Back to Search
Start Over
Optimization and Static Stress Analysis of Hybrid Fiber Reinforced Composite Leaf Spring
- Source :
- Advances in Materials Science and Engineering, Vol 2015 (2015)
- Publication Year :
- 2015
- Publisher :
- Hindawi Limited, 2015.
-
Abstract
- A monofiber reinforced composite leaf spring is proposed as an alternative to the typical steel one as it is characterized by high strength-to-weight ratio. Different reinforcing schemes are suggested to fabricate the leaf spring. The composite and the typical steel leaf springs are subjected to the same working conditions. A weight saving of about more than 60% can be achieved while maintaining the strength for the structures under consideration. The objective of the present study was to replace material for leaf spring. This study suggests various materials of hybrid fiber reinforced plastics (HFRP). Also the effects of shear moduli of the fibers, matrices, and the composites on the composites performance and responses are discussed. The results and behaviors of each are compared with each other and verified by comparison with analytical solution; a good convergence is found between them. The elastic properties of the hybrid composites are calculated using rules of mixtures and Halpin-Tsi equation through the software of MATLAB v-7. The problem is also analyzed by the technique of finite element analysis (FEA) through the software of ANSYS v-14. An element modeling was done for every leaf with eight-node 3D brick element (SOLID185 3D 8-Node Structural Solid).
- Subjects :
- Brick
Materials science
Article Subject
Composite number
General Engineering
Fiber-reinforced composite
Finite element method
Shear (sheet metal)
Leaf spring
lcsh:TA401-492
lcsh:Materials of engineering and construction. Mechanics of materials
General Materials Science
Fiber
Composite material
MATLAB
computer
computer.programming_language
Subjects
Details
- ISSN :
- 16878442 and 16878434
- Volume :
- 2015
- Database :
- OpenAIRE
- Journal :
- Advances in Materials Science and Engineering
- Accession number :
- edsair.doi.dedup.....2e306009594e13e3cb33d2d7fc1d7fda