Design and Analysis of aircraft Wing
Suraj Kumar
K L University, Green Fields, Vaddeswaram, Guntur District, A.P, INDIA, 522502 Department of Mechanical Engineering, (id no.-13007522)
Abstract:
This deals with bending Finite Element Analysis of the aircraft wing using commercial software ANSYS. An aircraft wing is made of composite with fibre angles in each ply aligned in different direction. Various air foil thickness and ply angles were considered to study the effect of bending-torsion decoupling. The laminate characteristics are usually calculated using the number of layer, stacking sequence, geometric and mechanical properties. A finite number of layers can be combined to form so many laminates. The only restriction that is imposed on the laminate as an element of composite structure concerns its total thickness which is assumed to be much smaller than the other dimensions of the structure.
Aircraft wing model as per the plan should be made in FEA and the model is subjected to various loading. The loading given by the self-weight or due to acceleration due to gravity was discussed and the deflection over here should be calculated. The wing model is severely affected by the loads on along wing direction, across wing direction, vertical direction.NACA 2412 airfoil was taken for designing wing. FLUENT was used for computational fluid dynamic analysis to determine the lift and drag for wing during zero degreed flaps and angled
Aircraft Solution is a leading company in the design and fabrication of component products and services for companies in the electronics, commercial, defense, and aerospace industry. The company is automated to increase production while reducing costs. The main goal of the Aircraft Solution is to provide users the product by low cost and the quality product. The users of the company are employees, customers, suppliers, and contractors are permitted access the company network.
This report details the process for the design of a composite laminate tube, the software package 'MathCAD' was used to determine a lamina design with a configuration that avoids mechanical failure under loading conditions. It was also used to obtain twist angles and maximum stresses for specific lamina wind up angles. The report will provide analysis of the methods used to obtain these criteria.
However, the absence of plastic deformation does not mean that composites are brittle materials like monolithic ceramics. The heterogeneous nature of composites result in complex failure mechanisms which impart toughness. Fiber-reinforced materials have been found to produce durable, reliable structural components in countless applications. The unique characteristic of composite materials, especially anisotropy, require the use of special design
The main company strategy of Aircraft Solutions is to provide low cost design and computer-aided modeling packages to customers to reduce their development operating cost. One thing AS is especially proud of is that it will help the customer through all phases of new product deployment. It will help starting from the early prototypes through final large-volume
Ever since I was little I was amazed at the ability for a machine to fly. I have always wanted to explore ideas of flight and be able to actually fly. I think I may have found my childhood fantasy in the world of aeronautical engineering. The object of my paper is to give me more insight on my future career as an aeronautical engineer. This paper was also to give me ideas of the physics of flight and be to apply those physics of flight to compete in a high school competition.
There is a world of jobs and careers out in the world. I don't want to be a doctor or nurse or vet or anything like that. All i want to be is a Mechanic. Not a car or truck mechanic but an airplane mechanic. It's my dream to go tho airfields and work on airplanes. As i'm working on airplanes I would love to have my pilots license as well. My career is going to consist of awesome airplane mechanics.
This project is intended to give the student an improved understanding of aircraft dynamic behavior thought the use of a SIMULINK flight simulation. The student is to use knowledge of flying and handling qualities to appropriately grade a certain maneuver, of a certain aircraft, under a certain condition. The student is to modify the performance of an aircraft through the implementation of a control law.
World War was had been the first major conflict that saw use of the newly invented airplane. Newspapers filled with stories of daring pilots, valiantly taking down the opposing Luftwaffe. Ace became a term for a pilot who successfully shot down at least five enemy aircraft; however there were a special few pilots who far surpassed this and went down in history as the top aces. America’s “Ace of Aces” was Eddie Rickenbacker who throughout the war won twenty-six aerial victories, and earned the Medal of Honor for taking on seven German planes by himself, downing two (Sherman). Coming in second was Frank Luke Jr. with 14 enemy balloons and four enemy planes. He was known as the “Arizona Balloon Buster” and was posthumously awarded the Medal of Honor for his last victory, when he shot down three balloons while taking fire from eight planes, then, as he was going down, he opened fire on German ground troops killing six, and finally, when asked to surrender, he instead
hen I graduate high school I plan to Join the United States Air Force and being a Aircraft and Avionics Technician. This career consists of working on Aircraft this job also requires to do inspections on Aircraft required by the Federal Aviation Administration (FAA) (“Summary’’). The reason I chose this career is because my father has this career and it seems very interesting to me. I also like this career because I will get to learn about how Aircraft fly and get to work on the Aircraft.
Kites for centuries have been an interesting object of flight fascinating people all over the world. The standard diamond kite can be made at home simply with 2 wooden dowels, plastic sheeting, strong tape, twine and a kite string or fishing line. Considering kites are simple and easy to make, at home you can also design it whatever way you like. It’s become an unpopular activity for as you can see technology has advanced, but today I’ll be presenting to you the history and aerodynamics on kites before the advancement of technology and a more scientific approach.
When a body moves with high velocity at that moment aerodynamics forces such as drag, lift (or down force) are the primary concern that are caused by the airflow over the body. In engineering aerodynamics principles are applied in every kind of design or structures such as automobiles, aeroplanes, tall buildings and bridges. However, largely the aerodynamics principles are applied on aeroplanes and automobiles. This project involves the influence of aerodynamics principles over the rear wing of a Subaru Sports Sedan race car.
In this module you design a rocket and you launch it at the end of the quarter. You also paint your rocket with the colors you like. In this module you learn about how a rocket is launched and how they control the rocket. You also learn about the main people that contributed to the research and tested the rockets.
The wings of airplanes are called airfoils. Airfoils have a cambered shaped, which means arched or curved, in order to allow them to produce lift even if the wing isn’t angled downward. Lift is generated due to the fact that air flow over and under the surface of the airfoil. The airfoil is designed so the top surface of the wing is “longer” than the bottom surface of the wing. This means that the distance between the front of the wing to the back of the wing is greater along the top surface of the wing than the bottom surface.
This report aims to investigate the effect the angle of attack of an aerofoil has on the air flow around it. This was done by recording the lift and drag forces the aerofoil experienced when positioned at different angles of attack. The experimental lift force the aerofoil experienced when positioned at different angles of attack was then compared with theoretical values. An attempt was made to explain any discrepancies between experimental and theoretical values.
New Large Aircraft (NLA) or New Generation Large Aircraft (NGLA) are the future of long distance air travel. With current air craft size reaching unknown proportions to humankind, airports that are interested in attracting future business as well as the revenue the large amount of passengers per flight may generate, will have to adapt their installations to the demanding needs of these supersized vehicles. The following paper will focus on the new Airbus A380 and the requirements that airports inviting this magnificent work of engineering to use their installations will need to meet.