# Feasibility of Reprocessing Natural Fiber Filled Poly(lactic acid) Composites: An In-Depth Investigation

Authors: Sujal Bhattacharjee; Dilpreet S. Bajwa
Journal: Advances in Materials Science and Engineering
 (2017)

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## Abstract

Poly(lactic acid) (PLA) based composites are biodegradable; their disposal after single use may be needless and uneconomical. Prodigal disposal of these composites could also create an environmental concern and additional demand for biobased feedstock. Under these circumstances, recycling could be an effective solution, since it will widen the composite service life and prevent the excessive use of natural resources. This research investigates an in-depth impact of recycling on the mechanical and thermomechanical properties of oak wood flour based PLA composites. Two composite formulations (30 and 50 wt% filler), each with 3 wt% coupling agent (PLA-g-MA), were produced and reprocessed six times by extrusion followed by injection molding. Measurements of fiber length and molecular weight of polymer were, respectively, carried out by gel permeation chromatography (GPC). Scanning electron microscopy (SEM), differential scanning calorimetry (DSC), thermogravimetric analysis (TGA), and Fourier transform infrared spectroscopy (FTIR) tools were used to study morphological and molecular alterations. With consecutive recycling, PLA composites showed a gradual decrease in strength and stiffness properties and an increase in strain properties. The 50% and 30% filler concentration of fibers in the composite showed an abrupt decrease in strength properties after six and two reprocessing cycles, respectively.


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## Body

## 1. Introduction

Currently, biodegradable polymers and their natural fiber composites are preferred to nonbiodegradable plastics and their composites all over the world [1–3]. This is because biodegradable polymers and their natural fiber composites are not only environment friendly but also capable of higher physicomechanical properties. Nonbiodegradable polymers can create huge environmental pollution at the end of their life cycle (by disposal in landfills and incineration); in addition, the petroleum based polymers have limited reserves [4–7]. A widely popular biodegradable polymer polylactic acid (PLA) is an aliphatic thermoplastic polyester generated by polymerization or polycondensation of monomers of lactic acid and these monomers can be produced from natural resources such as sugar, beet, wheat, and corn [7, 8]. PLA has higher strength and stiffness and is regarded as the best of all environment friendly polymers [5]. It has a wide range of application such as in biomedical field (e.g., drug delivery devices, sutures, and scaffolds), electronic field (e.g., portable device housings), automotive industry and construction (e.g., interior panels and indoor furnishing), and disposable items (e.g., packaging, plastic bags, disposable cups and plates, and compostable bottles) [4, 9–13]. However, incorporation of fiber in PLA is desired since the polymer itself is not able to meet all the anticipated properties and is relatively expensive [14]. Wood fiber is an attractive filler due to its cost, availability, biodegradability, and higher specific strength, and stiffness [2, 5, 6, 15]. Therefore, incorporation of wood fiber/filler (WF) in PLA is a logical approach to create an economical and completely biodegradable composite.Unfortunately, PLA and WF based composites have some minor drawbacks. Even though natural fiber reinforced composites have well established commercial market, PLA as matrix resin is yet to be extensively used in commercial engineering applications because of its lower impact resistance, lower softening temperature, higher brittleness, poor moisture resistance, and lower heat deflection temperature [2, 8, 16–18]. The manufacturing cost of PLA is comparatively higher, and the profitability of manufacturing has not yet been established strongly enough to be trusted [14]. Similarly, WF also has some shortcomings such as lower bulk density, higher heat sensitivity, and its hygroscopic nature [2]. Nonuniform dispersion of filler can result in less stress transfer from the matrix to fiber and can reduce the load carrying capacity of the composite [15]. Nevertheless, despite these challenges, the use of WF as filler in PLA is increasing globally primarily because of their biodegradability and higher specific properties [5].With increased demand for WF-PLA composites what concerns is their premature disposal after single use. From a rational point of view, disposal of these WPCs after single use could produce a huge amount of waste material, which is unnecessary and uneconomic. Additionally, this extravagant disposal would create more demand for PLA resulting in greater demand for biobased feedstocks. To overcome this situation, reprocessing or recycling could serve as a competent alternative. Reprocessing would enhance the life cycle (service life) of composites and reduce the consumption of the renewable natural resources. As a result, it will have a positive impact on the environment and could improve the economics of PLA based composites.Some research has been done to investigate the potential of reprocessing PLA based composites [1, 2, 15]. However, most of the research has focused on understanding the impact of blending recycled and virgin PLA polymers and its impact on physicomechanical properties. The studies found that mechanical properties of the composites initially remained constant and then started decreasing with increase in recycled content or number of reprocessing cycles. The degradation was mainly attributed to fiber length reduction and polymer degradation [1, 15, 19].The aim of this research is to understand the impact of reprocessing on the mechanical and thermomechanical properties of oak wood flour (WF) filled PLA composites. Two PLA based composite formulations with 30 or 50 wt% wood filler, 3 wt% coupling agent were selected and successively reprocessed six times by extrusion. After each extrusion cycle, test samples were prepared from composite pellets by injection molding.


