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Thermoelastic-plastic stress analysis in a thermoplastic composite disc
- Publication Year :
- 2005
-
Abstract
- In this study, an elastic-plastic stress analysis is carried out on a steel fiber-reinforced thermoplastic composite disc under uniform thermal distribution. The composite disc is reinforced by steel fibers curvilinearly. Its mechanical properties are obtained by strain gauges and Instron test machine. The modulus of elasticity in the tangential direction is measured by fitting a solid disc to the composite disc, exactly. However, other material properties are found approximately. The material is assumed to be non work hardening. Stresses are determined for uniform temperature distribution. The magnitude of the tangential stress component in polar coordinates is the highest at the inner points of the disc. Plastic solution is performed numerically. Plastic region beg-ins at the inner surface of the disc. The residual stress component of the tangential stress is the highest at the inner surface of the disc. C1 Dokuz Eylul Univ, Dept Mech Engn, TR-35100 Izmir, Turkey. Pamukkale Univ, Dept Mech Engn, Camlik, Denizli, Turkey.
- Subjects :
- Electric resistance
Materials science
Polymers and Plastics
Stress analysis
Composite number
Hydraulics
Young's modulus
02 engineering and technology
Work hardening
Steel fiber
Pressure effects
Disc
Fiber reinforced materials
Matrix algebra
Stress (mechanics)
symbols.namesake
Thermoelastic damping
0203 mechanical engineering
Residual stress
Materials Chemistry
Hydraulic press
Thermoplastic
Composite material
thermoelastic-plastic
steel fiber
thermoplastic
disc
Elastic modulus
Thermoelasticity
Strain hardening
Mechanical Engineering
Thermoelastic- plastic
Composite materials
021001 nanoscience & nanotechnology
020303 mechanical engineering & transports
Mechanics of Materials
Thermoelastic-plastic
Ceramics and Composites
symbols
Polyethylenes
0210 nano-technology
Material properties
Subjects
Details
- Language :
- English
- Database :
- OpenAIRE
- Accession number :
- edsair.doi.dedup.....d172d8be56a76d43a07d682ee1140f53