航空学および航空宇宙工学ジャーナル
オープンアクセス

概要

Review of Different Methods to Study and Investigate Aircraft Structure Failure under Dynamic Loading

Usama Tariq*

This Article aims at studying and investigating different methods of aircraft’s structure failure under dynamic loading. Aircraft Structural failure can cause catastrophic results with lots of loss of lift and the aircraft as well. So, it is important to investigate the major causes that lead to failure of aircraft. This paper discusses the major causes of failure due to material used in construction of aircraft wing and also fatigue failure. Along with investigation future remedies are also concluded with different case studies and their results. Aircraft wing is constructed using high strength materials so that they can withstand major loads during flight for longer duration. Fatigue failure monitoring has now been included in all aircraft. Failure monitoring system collects all data required to calculate safe life, damage life or time required to inspect whole aircraft. This paper presents fatigue monitoring systems and tools of military agile aircraft. It comprehensively reviews all techniques used in military aircrafts and their current systems. Some major problems and their corrective measures are suggested through case studies in different analysis of failure method. Different tests, analysis and their steps are included in this survey paper.