## 2. Materials and Methods

### 2.1. Materials

Oak wood flour was obtained from Southern Wood Services, GA, USA. The particle size distribution of wood flour is shown in Table1. The initial moisture content of wood flour was 5.5% as measured by using a moisture analyzer (Computrac, Model MAX 4000XL, AZ, USA). PLA (Ingeo Biopolymer 2003D) was obtained from NatureWorks LLC, MN, USA. The polymer has a MFI of 6 g/10 min (210°C, 2.16 Kg), specific gravity of 1.24, and heat deflection temperature of 55°C. Coupling agent PLA grafted maleic anhydride (MA) was manufactured in the laboratory using MA and PLA through extrusion process. Maleic anhydride (2,5-furandione) with molecular weight 98.06 and purity greater than 99% was purchased from Sigma Aldrich (St. Louis, MO, USA).Table 1
Particle size distribution of oak wood flour.
Wood particle size (mm)
Range (%)
0.841
0–5%
0.595
5–15%
0.400
35–42%
0.250
40–50%
0.177
6–9%
0.149
0-1%
<0.149
0–2%


### 2.2. Methods

#### 2.2.1. Composite Preparation

Two PLA composite formulations with 30 and 50 wt% wood flour each and 3 wt% PLA-g-MA were manufactured and then individually recycled six times by extrusion. Before extrusion, WF, PLA-g-MA, and PLA were dried in an oven at 80°C for 24 hours. The moisture content of dried wood flour and PLA before processing was below 0.5%. The dried materials were manually blended and extruded into pellets using a twin screw corotating extruder (Leistritz Micro 18 GL 40 D, NJ, USA) with seven heating zones. The temperature profile of these zones (from feed section to melting section) was controlled at 157°C, 180°C, 190°C, 200°C, 200°C, 202°C, and 205°C, respectively. Temperature of strand die and the gate adapter was maintained at 205°C and extruder screw speed at 200 rpm. Extruded composite strands were cooled down using a water bath and then pelletized. A portion of composite pellets were dried at 80°C and injection-molded using single-screw injection molder (Model SIM- 5080, Technoplas Inc., OH, USA) to make test samples of “cycle 0” or “virgin” composite material.The rest of the dried virgin composite pellets were again extruded under the same processing conditions and injection-molded to make test samples of “cycle 1” or “first time recycled” composite. This process was repeated five times to derive test samples representing six reprocessing cycles. All the test samples were conditioned at room temperature (25°C) before testing. The annotations for 30 wt% filler and 50 wt% filler composites are as “WF 30 PLA” and “WF 50 PLA” composites, respectively.


#### 2.2.2. Tensile Testing

Tensile test was performed with a universal testing machine Instron (Model 5567, MA, USA) according to ASTM D 638: standard test method for tensile properties of plastics. A 30 KN load cell and strain rate of 5 mm/min were used in the test.


#### 2.2.3. Flexural Testing

Flexural test was conducted using an universal testing machine (Instron Model 5567, MA, USA) with a load cell of 2 KN, according to ASTM D 790: standard test methods for flexural properties of unreinforced and reinforced plastics and electrical insulating materials. The crosshead speed was set at 1.4 mm/min. The sample dimensions were 75 mm× 12.9 mm × 3.3 mm with a support span of 53 mm.


#### 2.2.4. Coefficient of Thermal Expansion (CTE)

The coefficient of thermal expansion was performed by using a dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) with the aid of a tension film clamp. The sample dimensions were 38.1 mm× 12.9 mm × 3.3 mm where the initial length was 12.74 mm. Eight samples, for each cycle, were conditioned at room temperature and then tested from 30°C to 50°C with a ramp rate of 3°C /min. CTE was measured by using the following equation [22]:(1)α=ΔLΔT·1L.Here, α is the coefficient of thermal expansion, ΔL is the change in length, ΔT is the change in temperature, and L is the initial length (12.74 mm).


#### 2.2.5. Heat Deflection Temperature (HDT)

Heat deflection temperature was determined by using a dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) according to ASTM D 648: standard test method for deflection temperature of plastics under flexural load in the edgewise position (pressureδ = 0.455 MPa). Sample dimensions were 65.0 mm × 12.9 mm × 3.3 mm and the supported length was 50 mm. The temperature ramp rate was 3°C/min.


#### 2.2.6. Dynamic Mechanical Analysis

Storage modulus was determined by using the dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) with a dual cantilever beam clamp at 30°C. The soak time was 5 minutes (at 28°C) and the ramp rate was 3°C /min. The frequency was 1 Hz and the amplitude was 15μm. Test sample dimensions were 65 mm × 12.9 mm × 3.3 mm (supported length 41.6 mm).


#### 2.2.7. Izod Impact Test

Izod impact test (notched) was conducted by using an izod impact tester (Tinius Olsen, Model Impact 104, PA, USA) according to ASTM D 256: standard test method for determining the izod pendulum impact resistance of plastics. No additional load was added to the pendulum. Test sample dimensions were 63.5 mm× 12.9 mm × 3.3 mm with a 2 mm notch being made in the middle of the sample.


#### 2.2.8. Melt Flow Index (MFI)

Melt flow index was measured by using an extrusion plastometer (Tinius Olsen, Model MP 600, PA, USA) according to ASTM D 1238: standard test method for melt flow rates of thermoplastics by extrusion plastometer. The applied temperature and load were 190°C and 2.16 Kg, respectively.


#### 2.2.9. Scanning Electron Microscopy (SEM)

SEM test samples were obtained from the fracture surfaces of tensile specimens. These fracture surfaces were covered with a conductive gold-palladium layer by using a Balzers SCD 030 sputter coater (BAL-TEC RMC, Tucson, AZ, USA). Coated samples were then tested by using a JEOL JSM-6490LV scanning electron microscope (JEOL USA, Peabody, MA, USA). The accelerating voltage was 15 KeV.


#### 2.2.10. Fiber Length Measurement

Wood fiber length of composites was measured by dissolving the polymer in acetone at 130°C, with constant stirring for two hours. After the polymer dissolved, the wood fibers settled at the bottom of the container. Wood fibers were then separated from the solution and dried in an oven at 105°C for 12 h. A Zeiss microscope (Axiovart 40 Mat) was used to evaluate 100 fiber lengths.


#### 2.2.11. Differential Scanning Calorimetry (DSC)

DSC was performed by using a TA instrument (DSC, Q1000, DE, USA) from −10°C to 240°C with a nitrogen flow rate of 50 ml/min. The heating or ramp rate was 10°C/min. Each sample weighed approximately 10 mg.


