed-wing aircraft and even swing-wing or otherwise moving-wing airplanes are usually referred to as being in the fixed-wing category of aircraft.
>No it cannot fly with one wing. UNLESS the aircraft's body actually produces sufficient lift, such as a "flying wing" aircraft
the angle at which an aircraft's wing is set back from a right angle to the body
In regards to weight, since the wing is the main lifting body, heavier aircraft will require a larger wing with greater wing area. In regards to speed, a larger wing will of course produce more aerodynamic drag which tends to slow the aircraft down. Obviously large heavy aircraft must have a correspondingly large amount of thrust to overcome this.
AUTOROTATION is only for Rotary Wing aircraft...not fixed wing
Approximately 37 US fixed-wing aircraft and 23 rotor-wing aircraft were lost during DS. Approximately 15 of those fixed-wing aircraft & 18 of the rotor-wing aircraft were lost to operational causes (accidents).
A BWB (Blended wing body) aircraft is where the fuselage and the wings blend seamlessly into each other, and you cant really tell where the fuse. ends and the wing starts. A brilliant example is the B-2.
The central body is called the fuselage. http://en.wikipedia.org/wiki/Fuselage
The wing spar on this aircraft is one solid assembly tip to wing tip so it is an integral part of the fuselage. This aircraft is not the usual kingair wingbolt bathtub fitting holding the wing on.
An aircraft wing that is angled back.
Ailerons are hinged control surfaces attached to the trailing edge of the wing of a fixed-wing aircraft. The ailerons are used to control the aircraft in roll. The two ailerons are typically interconnected so that one goes down when the other goes up: the downgoing aileron increases the lift on its wing while the upgoing aileron reduces the lift on the other wing, producing a rolling moment about the aircraft's longitudinal axis. The word aileron is French for "little wing." The ailerons are control via the control column inside an aircraft's cockpit. If the control column is turned right, for example, then the right wing aileron will move upwards and the right wing will move downwards and the left wing aileron will move downwards and the left wing will lift, and the aircraft will roll right. On the tail of a fixed wing aircraft, the rudder is also used to conter-act the unwanted yaw, and is controlled by the foot pedals inside the cockpit. When the aircraft is rolled right using the ailerons, the rudder is turned right to help the aircraft begin its turn. The parts that help to bank the airplane are called the ailerons (on the wing next to the 'flaps') and the rudder (on the tail under the 'elevators').
Approximately 2,000 fixed wing aircraft were lost; approximately 5,000 rotary-wing aircraft were lost.