
DAVID C
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Its wind speed over the wing, and is goverened by Bernoulli's principle - states that in an ideal fluid (low speed air is a good approximation), with no work being performed on the fluid, an increase in velocity occurs simultaneously with decrease in pressure or gravitational energy. This principle is a simplification of Bernoulli's equation, which states that the sum of all forms of energy in a fluid flowing along an enclosed path (a streamline) is the same at any two points in that path. It is named after the Dutch/Swiss mathematician/scientist Daniel Bernoulli
So in English, a simple explanation would be that the wing is larger on the upper surfce, than it is on the lower one. thus when the air flow hits it, it is divided. This causes a pressure differential above and below a wing. the one under the wing is greater, and pushes the wing up.
However, this explanation often uses 'false' information, such as the incorrect assumption that the two parcels of air which separate at the leading edge of a wing must meet again at the trailing edge, and the assumption that it is the difference in air speed that causes the changes in pressure.
In air (or comparably in any fluid), lift is created as flow interacts with an airfoil or other body and is deflected downward. The plane on the runway, has a wing that is angled downward. The propeller, or jet moves the plane forward, thus the force created by this deflection of the air creates an equal and opposite upward force according to Newton's third law of motion. The deflection of airflow downward during the creation of lift is known as downwash.
It is important to note that the acceleration of the air does not just involve the air molecules "bouncing off" the lower surface of the wing. Rather, air molecules closely follow both the top and bottom surfaces, and so the airflow is deflected downward. The acceleration of the air during the creation of lift has also been described as a "turning" of the airflow.
this is enough to lift the weight of the plane, and allow it to accelerate to 50-70 mph. the wing thus takes on its flying profile, but on large passenger jets, additional truning is created by Flaps, which extend out of the wing, and cause huge downwash.
The Helmholtz theorem states that circulation is conserved; put simply this is conservation of the air's angular momentum. When an aircraft is at rest, there is no circulation. As the flow speed increases (that is, the aircraft accelerates in the air-body-fixed frame), a vortex, called the starting vortex, forms at the trailing edge of the airfoil, due to viscous effects in the boundary layer. Eventually the vortex detaches from the airfoil and gets swept away from it rearward. The circulation in the starting vortex is equal in magnitude and opposite in direction to the circulation around the airfoil. Theoretically, the starting vortex remains connected to the vortex bound in the airfoil, through the wing-tip vortices, forming a closed circuit. In reality, the starting vortex is dissipated by a number of effects, as are the wing-tip vortices far behind the aircraft. However, the net circulation in "the world" is still zero as the circulation from the vortices is transferred to the surroundings as they dissipate.
The aircraft starts to fly at the point that this vortex breaks from the wing. The large jet then lifts the flaps back into the wing, thus reducing the lift of the wing, but also reducing the drag, so the plane can speed up, to compensate the loss of wing area.
The circulation of a big wing is so much during take-off, that light aircraft can not take off after a large jet has done so. |