#### 2.2.12. Thermogravimetric Analysis (TGA)

TGA was accomplished by using a TA instrument (TGA, Q500, DE, USA) using temperature range from 25°C to 800°C in air as a sample gas (flow rate 60 ml/min) and nitrogen as a balance gas (flow rate 40 ml/min). The heating rate was controlled at 10°C/min. Each sample weighed approximately 10 mg.


#### 2.2.13. Fourier Transform Infrared Spectroscopy (FTIR)

A Thermo Scientific Nicolet 8700 spectrometer was used to perform FTIR. The test was done in photoacoustic mode and in the range of 700–3500 cm−1. All the samples had an approximate thickness of 0.5 mm. FTIR data analysis was done by using OMNIC spectra software.


#### 2.2.14. Gel Permeation Chromatography (GPC)

The acetone solution containing dissolved PLA produced in Section2.2.10 was used for GPC. The acetone solution containing PLA was exposed in the open air at room temperature (25°C) to obtain dried PLA. Dried PLA was then dissolved in tetrahydrofuran (THF) to make another solution (concentration 2 mg/ml). This solution was used in a GPC apparatus (EcoSEC HLC-8320GPC, Tosoh Bioscience, Japan) with an injection volume of 20 μl (at 40°C) and an eluent (THF) flow rate of 0.4 ml/min. Two columns (TSKgel SuperHM-L 6.00 mm ID × 15 cm) and a differential refractometer detector (DRI) were also used with the GPC apparatus, to measure the molecular weight of PLA.


#### 2.2.15. Statistical Analysis

Statistical analysis was conducted on the data of mechanical and thermomechanical tests with a confidence level of 95% by using Minitab 17 (Minitab, PA, USA). The mean comparison of different samples was conducted using Tukey’s test. Means with different alphabet show significant difference in the properties. Eight replicates from each cycle were tested for all the mechanical properties and five replicates for melt flow index.


## 2.1. Materials

Oak wood flour was obtained from Southern Wood Services, GA, USA. The particle size distribution of wood flour is shown in Table1. The initial moisture content of wood flour was 5.5% as measured by using a moisture analyzer (Computrac, Model MAX 4000XL, AZ, USA). PLA (Ingeo Biopolymer 2003D) was obtained from NatureWorks LLC, MN, USA. The polymer has a MFI of 6 g/10 min (210°C, 2.16 Kg), specific gravity of 1.24, and heat deflection temperature of 55°C. Coupling agent PLA grafted maleic anhydride (MA) was manufactured in the laboratory using MA and PLA through extrusion process. Maleic anhydride (2,5-furandione) with molecular weight 98.06 and purity greater than 99% was purchased from Sigma Aldrich (St. Louis, MO, USA).Table 1
Particle size distribution of oak wood flour.
Wood particle size (mm)
Range (%)
0.841
0–5%
0.595
5–15%
0.400
35–42%
0.250
40–50%
0.177
6–9%
0.149
0-1%
<0.149
0–2%


## 2.2. Methods

### 2.2.1. Composite Preparation

Two PLA composite formulations with 30 and 50 wt% wood flour each and 3 wt% PLA-g-MA were manufactured and then individually recycled six times by extrusion. Before extrusion, WF, PLA-g-MA, and PLA were dried in an oven at 80°C for 24 hours. The moisture content of dried wood flour and PLA before processing was below 0.5%. The dried materials were manually blended and extruded into pellets using a twin screw corotating extruder (Leistritz Micro 18 GL 40 D, NJ, USA) with seven heating zones. The temperature profile of these zones (from feed section to melting section) was controlled at 157°C, 180°C, 190°C, 200°C, 200°C, 202°C, and 205°C, respectively. Temperature of strand die and the gate adapter was maintained at 205°C and extruder screw speed at 200 rpm. Extruded composite strands were cooled down using a water bath and then pelletized. A portion of composite pellets were dried at 80°C and injection-molded using single-screw injection molder (Model SIM- 5080, Technoplas Inc., OH, USA) to make test samples of “cycle 0” or “virgin” composite material.The rest of the dried virgin composite pellets were again extruded under the same processing conditions and injection-molded to make test samples of “cycle 1” or “first time recycled” composite. This process was repeated five times to derive test samples representing six reprocessing cycles. All the test samples were conditioned at room temperature (25°C) before testing. The annotations for 30 wt% filler and 50 wt% filler composites are as “WF 30 PLA” and “WF 50 PLA” composites, respectively.


### 2.2.2. Tensile Testing

Tensile test was performed with a universal testing machine Instron (Model 5567, MA, USA) according to ASTM D 638: standard test method for tensile properties of plastics. A 30 KN load cell and strain rate of 5 mm/min were used in the test.


### 2.2.3. Flexural Testing

Flexural test was conducted using an universal testing machine (Instron Model 5567, MA, USA) with a load cell of 2 KN, according to ASTM D 790: standard test methods for flexural properties of unreinforced and reinforced plastics and electrical insulating materials. The crosshead speed was set at 1.4 mm/min. The sample dimensions were 75 mm× 12.9 mm × 3.3 mm with a support span of 53 mm.


### 2.2.4. Coefficient of Thermal Expansion (CTE)

The coefficient of thermal expansion was performed by using a dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) with the aid of a tension film clamp. The sample dimensions were 38.1 mm× 12.9 mm × 3.3 mm where the initial length was 12.74 mm. Eight samples, for each cycle, were conditioned at room temperature and then tested from 30°C to 50°C with a ramp rate of 3°C /min. CTE was measured by using the following equation [22]:(1)α=ΔLΔT·1L.Here, α is the coefficient of thermal expansion, ΔL is the change in length, ΔT is the change in temperature, and L is the initial length (12.74 mm).


### 2.2.5. Heat Deflection Temperature (HDT)

Heat deflection temperature was determined by using a dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) according to ASTM D 648: standard test method for deflection temperature of plastics under flexural load in the edgewise position (pressureδ = 0.455 MPa). Sample dimensions were 65.0 mm × 12.9 mm × 3.3 mm and the supported length was 50 mm. The temperature ramp rate was 3°C/min.


