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Grant: Discovery Grants Program - Individual

Toronto Metropolitan University

$32,000.00

Mechanical performance modeling and failure prediction of Fiber Reinforced Additively Manufactured (FRAM) composites under static, dynamic, cyclic, and long-term loading conditions

FY 2024-25

Summary
Towards the ultimate goal of using additively manufactured composites as end-use parts for functional engineering applications, this research pursues the following two long-term objectives: 1- Develop a micromechanical model to study Fiber Reinforced Additively Manufactured (FRAM) composites aimed at understanding the failure mechanisms in order to prevent/delay failure and enhance performance. 2- Establish a progressive damage model based on Continuum Damage Mechanics (CDM) using the insight and information obtained from the afore-developed micromechanical model to predict the failure of FRAM composite parts under static, dynamic, cyclic, and long-term loading conditions. The research effort seeks to present an experimentally validated numerical substitute for some of the costly and time-consuming experiments on FRAM composite materials. It aims in particular to examine the failure mechanisms and how these mechanisms are influenced by the additive manufacturing parameters. The break-down of the short-term objectives of this study is as follows: 1- Development of a micromechanical model with a Representative Volume Element (RVE) that can represent a 3D-printed fiber reinforced composite as opposed to the RVE used for conventionally manufactured composites. 2- Implementation of viscoelasticity and viscoplasticity into the constitutive behaviour of the fiber and thermoplastic matrix. 3- Experimental test program for material characterization of the fiber and matrix constituents. 4- Using the micromechanical model to predict the effective properties of 3D printed composite parts. 5- Using the micromechanical model to determine failure mechanisms and the correlation between the microstructure and the mechanical properties. 6- Development of a CDM model to predict the failure of 3D printed composites. 7- Experimental test program on various 3D printed composites and using the test results to validate the proposed damage model. 8- Implementation of the proposed damage model into a commercial Finite element- based software. According to the Aerospace Industries Association of Canada, advanced composites are one of three "priority technologies" of strategic importance to the future of the Canadian Aerospace Industry. An untapped potential in this area is the use of additively manufactured composite parts. Recent studies have shown that reinforcing 3D printed thermoplastic components can greatly enhance the mechanical properties and thus the functionality of these parts. Considering the various advantages of the additive manufacturing technology such as low cost, short production time, and minimal waste of material, the use of 3D printed composites will be a great step towards employing these materials as end-use, functional load- bearing components.
Program
Discovery Grants Program - Individual
Location
Ontario, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data

As published

Application id
RGPIN-2021-03053
Name nom
Fawaz, Zouheir
Department département
Aerospace Engineering - Aerospace Engineering
Organization id
43
Institution établissement
Toronto Metropolitan University
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2024
Competition year année de concours
2021
Award amount
32000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
DISCOVERY RESEARCH
Group fr
RECHERCHE AXÉE SUR LA DÉCOUVERTE
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2100
Research subject group en
Mechanical engineering
Research subject group fr
Génie mécanique
Research subject en
Mechanical engineering
Research subject fr
Génie mécanique
Field of research list names en
Not available
Field of research list names fr
Non disponible
Socioeconomic objective list names en
Not available
Socioeconomic objective list names fr
Non disponible
Application title
Mechanical performance modeling and failure prediction of Fiber Reinforced Additively Manufactured (FRAM) composites under static, dynamic, cyclic, and long-term loading conditions
Keywords
fiber reinforced composites; additive manufacturing; thermoplastic composites; continuum damage mechanics; numerical modeling; experimental characterization; failure prediction; strength; fatigue; mechanical properties
Application summary
Towards the ultimate goal of using additively manufactured composites as end-use parts for functional engineering applications, this research pursues the following two long-term objectives: 1- Develop a micromechanical model to study Fiber Reinforced Additively Manufactured (FRAM) composites aimed at understanding the failure mechanisms in order to prevent/delay failure and enhance performance. 2- Establish a progressive damage model based on Continuum Damage Mechanics (CDM) using the insight and information obtained from the afore-developed micromechanical model to predict the failure of FRAM composite parts under static, dynamic, cyclic, and long-term loading conditions. The research effort seeks to present an experimentally validated numerical substitute for some of the costly and time-consuming experiments on FRAM composite materials. It aims in particular to examine the failure mechanisms and how these mechanisms are influenced by the additive manufacturing parameters. The break-down of the short-term objectives of this study is as follows: 1- Development of a micromechanical model with a Representative Volume Element (RVE) that can represent a 3D-printed fiber reinforced composite as opposed to the RVE used for conventionally manufactured composites. 2- Implementation of viscoelasticity and viscoplasticity into the constitutive behaviour of the fiber and thermoplastic matrix. 3- Experimental test program for material characterization of the fiber and matrix constituents. 4- Using the micromechanical model to predict the effective properties of 3D printed composite parts. 5- Using the micromechanical model to determine failure mechanisms and the correlation between the microstructure and the mechanical properties. 6- Development of a CDM model to predict the failure of 3D printed composites. 7- Experimental test program on various 3D printed composites and using the test results to validate the proposed damage model. 8- Implementation of the proposed damage model into a commercial Finite element- based software. According to the Aerospace Industries Association of Canada, advanced composites are one of three "priority technologies" of strategic importance to the future of the Canadian Aerospace Industry. An untapped potential in this area is the use of additively manufactured composite parts. Recent studies have shown that reinforcing 3D printed thermoplastic components can greatly enhance the mechanical properties and thus the functionality of these parts. Considering the various advantages of the additive manufacturing technology such as low cost, short production time, and minimal waste of material, the use of 3D printed composites will be a great step towards employing these materials as end-use, functional load- bearing components.