Tesi etd-04022012-093143 |
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Tipo di tesi
Tesi di laurea specialistica
Autore
LAVORINI, LORENZO
URN
etd-04022012-093143
Titolo
Numerical validation of a new criterion of fracture for elastic-plastic materials with a subcritical crack growth
Dipartimento
INGEGNERIA
Corso di studi
INGEGNERIA AEROSPAZIALE
Relatori
relatore Prof. Frediani, Aldo
relatore Dott. Binante, Vincenzo
relatore Dott. Binante, Vincenzo
Parole chiave
- elastic-plastic materials
- fem
- subcritical crack growth
Data inizio appello
16/04/2012
Consultabilità
Non consultabile
Data di rilascio
16/04/2052
Riassunto
The objective of this thesis is to study the dependence of the P method on
the geometry of the specimen, crack length and applied load. We will try to
show how such constant value of the trace of the energy momentum tensor is
achieved in conjunction with the propagation of the crack (thus with the break
in the material microstructure); will also be interesting to show how this value is
an intrinsic characteristic of the material in analogy to that seen for the critical
value of the Stress Intensity Factor. In order to do this crack propagation in
thin-walled panels of two dierent aluminum alloys will be studied and, for one
of these, we will study the crack propagation starting from four dierent initial
crack length. Simulation will be carried out according to the assumption of
Plane Stress. A further simulation will be carried out to show the behavior of
the specimens according to the Plane Strain assumption.
the geometry of the specimen, crack length and applied load. We will try to
show how such constant value of the trace of the energy momentum tensor is
achieved in conjunction with the propagation of the crack (thus with the break
in the material microstructure); will also be interesting to show how this value is
an intrinsic characteristic of the material in analogy to that seen for the critical
value of the Stress Intensity Factor. In order to do this crack propagation in
thin-walled panels of two dierent aluminum alloys will be studied and, for one
of these, we will study the crack propagation starting from four dierent initial
crack length. Simulation will be carried out according to the assumption of
Plane Stress. A further simulation will be carried out to show the behavior of
the specimens according to the Plane Strain assumption.
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