### 2.2.6. Dynamic Mechanical Analysis

Storage modulus was determined by using the dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) with a dual cantilever beam clamp at 30°C. The soak time was 5 minutes (at 28°C) and the ramp rate was 3°C /min. The frequency was 1 Hz and the amplitude was 15μm. Test sample dimensions were 65 mm × 12.9 mm × 3.3 mm (supported length 41.6 mm).


### 2.2.7. Izod Impact Test

Izod impact test (notched) was conducted by using an izod impact tester (Tinius Olsen, Model Impact 104, PA, USA) according to ASTM D 256: standard test method for determining the izod pendulum impact resistance of plastics. No additional load was added to the pendulum. Test sample dimensions were 63.5 mm× 12.9 mm × 3.3 mm with a 2 mm notch being made in the middle of the sample.


### 2.2.8. Melt Flow Index (MFI)

Melt flow index was measured by using an extrusion plastometer (Tinius Olsen, Model MP 600, PA, USA) according to ASTM D 1238: standard test method for melt flow rates of thermoplastics by extrusion plastometer. The applied temperature and load were 190°C and 2.16 Kg, respectively.


### 2.2.9. Scanning Electron Microscopy (SEM)

SEM test samples were obtained from the fracture surfaces of tensile specimens. These fracture surfaces were covered with a conductive gold-palladium layer by using a Balzers SCD 030 sputter coater (BAL-TEC RMC, Tucson, AZ, USA). Coated samples were then tested by using a JEOL JSM-6490LV scanning electron microscope (JEOL USA, Peabody, MA, USA). The accelerating voltage was 15 KeV.


### 2.2.10. Fiber Length Measurement

Wood fiber length of composites was measured by dissolving the polymer in acetone at 130°C, with constant stirring for two hours. After the polymer dissolved, the wood fibers settled at the bottom of the container. Wood fibers were then separated from the solution and dried in an oven at 105°C for 12 h. A Zeiss microscope (Axiovart 40 Mat) was used to evaluate 100 fiber lengths.


### 2.2.11. Differential Scanning Calorimetry (DSC)

DSC was performed by using a TA instrument (DSC, Q1000, DE, USA) from −10°C to 240°C with a nitrogen flow rate of 50 ml/min. The heating or ramp rate was 10°C/min. Each sample weighed approximately 10 mg.


### 2.2.12. Thermogravimetric Analysis (TGA)

TGA was accomplished by using a TA instrument (TGA, Q500, DE, USA) using temperature range from 25°C to 800°C in air as a sample gas (flow rate 60 ml/min) and nitrogen as a balance gas (flow rate 40 ml/min). The heating rate was controlled at 10°C/min. Each sample weighed approximately 10 mg.


### 2.2.13. Fourier Transform Infrared Spectroscopy (FTIR)

A Thermo Scientific Nicolet 8700 spectrometer was used to perform FTIR. The test was done in photoacoustic mode and in the range of 700–3500 cm−1. All the samples had an approximate thickness of 0.5 mm. FTIR data analysis was done by using OMNIC spectra software.


### 2.2.14. Gel Permeation Chromatography (GPC)

The acetone solution containing dissolved PLA produced in Section2.2.10 was used for GPC. The acetone solution containing PLA was exposed in the open air at room temperature (25°C) to obtain dried PLA. Dried PLA was then dissolved in tetrahydrofuran (THF) to make another solution (concentration 2 mg/ml). This solution was used in a GPC apparatus (EcoSEC HLC-8320GPC, Tosoh Bioscience, Japan) with an injection volume of 20 μl (at 40°C) and an eluent (THF) flow rate of 0.4 ml/min. Two columns (TSKgel SuperHM-L 6.00 mm ID × 15 cm) and a differential refractometer detector (DRI) were also used with the GPC apparatus, to measure the molecular weight of PLA.


### 2.2.15. Statistical Analysis

Statistical analysis was conducted on the data of mechanical and thermomechanical tests with a confidence level of 95% by using Minitab 17 (Minitab, PA, USA). The mean comparison of different samples was conducted using Tukey’s test. Means with different alphabet show significant difference in the properties. Eight replicates from each cycle were tested for all the mechanical properties and five replicates for melt flow index.


## 2.2.1. Composite Preparation

Two PLA composite formulations with 30 and 50 wt% wood flour each and 3 wt% PLA-g-MA were manufactured and then individually recycled six times by extrusion. Before extrusion, WF, PLA-g-MA, and PLA were dried in an oven at 80°C for 24 hours. The moisture content of dried wood flour and PLA before processing was below 0.5%. The dried materials were manually blended and extruded into pellets using a twin screw corotating extruder (Leistritz Micro 18 GL 40 D, NJ, USA) with seven heating zones. The temperature profile of these zones (from feed section to melting section) was controlled at 157°C, 180°C, 190°C, 200°C, 200°C, 202°C, and 205°C, respectively. Temperature of strand die and the gate adapter was maintained at 205°C and extruder screw speed at 200 rpm. Extruded composite strands were cooled down using a water bath and then pelletized. A portion of composite pellets were dried at 80°C and injection-molded using single-screw injection molder (Model SIM- 5080, Technoplas Inc., OH, USA) to make test samples of “cycle 0” or “virgin” composite material.The rest of the dried virgin composite pellets were again extruded under the same processing conditions and injection-molded to make test samples of “cycle 1” or “first time recycled” composite. This process was repeated five times to derive test samples representing six reprocessing cycles. All the test samples were conditioned at room temperature (25°C) before testing. The annotations for 30 wt% filler and 50 wt% filler composites are as “WF 30 PLA” and “WF 50 PLA” composites, respectively.


## 2.2.2. Tensile Testing

Tensile test was performed with a universal testing machine Instron (Model 5567, MA, USA) according to ASTM D 638: standard test method for tensile properties of plastics. A 30 KN load cell and strain rate of 5 mm/min were used in the test.


