Since damage evolutions of materials play important roles in simulations, such as ballistic impacts and collisions, a new experimental and numerical method is established to determine the revised Johnson–Cook (JC) failure parameters of a 2618 aluminum alloy and a Ti-6Al-4V titanium alloy. Not only the strain distributions, but also the stress triaxialities of designed specimens with different notches, are analyzed and revised using the finite element (FE) model. Results show that the largest strain concentrated on the surface of the circumferential area where the initial damage happened, which coincided with the practical damage evolution in the FE model. The complete damage strain, which denoted the largest strain before fracture cal...
Based on our needs, that is to say, through precise simulation of the impact phenomena that may occu...
Extraction of the material stress-strain curve from a dynamic tensile or shear e...
A collision between a bird and an aircraft engine occurs once in a while during flight, and can caus...
Since damage evolutions of materials play important roles in simulations, such as ballistic impacts ...
Large deformation and fracture processes of materials are often involved in the finite element simul...
A numerical model relying on triaxial and deviatoric levels of stress is used to describe ductile da...
In this paper, modified Mohr Coulomb (MMC) and Lemaitre's damage model have been calibrated for a Ti...
It is a significant issue to deeply understand the nature relationships between damage degradation a...
A physics-based, uncoupled damage model is calibrated using cylindrical notched round tensile specim...
Containment structures for aircraft engines must withstand impacts of failed engine components, whi...
The plastic behavior of the Ti-6Al-4V alloy includes several features as strength differential effe...
This report describes studies of the deformation and failure behavior of Ti-6Al-4V and 2024-T3 alumi...
Nowadays the numerical failure simulations are becoming popular in industrial applications; in this ...
peer reviewedIn this research, the Stewart-Cazacu micromechanics coupled damage model is extended an...
Uniaxial and notched tension samples are utilized to investigate the damage and failure of titanium ...
Based on our needs, that is to say, through precise simulation of the impact phenomena that may occu...
Extraction of the material stress-strain curve from a dynamic tensile or shear e...
A collision between a bird and an aircraft engine occurs once in a while during flight, and can caus...
Since damage evolutions of materials play important roles in simulations, such as ballistic impacts ...
Large deformation and fracture processes of materials are often involved in the finite element simul...
A numerical model relying on triaxial and deviatoric levels of stress is used to describe ductile da...
In this paper, modified Mohr Coulomb (MMC) and Lemaitre's damage model have been calibrated for a Ti...
It is a significant issue to deeply understand the nature relationships between damage degradation a...
A physics-based, uncoupled damage model is calibrated using cylindrical notched round tensile specim...
Containment structures for aircraft engines must withstand impacts of failed engine components, whi...
The plastic behavior of the Ti-6Al-4V alloy includes several features as strength differential effe...
This report describes studies of the deformation and failure behavior of Ti-6Al-4V and 2024-T3 alumi...
Nowadays the numerical failure simulations are becoming popular in industrial applications; in this ...
peer reviewedIn this research, the Stewart-Cazacu micromechanics coupled damage model is extended an...
Uniaxial and notched tension samples are utilized to investigate the damage and failure of titanium ...
Based on our needs, that is to say, through precise simulation of the impact phenomena that may occu...
Extraction of the material stress-strain curve from a dynamic tensile or shear e...
A collision between a bird and an aircraft engine occurs once in a while during flight, and can caus...