Do you believe that combining the fiber and matrix is enough to create a fiber-reinforced composite (FRC)? That’s not all! The composite needs a well-designed curing process to become acceptable for real-world applications. Have you ever explored the role of Abaqus curing process simulation in designing the curing cycles?
Without proper curing, fiber-reinforced composites would not reach their desired performance. Fiber-reinforced composite curing simulation, however, is a complex and challenging task. Curing simulation using subroutines is a way to address this challenge. Abaqus, with its subroutines, stands out as a powerful tool for composite curing simulation.
This post explores the world of fiber-reinforced composites, starting with their fundamentals and applications. Next, we will discuss the crucial role of curing in achieving high-quality composites, followed by an exploration of various curing methods. Lastly, we will explain how Abaqus subroutines simplify the efficient simulation of the composite curing process.
1. What are fiber-reinforced composites (FRCs)?
Fiber-reinforced composites are a class of materials consisting of two main phases: reinforcing fibers (phase 1) embedded within a matrix (phase 2). However, some references consider the interface between the matrix and fiber as a separate phase. Figure 1 depicts a piece of fiber-reinforced composite.
Figure 1: A piece of fiber-reinforced composite
The fibers in FRCs are typically made of stiff materials to provide sufficient strength for the composite. The matrix, often a type of polymer, holds the fibers together and transfers stress between them. When these two components are combined, a composite with unique properties is formed. This composite is lightweight yet strong. So, it is suitable for various applications.
2. Common types of FRCs
Fiber-reinforced composite (FRC) is a general term that represents a wide range of materials with diverse properties. Depending on the characteristics of the fibers and matrix, FRCs can be classified into various types. Each type, with its distinct properties, is ideal for specific applications.
Figure 2 presents a classification of FRCs based on their matrix material. As shown, FRCs can be made from various matrices, including polymers, metals, ceramics, and carbon/carbon materials. Among these, polymer matrix FRCs are the most widely used composites. They can be further divided into two subgroups: thermoplastics and thermosets.
Figure 2: A classification of composites based on their matrix material
Thermoplastics are a type of polymer-based matrix that can be remelted after curing. In contrast, thermosets remain permanently cured once heated. Figure 3 compares the behavior of thermoplastic and thermoset matrices when reheated after curing.
Figure 3: Comparison of the behavior of thermoplastic and thermoset matrices upon reheating
Thermosets form an extensive group of FRCs with various types and applications. Figure 4 provides a classification of thermoset composites based on the matrix and fiber materials, highlighting their diversity. While this post has focused on thermoset composites, thermoplastic composites also play a significant role in the FRC industry.
Figure 4: A classification of thermoset composites based on the matrix and fiber materials
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2.1. Single vs. multilayered FRCs
We can produce fiber-reinforced composites in both single and multilayered forms. As their names suggest, single-layered FRCs consist of a single layer, while multilayered FRCs (laminates) include multiple layers. Figure 5, illustrates the structure of a laminate, where each individual layer is called a lamina or ply.
Figure 5: Schematic representation of a multilayered composite [1]
As shown in Figure 6, composite plies can have the same or different orientations, so-called unidirectional or multidirectional laminates, respectively.
Figure 6: Representation of the unidirectional and multidirectional laminates [2]
It was a brief overview of the common types of fiber-reinforced composites. You can explore more about this topic by conducting an online search.
3. Advantages of FRCs over traditional materials
Have you ever asked yourself about the advantages of FRCs over other materials? The answer may depend on the specific type of FRC. However, in general, they are lightweight, high-strength, stiff, and durable materials with the ability to resist corrosion, impact, and fire. These features collectively make FRCs more suitable than other materials for numerous applications.
4. Attractive applications of FRCs
From aerospace to the medical field, FRCs have found applications in diverse areas. This post has highlighted a few examples of their many applications.
FRCs have found numerous applications in the aircraft production industry. For instance, by employing FRCs, we can reduce the weight of aircraft and their fuel consumption. Moreover, FRCs enable the improvement of aerodynamic performance and corrosion resistance of aircraft. Figure 7 showcases some parts of the Airbus A380 made from composite materials.
Figure 7: An overview of Airbus A380’s parts made from composite materials
FRCs are highly resistant to impact and corrosion. This makes them ideal for a wide range of military applications. For example, the armored vehicle in Figure 8 showcases the advantages of FRCs in defense systems. Moreover, the lightweight nature of FRCs enhances vehicle movement and reduces radar and thermal signatures.
In recent years, composites have played an increasingly important role in the automotive industry. They can be used to enhance the safety and efficiency of cars, while also contributing to the reduction of emissions and noise. Figure 9 provides an overview of the components in cars that can be made from composite materials.