## 2.2.3. Flexural Testing

Flexural test was conducted using an universal testing machine (Instron Model 5567, MA, USA) with a load cell of 2 KN, according to ASTM D 790: standard test methods for flexural properties of unreinforced and reinforced plastics and electrical insulating materials. The crosshead speed was set at 1.4 mm/min. The sample dimensions were 75 mm× 12.9 mm × 3.3 mm with a support span of 53 mm.


## 2.2.4. Coefficient of Thermal Expansion (CTE)

The coefficient of thermal expansion was performed by using a dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) with the aid of a tension film clamp. The sample dimensions were 38.1 mm× 12.9 mm × 3.3 mm where the initial length was 12.74 mm. Eight samples, for each cycle, were conditioned at room temperature and then tested from 30°C to 50°C with a ramp rate of 3°C /min. CTE was measured by using the following equation [22]:(1)α=ΔLΔT·1L.Here, α is the coefficient of thermal expansion, ΔL is the change in length, ΔT is the change in temperature, and L is the initial length (12.74 mm).


## 2.2.5. Heat Deflection Temperature (HDT)

Heat deflection temperature was determined by using a dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) according to ASTM D 648: standard test method for deflection temperature of plastics under flexural load in the edgewise position (pressureδ = 0.455 MPa). Sample dimensions were 65.0 mm × 12.9 mm × 3.3 mm and the supported length was 50 mm. The temperature ramp rate was 3°C/min.


## 2.2.6. Dynamic Mechanical Analysis

Storage modulus was determined by using the dynamic mechanical analyzer (TA Instruments, DMA Q800, DE, USA) with a dual cantilever beam clamp at 30°C. The soak time was 5 minutes (at 28°C) and the ramp rate was 3°C /min. The frequency was 1 Hz and the amplitude was 15μm. Test sample dimensions were 65 mm × 12.9 mm × 3.3 mm (supported length 41.6 mm).


## 2.2.7. Izod Impact Test

Izod impact test (notched) was conducted by using an izod impact tester (Tinius Olsen, Model Impact 104, PA, USA) according to ASTM D 256: standard test method for determining the izod pendulum impact resistance of plastics. No additional load was added to the pendulum. Test sample dimensions were 63.5 mm× 12.9 mm × 3.3 mm with a 2 mm notch being made in the middle of the sample.


## 2.2.8. Melt Flow Index (MFI)

Melt flow index was measured by using an extrusion plastometer (Tinius Olsen, Model MP 600, PA, USA) according to ASTM D 1238: standard test method for melt flow rates of thermoplastics by extrusion plastometer. The applied temperature and load were 190°C and 2.16 Kg, respectively.


## 2.2.9. Scanning Electron Microscopy (SEM)

SEM test samples were obtained from the fracture surfaces of tensile specimens. These fracture surfaces were covered with a conductive gold-palladium layer by using a Balzers SCD 030 sputter coater (BAL-TEC RMC, Tucson, AZ, USA). Coated samples were then tested by using a JEOL JSM-6490LV scanning electron microscope (JEOL USA, Peabody, MA, USA). The accelerating voltage was 15 KeV.


## 2.2.10. Fiber Length Measurement

Wood fiber length of composites was measured by dissolving the polymer in acetone at 130°C, with constant stirring for two hours. After the polymer dissolved, the wood fibers settled at the bottom of the container. Wood fibers were then separated from the solution and dried in an oven at 105°C for 12 h. A Zeiss microscope (Axiovart 40 Mat) was used to evaluate 100 fiber lengths.


## 2.2.11. Differential Scanning Calorimetry (DSC)

DSC was performed by using a TA instrument (DSC, Q1000, DE, USA) from −10°C to 240°C with a nitrogen flow rate of 50 ml/min. The heating or ramp rate was 10°C/min. Each sample weighed approximately 10 mg.


## 2.2.12. Thermogravimetric Analysis (TGA)

TGA was accomplished by using a TA instrument (TGA, Q500, DE, USA) using temperature range from 25°C to 800°C in air as a sample gas (flow rate 60 ml/min) and nitrogen as a balance gas (flow rate 40 ml/min). The heating rate was controlled at 10°C/min. Each sample weighed approximately 10 mg.


## 2.2.13. Fourier Transform Infrared Spectroscopy (FTIR)

A Thermo Scientific Nicolet 8700 spectrometer was used to perform FTIR. The test was done in photoacoustic mode and in the range of 700–3500 cm−1. All the samples had an approximate thickness of 0.5 mm. FTIR data analysis was done by using OMNIC spectra software.


## 2.2.14. Gel Permeation Chromatography (GPC)

The acetone solution containing dissolved PLA produced in Section2.2.10 was used for GPC. The acetone solution containing PLA was exposed in the open air at room temperature (25°C) to obtain dried PLA. Dried PLA was then dissolved in tetrahydrofuran (THF) to make another solution (concentration 2 mg/ml). This solution was used in a GPC apparatus (EcoSEC HLC-8320GPC, Tosoh Bioscience, Japan) with an injection volume of 20 μl (at 40°C) and an eluent (THF) flow rate of 0.4 ml/min. Two columns (TSKgel SuperHM-L 6.00 mm ID × 15 cm) and a differential refractometer detector (DRI) were also used with the GPC apparatus, to measure the molecular weight of PLA.


## 2.2.15. Statistical Analysis

Statistical analysis was conducted on the data of mechanical and thermomechanical tests with a confidence level of 95% by using Minitab 17 (Minitab, PA, USA). The mean comparison of different samples was conducted using Tukey’s test. Means with different alphabet show significant difference in the properties. Eight replicates from each cycle were tested for all the mechanical properties and five replicates for melt flow index.


