How Does the Aircraft Wing Work and What Components Are on the Wing - Literature review Example

Name Instructor Course Date: Air Craft Wings Several critical components that enable the plane to fly are the wings. The document indicates the great feasibility of the wings and how the design, materials, and manufacturing are making a change in the operation of the aircraft. To make a scientific research, I referred to some trustworthy resources to consolidate my point. My references include a book ( Aviation and Climate Change), a web article (How wings work), and Journal (UK Vehicle technology ). Dr. Ruth Mallors and Dr. Mike Hicks wrote the journal giving the views of specialists in aerospace and defence technology. Work of Dr. Ruth Mallors and Dr. Mike Hicks has the concept of wing development set right. There was a combination. It involved simple and the practical approaches. The purpose was to demonstrate the crucial importance of the wings for any aircraft displayed in the great attention paid in their manufacturing. The wing design according to them differs from one manufacturer to another specifically in connecting the fuselage wall to separate sides through a central wing box. The upper part of the wings of a plane primarily undergoes compression, so the materials used are of aluminium alloys which resistant to compression and have good stability. Also, the lower part of the wings are also subject to high pressure and fatigue, so the materials chosen are also of aluminium alloys that are themselves more tolerant to fatigue and damage than the upper part. The rest of the wings made of composite materials occur. Wings in modern aircrafts such as the A 350 and the A 380 made of composite materials such as the fibreglass, and this makes the aircraft lighter exist. Therefore, there is less fuel consumption. Professor Holger Babinsky attached to the University of Cambridge contradicts the renowned explanation of the way wings work. The professor develops a plan to change many concepts used today. The old report says that a wing lift occurs because the flow of the air on the wings travels for a longer distance if the surface is curved rather than flat. He filmed an experiment showing of smoke floating around an aerofoil and after pausing the video, he reached a surprising conclusion that the curved shape that creates lift, not the distance. The wing is a bearing surface. The goal is to get a particular lift or force that makes possible for objects that are heavier than air such as aircrafts to fly. The discovery of Prof. Babinsky is going to make the manufacturers focus on the shape of the wings of their planes more than ever. Thirdly, in their book “Aviation and Climate Change», Stephan Gossling and Paul Upham show the impact of the design and the materials used to manufacture wings on the environment. According to them, the tendency of building jumbo aircrafts leads to an increase in weight and thus more fuel consumption and thus more gas emission in the air. In reducing consumption, high aspect ratio wings undergo manufacturing. There is also fuselage and wing combination in a configuration called “Blended Wing Body." The configuration has new materials like composites that make this aircraft like the A380 much lighter than a similar Jumbo jet and thus less gas emission. (p.297). The engines of the aircraft alone are not enough to make you take off, but it is the wings that we have to thank. The engines in the arms forward the aircraft at high speed but do not fall on the ground. Here comes the role of the arms that are essential for the planes to fly and maintain or change altitude. The wings of most commercial aircraft hold fuel tanks and their outer sections include many devices such as the fixed D-nose, air-brakes spoilers, and the flaps that are crucial for the lifting operation. Without the wings, there will be no flights from one place to another (Holger, 2009). To sum up, the resources consulted demonstrate that the wing is a major constituent of the aircraft body that enable it to fly, maintain altitude and do many other maneuvers. The manufacturers are working on developing the wings in a matter of the material used, and the shape to meet the weight loss requirement and, therefore, reduce fuel consumption and thus gas emission in the atmosphere. The process of improving the wings never ends (Holger, 2009). There are indeed several part of aircraft wings. The parts work hand in hand in order to allow the active movement to f the plane from one point to another. The Adaptive Compliant Trailing Edge (ACTE) helped in understanding several of these components of the aircraft wings. The aileron commonly known as the little side has a hinge connected to the edge of the wings. The purpose of the aileron is to overcome the situation in which the aircraft is in roll (the moving of the airplane about