Understanding the degradation of material properties and stress–strain behavior of rubberlike materials that have been exposed to elevated temperature is essential for rubber components design and life time prediction. The complexity of the relationship between hyperelastic materials, crosslinking density (CLD), and chemical composition presents a difficult problem for the accurate prediction of mechanical properties under thermal aging. In this paper, a new and relatively simple mathematical formulation is presented to expresses the change in material properties of hyperelastic materials under thermal aging. The proposed formulation has been applied to a natural rubber (NR). Testing was performed on more than 130 specimens that were thermally aged then subjected uniaxial tension and hardness tests. The aging temperatures ranged from 76.7 °C to 115.5 °C, and the aging times ranged from 0 to 600 h. Based on the recorded experimental data, the NR mechanical properties under thermal aging showed a similar behavior to the rate of change of the CLD with aging time and temperature. Three mechanical properties have been chosen to be studied in this paper: the ultimate tensile strength, the fracture stretch value, and the secant modulus at 11.0% strain. The proposed mathematical formulation is a phenomenological equation that relates the material properties with the change in CLD based on a form of Arrhenius equation. The proposed equation showed promising results compared to the experimental data with an acceptable error margin of less than 10% in most of the cases studied.
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January 2018
Research-Article
A Model for Calculating Hyperelastic Material Properties Under Thermal Aging
Ahmed G. Korba,
Ahmed G. Korba
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: agkorba@crimson.ua.edu
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: agkorba@crimson.ua.edu
Search for other works by this author on:
Abhishek Kumar,
Abhishek Kumar
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: akumar16@crimson.ua.edu
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: akumar16@crimson.ua.edu
Search for other works by this author on:
Guoqin Sun,
Guoqin Sun
Department of Mechanical Design and Method,
College of Mechanical Engineering and
Applied Electronics Technology,
Beijing University of Technology,
Beijing 100022, China
e-mail: sguoq@bjut.edu.cn
College of Mechanical Engineering and
Applied Electronics Technology,
Beijing University of Technology,
Beijing 100022, China
e-mail: sguoq@bjut.edu.cn
Search for other works by this author on:
Mark E. Barkey
Mark E. Barkey
Professor
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: mbarkey@eng.ua.edu
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: mbarkey@eng.ua.edu
Search for other works by this author on:
Ahmed G. Korba
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: agkorba@crimson.ua.edu
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: agkorba@crimson.ua.edu
Abhishek Kumar
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: akumar16@crimson.ua.edu
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: akumar16@crimson.ua.edu
Guoqin Sun
Department of Mechanical Design and Method,
College of Mechanical Engineering and
Applied Electronics Technology,
Beijing University of Technology,
Beijing 100022, China
e-mail: sguoq@bjut.edu.cn
College of Mechanical Engineering and
Applied Electronics Technology,
Beijing University of Technology,
Beijing 100022, China
e-mail: sguoq@bjut.edu.cn
Mark E. Barkey
Professor
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: mbarkey@eng.ua.edu
Department of Aerospace
Engineering and Mechanics,
The University of Alabama,
Tuscaloosa, AL 35401
e-mail: mbarkey@eng.ua.edu
Contributed by the Materials Division of ASME for publication in the JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY. Manuscript received February 2, 2017; final manuscript received June 18, 2017; published online August 9, 2017. Assoc. Editor: Huiling Duan.
J. Eng. Mater. Technol. Jan 2018, 140(1): 011006 (10 pages)
Published Online: August 9, 2017
Article history
Received:
February 2, 2017
Revised:
June 18, 2017
Citation
Korba, A. G., Kumar, A., Sun, G., and Barkey, M. E. (August 9, 2017). "A Model for Calculating Hyperelastic Material Properties Under Thermal Aging." ASME. J. Eng. Mater. Technol. January 2018; 140(1): 011006. https://doi.org/10.1115/1.4037170
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