## 3. Discussion

### 3.1. Effect of Wood Flour Content on Virgin Composites

Higher WF content (50 wt% filler) increased stiffness properties and tensile and flexural modulus but showed no impact on the tensile and flexural strength. On the contrary, higher filler content decreased composite strain properties. No improvement in the strength properties of composites despite higher filler content can be attributed to poor interfacial adhesion between the fiber and polymer matrix. It is possible that higher filler content could produce fiber agglomeration in the composite matrix resulting in stress concentration, as stress concentration initiates crack propagation which leads to lower composite strength properties [13].Higher filler composite showed increased tensile, flexural, and storage modulus by 950 MPa, 450 MPa, and 450 MPa, respectively, as compared to lower filler (30 wt% filler) composite. This is because the stiffness properties of biocomposites mainly depend on wood flour content [7, 14]. In higher filler composite, higher constrain to polymer chain movement is created, and hence the composite stiffness is increased [2, 9, 14]. As the composite becomes stiffer, it produces more resistance to mechanical or thermal stresses and thus showed a decrease in strain properties.Similarly, heat deflection temperature (HDT) properties showed no response to WF loading levels. This is because lower crystalline polymers, such as PLA, show HDT nearly close to their glass transition temperature, while higher crystalline polymers show HDT around their melting temperature [18]. Higher filler content did not play any role in altering the HDT of lower crystalline polymers [23, 24].


### 3.2. Effect of Recycling on Fiber Length

The fiber length in WF 30 PLA and WF 50 PLA composites decreased with successive reprocessing. At cycle 0 and cycle 6, the average fiber lengths were, respectively, 253.24μm and 111.15 μm, which are noticeably lower than the fiber length of original wood flour (Table 1 and Figure 1). This could be due to two probable reasons, lower MFI of PLA (6 g/10 min) and higher screw rpm of the extruder (200 rev/min), both of which can lead to higher shear stress during extrusion which can result in high attrition causing lower average fiber length in the PLA composite. The results are in agreement with previously reported results [1, 22]. Figure 2 shows the normal distribution of fiber lengths of the composite at cycle 0 and cycle 6.Figure 1
Fibers of WF 30 PLA composite at (a) cycle 0 and (b) cycle 6 (magnification 10x).
(a)
(b)Figure 2
Normal distribution plot of fiber length of WF 30 PLA composite at cycle 0 and cycle 6.


### 3.3. Effect of Recycling on Molecular Weight of PLA

Table2 shows the average molecular weights of WF 30 PLA composite at cycle 0 and cycle 6. Both types of molecular weights, weight averaged (Mw) and number averaged (Mn), showed a decrease with successive recycling. These results agree with the work of other researchers [25]. The polydispersity index (PDI) showed an increase with increased number of reprocessing cycles. This increase in PDI also implies a decrease in molecular weights of PLA [26]. This could be attributed to the breakage of polymer chains due to thermal degradation. Recycling of polymer leads to decrease in Mn resulting in higher PDI.Table 2
Fiber length and molecular weight of WF 30 PLA composite at cycle 0 and cycle 6.
Property
Cycle 0
Cycle 6
Average fiber length (μm)
253.24
111.15
M
w (g/mole)
151,115
81,958
M
n (g/mole)
133,762
50,742
Polydispersity index (PDI)
1.13
1.62