the longer axis). Once the plane is in the roll, and there are no a pair of ailerons, the result is that the there is a deviation of the plane from the original path of flight. The meaning would be that the plane will head straight to another direction. The change, of course, is due to tilting of vectors associated with the lift. Banking, also known as rolling is the movement of the plane about the longitudinal axis. Matthew Piers patented the aileron in 1868 as he was the inventor. In the present day, the components (ailerons) have certain complicated and unique designs depending on the existence of the aircraft (Ferguson, 1984). Another part of the aircraft wing acts as the high lift device. The method commonly known as the circulation control side (CCW) has the role of increasing the coefficient of lift. The element had six years of development in the past and started out as blown flaps. The increase of the coefficient of lift is over the leading and trailing edge. The increase is possible through using a number of slots into which air blows so that they give off a high pressure of the air jet. The addition increase of the speed of the flow of air will in turn increase the force for lift by the use of stated airfoil production of lift. The primary objective of the element is to help in the increase of the force of lifting of the entire aircraft in the situations when huge lifting power at a low-velocity matter. These situations are takeoff accompanied with landing. However, other flaps and slats help when the plane is going to land down and takes off as for large jets. The components have a high value for drag. The added advantage of this tool is that no other drug matters while increasing the coefficient of lift. However, other engineers have a reason that they increase the ratio of landing. The reduction in speed is by a percentage of 150% to 250%. The droop also called the droop nose is a certain kind of device for high – lift located on the wing of several aircrafts. The role of the droop resembles that of the slats, but the only dissimilarity is the whole operation of the leading edge is downwards. That of the slat deviates away from the edge of the main wing once in operation. It is a part of the aircraft wing that works with devices of high – lift while chasing the speed of the slanting part of the given side and at the same time reducing the speed of installation. For example, the drops of the Airbus A380 have an application (Ferguson, 1984). Flaps help in alteration of features of the wing, and there is lifting of the edges of the wings of a fixed to reduce speed at which aircraft runs. The whole objective of the tool is to increase the amount of the descent of the landing. The elements reduce the amount of time for takeoff and landing. The ability of the flaps to do so is by getting the speed of stall to a lower level and later increase drag. The ability to increase the curvature will increase the minimum coefficient of lift generate the lift. The increase of drug is by the extended flaps that are helpful when it comes to landing. The reason is that the aircraft slows down. Individual aircraft has a functional effect on the deployment of the flap. There is a decrease of the pitch of the aircraft by lowering the nose of the improvement of the view of the pilot. The problem is that flaps lead to pitch ups given the type and position of the wing. There are various folds with a particular choice given different amounts, velocity, and the degree of operation of the aircraft. There are several types of flaps are Fowler, Plain, Slotted brands (Ferguson, 1984). The spoiler is another element that has the sole purpose of reducing the lift of the aircraft. The spoilers are plates in the top position of the wing. They can have an extension upwards into the area of the flat of the air. The meaning of this is that the spoiler makes a stall at the behind position of the wing. In doing so, the lift undergoes reduction for that particular part of the side. There are several types of spoilers. There are some placed at the desired angles as the flight occurs for the sole purpose of increasing descent time. There are others set during the time of landing to decrease the lift. There are air breaks whose sole purpose is to increase the drag while not affecting the lift. The spoilers reduce the lift (Ferguson, 1984). Works Cited Civil Aircraft For Leisure, Business And Freight. "UK Air Vehicle Technology." Ed. Ruth Mallors and Mike Hicks. Aerospace & DefenceAbstract (n.d.): n. pag. Web. Ferguson, Robert A. Law and Letters in American Culture. Cambridge, MA: Harvard U, 1984. Print. Gössling, Stefan, and Paul Upham. Climate Change and Aviation: Issues, Challenges and Solutions. London: Earthscan, 2009. Web. "How Wings Really Work." University of Cambridge. N.p., n.d. Web. 23 Feb. 2015. . N.p., n.d. Web. Read More