Figure 9: An overview of the components in cars made from composite materials [5]
FRCs are fundamental materials in marine systems, offering several key benefits. They can improve the hydrodynamic performance of marine vessels and make them more efficient. Additionally, we can utilize them to create durable and corrosion-resistant marine structures and vessels. Figure 10 depicts the production of a boat made of composites.
Figure 10: Production of a boat made of composites
Composite materials have numerous applications in the production of dental bridges and prostheses for tooth replacement. This extensive application is primarily due to their sufficient strength and low elastic modulus, similar to natural teeth. This low elastic modulus minimizes stress generation and makes prostheses more resistant. Figure 11 illustrates a dental bridge made of composites.
Figure 11: A dental bridge made of composite [6]
Composites have numerous other applications in the medical field, including the production of orthopedic prostheses and metal-free fracture fixation devices. You can discover many more applications in medicine and other fields through a simple online search.
5. How FRCs are made?
Two commonly used methods for creating FRCs are prepreg and Resin Transfer Molding (RTM). Both methods involve combining fibers and the matrix under pressure and stress to form a stable composite. In the RTM method, dry fibers are placed in the mold. Then, the resin is injected into the mold under a vacuum to saturate the voids between the fibers. Next, the composite is cured with heat and pressure to form the final product. Figure 12 shows the RTM process, schematically.
Figure 12: Schematic representation of the resin transfer molding process [7]
The RTM offers several advantages compared to the prepreg lamination method. It is more cost-effective due to simpler pre-processing requirements for resin and fibers. Additionally, RTM provides greater flexibility in choosing various combinations of materials. However, careful control of the injection process is essential to prevent air voids and ensure the production of high-quality composites.
Figure 13 shows the prepreg lamination procedure, schematically. As depicted in the figure, in the prepreg method, the fibers are pre-coated with a partially cured resin. This eliminates the need for resin injection during the final curing process. Consequently, the prepreg method guarantees a more uniform resin distribution, leading to higher product quality compared to RTM. However, the pre-coating process can increase the production cost.
Figure 13: Schematic representation of the prepreg lamination process [8]
Note that, regardless of the production method, curing is a crucial stage in composite manufacturing. So, we must perform it carefully to achieve a high-quality composite.
6. What is the composite curing process?
Curing is the process of applying heat and pressure to a composite, causing the matrix to lose its flow ability. The composite curing process must be carefully controlled to achieve the desired performance and quality in the final composite.
Today, two well-established methods are used for the composite curing process: autoclave and oven-curing. In general, oven-curing is a traditional method, that utilizes a standard oven to apply heat to the composite. As depicted in Figure 14, it needs a vacuum bag to apply pressure and remove the air. Despite its lower cost compared to the autoclave method, oven curing results in higher porosity and lower mechanical properties.
Figure 14: Schematic representation of the oven-curing process [9]
The autoclave method is more advanced than the oven-curing. It utilizes a pressure vessel (autoclave) to apply both heat and pressure simultaneously to the composite, as shown in Figure 15. This process enables the production of high-quality laminates with low porosity and superior mechanical properties. However, unlike oven curing, the autoclave method is more expensive and requires complex equipment.
Figure 15: An autoclave device [10]
6.1. How the composite curing process affects the product quality?
During the composite curing process, FRCs experience specific pressure and temperature cycles to achieve optimal quality. However, the standard composite curing process can last several hours, making it inefficient for industrial production. Manufacturers prefer to shorten the curing cycles by applying higher temperatures within shorter time periods. While this approach can increase production speed, it may impact the product quality and lead to residual deformations. Figure 16 showcases a product that experienced residual deformations after the composite curing process.
Figure 16: Schematic representation of the residual deformations in a composite [11]
The traditional approach for balancing production efficiency and quality involves performing several experimental cure cycles for each product. However, the process is both costly and time-consuming. This highlights the challenge of designing optimal cure cycles that ensure both production quality and efficiency. Composite curing simulation is one way to address this challenge.
7. Fiber reinforced composite curing simulation
Numerical methods have simplified the fiber reinforced composite curing simulation. They are valuable alternatives to experimental tests for designing cure cycles. Such methods simplify the process of designing optimal curing cycles that ensure desired product quality while maintaining efficient production. A fiber reinforced composite curing simulation must address the coupled chemical, thermal, and mechanical fields simultaneously. So, it is referred to as the thermo-chemo-mechanical composite curing simulation.
7.1. Simulation of the thermo-chemical reactions in the curing process
During the composite curing simulation, heat originates from two sources: external and internal. Calculating external heat within the composite curing simulation is relatively simple. However, the calculation of internal heat within the composite curing simulation is a challenging task. Internal heat arises from the chemical reactions within the composite during curing. Therefore, we need a thermo-chemical model to account for the internal heat within the composite curing simulation. In such a model, the generated heat is a function of the degree of cure. Note that the degree of cure is a parameter between zero and one, that represents the extent of curing. A value of zero indicates an uncured composite, while a value of one represents a fully cured one. Figure 17 compares the applied temperature and the temperature developed during curing within a composite. The difference represents the internal heat generation, predicted by the composite curing simulation.
