The thickness of the gaseous layer in disk galaxies

il profilo verticale del gas dipende sia dal potenziale galattico, e quindi dalla distribuzione di materia, sia dalla dispersione di velocit`a del gas La nostra analisi teorica ha mostrato che l’altezza scala dell’idrogeno gassoso ad un certo raggio `e fortemente legata alla componente di massa dominate: nelle parti centrali, dove domina la materia barionica, il disco gassoso incrementa il suo spessore esponenzialmente con una lunghezza scala pari al doppio di quella del disco stellare; dalle zone intermedie fino alla fine del disco, il profilo verticale del gas `e influenzato dalla distribuzione di DM. In queste zone lo spessore del disco gassoso cresce con il raggio in maniera circa lineare. Tale fenomeno viene definito gas flaring. Lo scopo principale di questa tesi `e la ricerca di una nuova tecnica per poter stimare il profilo vertical del gas in galassie con inclinazione intermedia.

Numerical evaluation of material model and thickness effect on LSP induced residual stresses

Laser Shock Peening (LSP) is a technological process used to improve mechanical properties in metallic components. When a short and intense laser pulse irradiates a metallic surface, high pressure plasma is generated on the treated surface; elasto-plastic waves, then, propagate inside the target and create plastic strain. This surface treatment induces a deep compressive residual stresses field on the treated area and through the thickness; such compressive residual stress is expected to increase the fatigue resistance, and reduce the detrimental effects of corrosion and stress corrosion cracking.

Influence of adhesive thickness on adhesively bonded joints under fatigue loading

Research on adhesive joints is arousing increasing interest in aerospace industry. Incomplete knowledge of fatigue in adhesively bonded joints is a major obstacle to their application. The prediction of the disbonding growth is yet an open question. This thesis researches the influence of the adhesive thickness on fatigue disbond growth. Experimental testing on specimens with different thickness has been performed. Both a conventional approach based on the strain energy release rate and an approach based on cyclic strain energy are provided. The inadequacy of the former approach is discussed. Outcomes from tests support the idea of correlating the crack growth rate to the cyclic strain energy. In order to push further the study, a 2D finite element model for the prediction of disbond growth under quasi-static loading has been developed and implemented in Abaqus. Numerical simulations have been conducted with different values of the adhesive thickness. The results from tests and simulations are in accordance with each other. According to them, no dependence of disbonding on the adhesive thickness has been evidenced.