Complex Engineering Systems: Failure Of The Most Complex Engineering Systems

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Abstract
One of the most complex engineering system is failure of an aircraft component which leads to the catastrophic consequences which result in events that cause loss of life and also damage the aircraft.
I’m doing investigation on defect and failure in the aircraft structures which is important for the prevention of further catastrophic incidents. One of the main reason for the failure of the aircraft components or structure under high stress which is during the operation where the component no longer bear the stress which is imposed.
Here in the analysis of stress on the piston road end is carried out with the finite element techniques. The most common cause for the failure of the aircraft is complex engineering system that causes …show more content…

I’m doing investigation on defect and failure in the aircraft structures which is important for the prevention of further catastrophic incidents. One of the main reasons for the failure of the aircraft components or structure under high stress which is during the operation where the component no longer bears the stress which is imposed. Here in the analysis of stress on the piston road end is carried out with the finite element techniques. The most common cause for the failure of the aircraft is complex engineering system that causes Fatigue cracking which causes structural failures in the …show more content…

The stress raiser which is in the nature of geometrical or in metallurgical or combination of two. Geometrical stress raiser in the shape of the parts such as step changes in diameter, sharp corners and surface discontinuities like notches and machining marks etc. are non-uniformities. Metallurgical stress are stress raiser which may be corrosion pits, brittle second-phase particles, gross metallic inclusions, quench cracks etc. Also, the initiation of fatigue failures where microstructure of the material plays a vital role but also the fatigue crack to cause failure of the material during the progressive growth. Near free surface Fatigue initiation occurs frequently, where nominal stress will be higher. While doing manufacturing and fabrication processes where machining can form surface irregularities or discontinuities which is the point of stress concentration also initiate the fatigue

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