Figure 17: Comparison of the applied temperature and the temperature developed in a composite during curing
For a deeper understanding of composite curing simulation, you can explore our learning package “HETVAL subroutine in Abaqus“. It presents the formulations for calculating the internal heat during curing, with a specific focus on the well-known AS4/3501-6 prepreg.
7.2. Evaluation of stress components during the composite curing simulation
Stress prediction is a challenge for the numerical simulation of the composite curing process. This challenge arises due to the changes in the resin’s modulus of elasticity. It makes the composite curing simulation complex. As illustrated in Figure 18, the modulus starts very low and rises significantly during curing as chemical reactions take place. Finally, it reaches a constant value.
Figure 18: Schematic representation of the resin modulus variation during the curing process ([13])
Several models have been proposed to capture the variation of the resin’s modulus during composite curing simulation. The proposed models include linear-elastic, viscoelastic, and path-dependent ones. Each offers advantages and limitations. Table 1 summarizes the models specifically developed for calculating the resin modulus or stress components in the AS4/3501-6 prepreg. You can check this article “Effect of cure cycles on residual stresses in thick composites using multi-physics coupled analysis with multiple constitutive models” for more details on these models. They have simplified the composite curing simulation.
Table 1: An overview of the models for calculating the resin modulus or stress for AS4/3501–6 prepreg [14]
We have provided a detailed description of linear-elastic models and a step-by-step guide for their implementation within the provided package. It simplifies the composite curing simulation. For validation, we compared the results with reference solutions, as shown in Figure 19.
Figure 19: Comparison of the stress in a composite with the reference solution
In summary, numerical composite curing simulation requires the simultaneous consideration of thermal, chemical, and mechanical fields. You might be wondering how to implement such a complex model, but don’t worry! We will guide you through an accurate and efficient method to tackle this challenge.
7.3. Strain evaluation in FRCs during curing
The curing process can result in undesirable deformations in composites, and negatively impact product quality. To minimize these deformations, we should consider the residual strains in a fiber reinforced composite curing simulation.
During the curing process, composites experience two types of strain: mechanical and non-mechanical. The non-mechanical strains in composites originate from both cure shrinkage and thermal expansion. Cure shrinkage arises due to the release of gases and solvents, in the matrix, during the curing process. We can calculate it from the following equation.
In this equation, 
represents the effective chemical shrinkage coefficient of the matrix, and ∆α is the variation in the degree of cure. Figure 20 schematically illustrates how the chemical shrinkage occurs during the curing process.
Figure 20: Illustration of the chemical shrinkage effect during the curing process (Adapted form [12] with modifications)
The thermal expansion depends on both the externally applied heat and the internal heat generated during curing. Since the internal heat depends on the degree of cure, the thermal expansion is also influenced by the chemical reactions. You can calculate it from the following equation.
Where 
is the thermal expansion coefficient of the composite, and is the variation in its temperature.
In summary, several factors influence the total strain experienced by composites during curing, as detailed in Figure 21.
Figure 21: An overview of the strain components generated in a composite during the curing process
Considering all strain components together in a fiber reinforced composite curing simulation can be challenging. However, the “Curing process simulation in Abaqus” learning package on our website simplifies this process. It offers a step-by-step guide on calculating strain components during composite curing simulation. For validation, we compared our results with a reference solution, as shown in Figure 22.
Figure 22: Comparison of the total strain in the composite with the reference solution
8. Abaqus curing process simulation
Abaqus is a widely used finite element program, that has simplified the fiber reinforced composite curing simulation. It has been extensively used in published papers to analyze internal heat generation and mechanical fields during the composite curing process. However, the lack of required thermo-chemo-mechanical models in Abaqus presents a significant challenge for Abaqus curing process simulation. Fortunately, Abaqus user-defined subroutines provide a powerful solution to overcome this challenge.
9. Composite curing simulation using subroutines
Have you ever heard of composite curing simulation using subroutines? Abaqus has a large number of user-defined subroutines with diverse functionalities. You need to utilize several subroutines simultaneously for the Abaqus curing process simulation. All the necessary subroutines and their specific functionalities are detailed in Figure 23.
Figure 23: Necessary subroutines for curing simulation in Abaqus
9.1. USDFLD subroutine
USDFLD is a subroutine that enables us to define user-defined field variables in Abaqus. You can use USDFLD to calculate the degree of cure and its variation with respect to time, for the composite curing simulation. The subroutine enables us to save these parameters as solution-dependent variables (SDVs). These SDVs can be called by other subroutines to calculate internal heat, non-mechanical strains, and stress components. The subroutine’s interface is shown in Figure 24.
