To solve the problems of few-shot samples, different structural degradation trends and poor
damage evaluation effect in fatigue damage evaluation of aircraft structure, an intelligent …

The frequent utilisation of aircraft across the globe significantly increases the likelihood of
structural failures. One contributing factor to aviation accidents, as revealed by the …

In this study, the root cause of a recurring corrosion problem at the tip of an internally cooled
high-pressure turbine blade (HPT) of a turbofan engine was investigated. A two-pronged …

The research is aimed to identify the failure mechanism which leads to cracks development
in the wing spar cap of a transport aircraft and subsequently devise a mitigation strategy to …

This study focuses on determining the root cause of crack development in a longeron fitting
of a cargo aircraft followed by devising of appropriate mitigation strategy to prevent such …

Purpose The present research paper focuses on the free in-plane vibrational analysis of a
curved cracked cantilever beam using experimental and computational methods with reuse …

Interdependence is an inherent feature of the cyber-physical system. Small damage to one
component in the system may affect several other components, leading to a series of …

Each part of the reducer has a design life, if any of the parts fail to reach the design life, it will
affect the normal operation of the entire equipment. The life of a part is affected by its own …

Multi-objective optimization design of gear shaft, first determine the design variables, gear
shaft structure size mainly includes length size and radius size, gear shaft shaft diameter as …