Need an research paper on the newtons law of motion. Needs to be 5 pages. Please no plagiarism. Fries Ailerons add drag by extending one part of the aileron down into the airstream. In contrast, the other half of the aileron is extended up into the airstream according to the manual prepared by the Headquarters of the Department of Army (2007).A Stabilator is the combination of a stabilizer and an elevator for better maneuverability. It is used to generate and control the pitching motions of the aircraft (Benson, 2008).The boat’s speed can be obtained by measuring the flow of the water beneath it relative to the surface of the ship. This can be done by measuring the flow’s static and dynamic pressures using tubes connected to pressure gauges with openings oriented perpendicular and parallel to the flow, respectively (Anderson & Eberhardt, 2001). The changes in dynamic pressure would be directly proportional to the speed of the boat.The B747 has a wider wingspan than the standard light aircraft to compensate for its heaviness. Its wider wingspan lowers its wing load and effectively slows down its flight. However, its wingspan allows the plane to better control the aircraft’s attitude and therefore increases maneuverability.Structural loads are loads or forces acting on the aircraft caused by its internal structure and form. One example is the weight of the material used in the aircraft’s body for it to be enough to withstand the pressure during flight while also being strong enough to support its cargoes. Structural loads may also pertain to the forces exerted on specific parts of the aircraft due to its form.
According to Benson of NASA (2010), the lift is generated due to the contact between the air and the flying solid object. Since the molecules of air is free to move, there is variation in both pressure and velocity along the flow of air. Making use of either the Bernoulli’s equation or Newton’s third law of motion, integration of either pressure or velocity variations would conclude an aerodynamic force.An aircraft cannot fly straight and level if it is in an out-of-trim position. If this happens, it would be difficult to control the attitude of the plane. The gauges and parts of the flight may not function properly. The pilot may also get disoriented and could end up in an accident.