Figure 24: The user interface for the USDFLD subroutine
For further details on the USDFLD subroutine, you can refer to the learning package “Introduction to USDFLD and VUSDFLD Subroutine“ on our website.
9.2. UEXPAN subroutine
UEXPAN is another Abaqus subroutine that enables us to calculate non-mechanical strains during the composite curing process. The subroutine’s interface is presented in Figure 25.
Figure 25: The user interface for the UEXPAN subroutine
Within UEXPAN, you can call state variables like the degree of cure to calculate cure shrinkage strains. Moreover, you can obtain the current temperature to calculate thermal expansion. For a detailed explanation of this subroutine, refer to the learning package “UEXPAN and VUEXPAN Subroutine” on our website.
9.3. UMAT subroutine
UMAT is a subroutine that allows users to define their desired material properties, particularly for models not available in the Abaqus library. It enables us to calculate the resin’s density as a function of the degree of cure, for the composite curing simulation. UMAT ultimately returns the calculated stress components to Abaqus for further calculations. The subroutine’s interface is shown in Figure 26.
Figure 26: The user interface for the UMAT subroutine
For a basic introduction to writing UMAT subroutines, refer to this free tutorial “UMAT subroutine free tutorial“. Additionally, a more detailed tutorial with a step-by-step guide is offered for those interested in advanced applications in “UMAT subroutine introduction“.
9.4. HETVAL subroutine
HETVAL, another Abaqus subroutine, allows for calculating internal heat generation during the composite curing process. It enables the user to define the thermo-chemical model and calculate the heat generated due to chemical reactions. The subroutine retrieves the degree of cure and its derivative with respect to time from user-defined state variables, for the composite curing simulation. With this information, the subroutine calculates the internal heat and transfers it to Abaqus CAE for the solution process. The subroutine’s interface is shown in Figure 27.
Figure 27: The user interface for the HETVAL subroutine
We recommend checking out this tutorial “HETVAL subroutine in Abaqus” on our website which shows how to write the HETVAL subroutine for different scenarios.
9.5. DISP subroutine
DISP is a subroutine that allows you to define complex boundary conditions. While Abaqus offers built-in features for defining boundary conditions for composite curing simulation, DISP provides more flexibility and control. So, the subroutine is useful for simulating the curing process under complex temperature cycles. Figure 28 presents the subroutine’s interface.
Figure 28: The user interface for the DISP subroutine
For more information on this subroutine, we recommend checking the provided learning package “DISP and VDISP subroutines in Abaqus“.
10. A learning package for the simulation of the curing process in Abaqus
Utilizing the mentioned subroutines to simulate the curing process is challenging, especially for those unfamiliar with the Fortran programming language. Moreover, defining the complex thermo-chemo-mechanical equations within the subroutines increases this difficulty. However, we have simplified the learning experience to help you overcome these challenges.
In the provided learning package “Composite Curing simulation“, you can gain a comprehensive understanding of the basics of fiber reinforced composite curing simulation using subroutines. Additionally, it helps you become familiar with a well-known thermo-chemo-mechanical model for fiber reinforced composite curing simulation in AS4/3501-6 prepreg. The tutorial provides a step-by-step guide for you to write all the mentioned subroutines and the Abaqus curing process simulation. For validation, we have compared the results of the composite curing simulation with those from the following papers. They have discussed the numerical modeling of the composite curing process in detail.
- Numerical Simulation and Multi-objective Optimization for Curing Process of Thermosetting Prepreg
- Effect of cure cycles on residual stresses in thick composites using multi-physics coupled analysis with multiple constitutive models
11. Summary
This article focused on the simulation of the composite curing process in Abaqus, particularly for fiber-reinforced composites (FRCs). The importance of understanding and optimizing this process lies in its direct impact on the quality, strength, and durability of composite materials, which are critical for applications in aerospace, automotive, and other high-performance industries.
The article began by discussing the nature of FRCs, their types, and the methods used to produce them. It then highlighted the advantages of FRCs over traditional materials and their broad applications. The article outlined the curing process, comparing oven-curing and autoclave methods, and emphasized the need for accurate simulations to optimize this process. The complexity of composite curing simulation was explored, detailing the thermo-chemo-mechanical aspects that need to be addressed. Finally, the article discussed the use of Abaqus subroutines to perform these simulations, specifically USDFLD, UEXPAN, UMAT, HETVAL, and DISP, which allow for detailed control and modeling of the curing process.
In conclusion, this article provided a comprehensive guide on simulating the composite curing process using Abaqus, covering essential methods, challenges, and tools required for accurate and efficient simulation. Through the use of specific subroutines, the article demonstrated how to achieve precise control over the curing process, ensuring the production of high-quality composites.
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