### 3.4. Effect of Recycling on Composite Strength Properties

Strength properties of WF 30 PLA composite (tensile strength, flexural strength, and impact strength) decreased sharply at cycle 6, while they did not exhibit any shift in the previous cycles (Table3). Strength properties of biocomposites primarily depend on fiber length (or aspect ratio), fiber content, void content, interfacial adhesion, and molecular weight of polymer. In this case, fiber length and molecular weight of polymer possibly decreased by a greater extent at cycle 6 than the previous cycles. In addition, crack propagation and fiber pull-outs are observed at cycle 6 that indicate lower interfacial adhesion between the fiber and matrix (Figures 3(a) and 3(b)). This lower interfacial adhesion, attributable to repeated heat and shear stress history due to extrusion, probably results in lower strength properties of the composite [1].Table 3
Physical and mechanical properties of WF-PLA composites after six reprocessing cycles.
(a)
Composite with 30% wood flour
Properties
WF 30 PLA
Cycle 0
Cycle 1
Cycle 2
Cycle 3
Cycle 4
Cycle 5
Cycle 6
Tensile strength (MPa)
55.46 (2.96)AB
55.89(0.73)A
56.55 (0.68)A
53.73 (1.53)AB
52.54 (1.49)BC
50.58 (1.52)C
29.21 (3.23)D
Flexural strength (MPa)
90.96 (2.54)A
89.23 (2.21)A
87.06 (2.72)A
86.70 (2.70)A
87.40 (2.08)A
81.07 (2.94)B
26.81 (3.93)C
Impact resistance (J/m)
47.18 (5.48)A
45.56 (9.62)A
35.36 (6.09)B
34.90 (6.05)B
34.51 (4.45)B
28.91 (7.17)B
13.13 (3.73)C
Tensile modulus (MPa)
6949.95 (332)A
6361.13 (267.86)AB
6484.70 (490.03)AB
6185.56 (792.19)AB
6533.57 (594.27)AB
5978.74 (541.50)B
6303.36 (759.82)AB
Flexural modulus (MPa)
5811.89 (273.48)A
5424.19 (138.78)B
5368.78 (81.01)B
5288.02 (205.17)B
5347.51 (144.87)B
5256.00 (94.96)B
4163.17 (74.57)C
Storage modulus (MPa)
6405.88 (303.48)A
6179.75 (88.9)ABC
6237.50 (144.73)AB
6365.25 (101.37)A
5927.38 (302.9)BCD
5844.25 (274.45)CD
5721.88 (271.06)D
Heat deflection temperature (°C)
56.78 (0.39)A
56.58 (0.27)A
56.73 (0.21)A
56.52 (0.10)A
56.65 (0.24)A
56.15 (0.63)A
54.83 (0.26)B
Failure strain (%)
1.59 (0.27)B
2.05 (0.10)A
2.32 (0.05)A
2.19 (0.25)A
2.20 (0.18)A
2.21 (0.22)A
0.46 (0.05)C
Coefficient of thermal expansion (mm/mm/°C)× 10−5
0.68 (0.31)D
1.22 (0.23)BC
1.31 (0.22)BC
1.19 (0.25)C
1.63 (0.46)ABC
1.69 (0.24)AB
1.90 (0.33)A
Melt flow index (g/10 min)
2.85 (0.26)F
6.45 (0.20)E
7.84 (0.59)D
12.00 (0.36)C
14.26 (0.92)B
14.62 (0.50)B
21.09 (0.13)A
(b)
Composite with 50% wood flour
Properties
WF 50 PLA
Cycle 0
Cycle 1
Cycle 2
Cycle 3
Cycle 4
Cycle 5
Cycle 6
Tensile strength (MPa)
53.98 (3.61)A
53.20 (2.90)A
32.78 (5.17)B
36.84 (6.19)B
27.86 (6.08)B
34.34 (8.15)B
31.38 (9.56)B
Flexural strength (MPa)
91.24 (5.81)A
92.16 (2.71)A
28.57 (1.45)C
36.63 (8.83)B
31.74 (3.73)BC
30.74 (1.87)BC
27.26 (2.16)C
Impact resistance (J/m)
31.32 (6.13)A
31.33 (3.65)A
22.06 (5.46)B
20.48 (6.19)B
18.93 (4.90)B
15.71 (5.45)B
18.76 (4.15)B
Tensile modulus (MPa)
8487.95 (698.60)A
8847.76 (894.24)A
6925.42 (1428.47)AB
5251.07 (1326)BCD
6156.28 (2333.36)BC
4660.82 (1572.32)CD
3907.93 (725.54)D
Flexural modulus (MPa)
6685.00 (480.84)AB
5936.28 (547.61)C
6582.87 (440.04)AB
6850.69 (243.49)A
6713.83 (104.07)AB
6428.03 (293.98)ABC
6284.67 (135.05)BC
Storage modulus (MPa)
7347.88 (498.78)A
7286.13 (476.55)A
7060.13 (825.99)AB
7391 (199.80)A
7106.13 (653.38)AB
6622.25 (589.05)AB
6317.00 (288.40)B
Heat deflection temperature (°C)
56.07 (0.33)A
55.71 (0.59)AB
54.49 (0.43)D
54.58 (0.33)D
54.71 (0.33)CD
55.18 (0.28)BC
54.62 (0.20)CD
Failure strain (%)
1.41 (0.15)AB
1.26 (0.18)B
1.31 (0.52)B
1.84 (0.43)AB
1.41 (0.24)AB
1.93 (0.45)A
1.83 (0.55)AB
Coefficient of thermal expansion (mm/mm/°C)× 10−5
1.29 (0.48)A
0.91 (0.54)AB
0.49 (0.15)B
0.57 (0.23)B
0.54 (0.17)B
0.64 (0.21)B
0.76 (0.19)B
Melt flow index (g/10 min)
2.50 (0.21)F
3.15 (0.12)EF
15.34 (0.99)E
25.09 (0.55)D
28.85 (0.59)C
32.73 (0.56)B
36.67 (0.58)A
Values are shown as the mean with standard deviation in parenthesis. Means with different letters are significantly different (P<0.05).Figure 3
SEM of WF-PLA composite at (a) cycle 0 (WF 30 PLA), (b) cycle 6 (WF 30 PLA), and (c) cycle 2 (WF 50 PLA).
(a)
(b)
(c)On the contrary, strength properties of WF 50 PLA composite decreased vastly after cycle 2 and then became somewhat constant up to cycle 6 (Tables3(a) and 3(b)). This could be due to the higher degradation in fiber and polymer, coupled with lower interfacial adhesion due to higher filler content at cycle 2. Microvoids were also observed in the composite matrix at cycle 2 (Figure 3) that could significantly contribute towards lower strength properties. Strength properties of composites were almost constant from cycle 2 to cycle 6, as the number of pores at cycle 2 and cycle 6 remained equivalent.The sudden change in strength properties for WF 50 PLA at cycle 2 can be related to higher amount of shear stress during extrusion as well as inherent moisture content due to higher amount of wood flour. It is reported that PLA is highly sensitive to shear stress and moisture, which can lead to a rapid decrease in strength properties in highly filled composites [1].


### 3.5. Effect of Recycling on Composite Stiffness Properties

Composite stiffness properties experimented in this study include tensile modulus, flexural modulus, storage modulus, and heat deflection temperature (HDT). All these properties showed a gradual decrease with increasing number of reprocessing cycles for both composites (Tables3(a) and 3(b)). This may be due to the less efficient stress transfer from the matrix to fiber, that is, caused by (1) fiber and polymer degradation, (2) increased number of microvoids, (3) less polymer chain entanglement by fibers, and (4) poor fiber-matrix interfacial adhesion with successive recycling [22, 27].Overall, most stiffness properties showed minor decrease, from cycle 0 to cycle 6 for both formulations of composites, as compared to the corresponding strength properties (Tables3(a) and 3(b)). For example, after reprocessing six times, flexural modulus for higher and lower filler composite decreased by 6% and 28%, respectively, while both flexural strengths decreased approximately 70% (Table 4). As mentioned earlier (Section 3.1), fiber content is the most important parameter to determine stiffness properties of biocomposites [7, 14]. Since the fiber content was constant for each formulation during reprocessing, the amount of polymer chain entanglement decreased less, which contributed to decrease in composite stiffness properties. These findings are consistent with the findings of other research workers [1, 22].Table 4
Relative difference in means of properties of WF/PLA composites between cycle 0 and cycle 6.
Properties
WF 30 PLA composite (%)
WF 50 PLA composite (%)
Tensile strength (MPa)
−47.34
−41.86
Tensile modulus (MPa)
−9.30
−53.96
Failure strain (%)
−71.22
29.20
Flexural strength (MPa)
−70.53
−70.12
Flexural modulus (MPa)
−28.37
−5.99
Impact resistance (J/m)
−72.18
−40.10
Heat deflection temperature (°C)
−3.43
−2.58
Storage modulus (MPa)
−10.68
−14.03
Coefficient of thermal expansion (mm/mm/°C)
175.94
−40.93
Melt flow index (g/10 min)
640.37
1364.60
Negative sign shows a decrease and a positive one shows an increase in the value of the property.The tensile modulus of WF 50 PLA composites from cycle 0 and cycle 6 showed a much higher decrease (54%) than the corresponding flexural modulus (6%) (Tables3(a) and 3(b)). The difference in the property values could be due to the difference in testing methods since tensile test is thickness dependent and flexural test is surface property dependent [19].


