Stress And Strain On Aircraft – Article Example

Stress and Strain on Aircraft Stress and Strain on Aircraft Every airplane is tostructural stress because it acts on an airplane whether on ground or in flight. Stress is the load applied to a unit area of material. What is the effect of stress in an airplane? Stress produces a deformation or deflection in the material, which is called strain. In most cases stress is usually accompanied by strain. Most aircrafts are built using numerous materials; the main one is the aluminum alloys (Katz, 1997). The construction of aircraft uses bolts, crews, rivets, and special bonding adhesives essential in holding the sheet metal in place. Regardless of the method used, all parts of the fuselage usually carry a load; resist a stress placed on it. The design has numerous metal skin playing different roles to ensure that the safe arrangement adept of withstanding expected load and stress (Katz, 1997).
Stresses and Strains on Aircraft Copyright © 1997 by Peter Katz Productions
The above article is essential because it has enough information that may help a person who does not understand the strains and stresses on aircraft. It elucidates regarding numerous types of structural stress namely: torsion, compression, shear, tension, and bending. It further highlights concerning the construction of the fuselage design and its construction, which are designed to withstand both compression and tension loads that eventually defines stress and strains in an aircraft. Nonetheless, the article does not highlight in details the wing structure that helps transmit loads to the fuselage (Katz, 1997).
Finally, it is noteworthy that stress and strain is a fact of life for airplanes. One performs by the help of the other and most pilots should be worried about the undue stress on the aircraft. It should be handled carefully and in line with its design confines because there is normal and abnormal stress.
Reference
Katz, P. (1997). Stresses and Strains on Aircraft. Retrieved on November 6, 2014, from http://www.netc.navy.mil/nascweb/sas/structures_stress_strain.htm