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Differential Models Of Hysteresis

고분자 재료에서의 파괴역학 ( Fracture Mechanics in Polymers )

A novel approach based on the elastoplastic fatigue damage and machine learning models for life prediction of aerospace alloy parts fabricated by additive manufacturing

Well-designed and well-operated postharvest mechanical handling processes are vital if fresh fruits are to enter markets with minimal damage. The susceptibility of fruit to quality loss during handling is largely determined by mechanical contact and damage. This article reviews current understanding concerning the effect of impact and other mechanical contacts on fruits. It also discusses the major mechanical models that represent the interaction between fruits or a fruit and a surface. In total, 25 mechanical models associated with compression and impact behaviors of fresh fruits, mainly characterizing such behavior between 2 deformable spherical bodies and between a deformable spherical body and a rigid plate are reviewed. Finally, possible future research directions are discussed. The main challenge in fruit handling is to recognize and prevent microscopic damage to fruits, especially internal tissue/cell damage and microcracks resulting from multiple/repetitive impacts and compressions.

https://onlinelibrary.wiley.com/doi/pdf/10.1111/1541-4337.12296

Mechanical Models of Compression and Impact on Fresh Fruits.

The early-warning system based on hybrid optimization algorithm and fuzzy synthetic evaluation model

Observation of the relation between uniaxial creep and stress relaxation of filled rubber

Estimation of air-spring life based on accelerated experiments

The material characterization of the air spring bellow sealing layer

This paper details an advanced method of continuous fatigue damage prediction of rubber fibre composite structures. A novel multiaxial ener gybased approach incorporating a mean stress correction is presented and also used to predict the fatigue life of a commercial vehicle air spring. The variations of elastic strain and complementary energies are joined to form the energy damage parameter. Material parameter is introduced to adapt for any observed mean stress effect as well as being able to reprodu ce the wellknown Smith-Watson-Topper criterion. Since integration to calculate the energies is simplified, the approach can be empl oyed regardless of the complexity of the thermomechanical load history. Several numerical simulations and experimental tests were performed in order to obtain the required stressstrain tensors and the corresponding fatigue lives, respectively. In simulations, the rubber material of the air spring was simulated as nonlinear elastic. The mean stress parameter, which controls the influence of the mean stress on fatigue life, wa s adjusted with respect to those energy life curves obtained experimen- tally. The predicted fatigue life and the location of failure are in very good agreement with experimental observations.

/pdf/continuous-fatigue-damage-prediction-of-a-rubber-fibre-2w8jvgxlw3.pdf

Continuous fatigue damage prediction of a rubber fibre composite structure using multiaxial energy-based approach

/pdf/determining-influential-factors-for-an-air-spring-fatigue-3g82jde17i.pdf

Simon Oman

Papers

Observation of the relation between uniaxial creep and stress relaxation of filled rubber

Estimation of air-spring life based on accelerated experiments

The material characterization of the air spring bellow sealing layer

Continuous fatigue damage prediction of a rubber fibre composite structure using multiaxial energy-based approach

Determining influential factors for an air spring fatigue life