### 3.6. Effect of Recycling on Composite Strain Properties

The impact of reprocessing was investigated on the thermomechanical strain properties of composites such as failure strain, coefficient of thermal expansion (CTE), and melt flow index (MFI). For both composites, most of these strain properties showed an increase with repetitive extrusion cycles (Tables3(a) and 3(b)). This increase in composite strain is caused by the same factors (or change in factors) that have reduced composite stiffness with successive recycling (Section 3.5).However, for WF 30 PLA composite, although CTE increased with consecutive recycling, failure strain first increased from cycle 0 to cycle 5 but then sharply decreased at cycle 6 (Table3(a)). This could be attributed to the fact that failure strain was measured with a tensile load while CTE was measured with no preload force and is temperature dependent. At cycle 6, the composite may have degraded to the extent that it could not withstand higher load (Table 3(a)) and failed earlier as compared to the previous cycles. As the composite failed earlier, its failure strain decreased instead of increasing. In contrast, CTE showed a higher value at cycle 6 due to the absence of external force that resulted in no failure of the composite.


### 3.7. FTIR Analysis

Figure4 and Table 5, respectively, show the FTIR spectra and FTIR analysis conducted on WF 30 PLA composite at cycle 0 and cycle 6. This analysis reveals the formation of different functional groups during extrusion that implies composite degradation caused by oxidation and weaker bond formation. Both composites show almost the same characteristic absorptions at cycle 0 and cycle 6. However, because of unequal thickness and heterogeneity of small samples, the relative degradation at cycle 6 as compared to cycle 0 could not be measured.Table 5
FTIR functional group analysis of WF 30 PLA composite at cycle 0 and cycle 6 [20, 21].
Characteristic absorption (cm−1)
Functional group
Indication by functional group
1769
Carboxylic acid
Oxidation
1505
Carboxylic acid
Oxidation
1454
Amine
Weaker bond
1370
Alcohols or phenols
Oxidation
1214
Ether/amine
Oxidation/weaker bond
1091
Ether/amine
Oxidation/weaker bond
1049
Ether/amine
Oxidation/weaker bond
870
Amine
Weaker bondFigure 4
FTIR spectra of WF 30 PLA composite at cycle 0 and cycle 6.


### 3.8. Effect of Recycling on Crystallinity and Thermal Stability

The percentage crystallinity of PLA in the WF 50 PLA composites was measured at cycle 0 and cycle 6 by the following equation [2]:(2)%Crystallinity=ΔHexpΔH×1W×100.Here, ΔHexp is the experimental heat of fusion provided by DSC, ΔH is the heat of fusion of pure PLA (93.1 J/g), and W is the mass fraction of PLA in the composite. The crystallinity of PLA in composite decreased with increased number of reprocessing cycles (Figure 5 and Table 6). This is because the fibers probably degraded at a relatively higher amount that PLA, at cycle 6. From cycle 0 to cycle 6, the average fiber length decreased approximately 56%, while the weight averaged molecular weight of PLA decreased 45.7% (Table 2). Similarly, the melting temperature of PLA, at cycle 6, decreased with successive reprocessing due to the molecular weight reduction of PLA [22].Table 6
DSC analysis of WF 50 PLA composite at cycle 0 and cycle 6.
Properties
Cycle 0
Cycle 6
Melting point (°C)
152.15
149.64
Crystallization temperature (°C)
145.33
144.24
Heat of fusion (J/g)
16.64
15.42
Crystallinity (%)
38.03
35.24Figure 5
DSC analysis curves of WF 50 PLA composite at cycle 0 and cycle 6.However, thermal stability of WF 50 PLA composite increased with consecutive recycling (Table7 and Figure 6) that was caused by the polymer degradation (molecular weight reduction) at cycle 6 [22]. Lower number of volatiles at cycle 6 could be a probable reason for increased thermal stability of the composites.Table 7
TGA of WF 50 PLA composite at cycle 0 and cycle 6.
Property
Cycle 0
Cycle 6
Onset thermal degradation Temperature (°C)
312.42
316.10
Fastest decomposition Temperature (°C)
327.06
337.22
Residue (%)
0
1.35Figure 6
TGA curve and its 1st derivative of WF 50 PLA composite at (a) cycle 0 and (b) cycle 6.
(a)
(b)


## 3.1. Effect of Wood Flour Content on Virgin Composites

Higher WF content (50 wt% filler) increased stiffness properties and tensile and flexural modulus but showed no impact on the tensile and flexural strength. On the contrary, higher filler content decreased composite strain properties. No improvement in the strength properties of composites despite higher filler content can be attributed to poor interfacial adhesion between the fiber and polymer matrix. It is possible that higher filler content could produce fiber agglomeration in the composite matrix resulting in stress concentration, as stress concentration initiates crack propagation which leads to lower composite strength properties [13].Higher filler composite showed increased tensile, flexural, and storage modulus by 950 MPa, 450 MPa, and 450 MPa, respectively, as compared to lower filler (30 wt% filler) composite. This is because the stiffness properties of biocomposites mainly depend on wood flour content [7, 14]. In higher filler composite, higher constrain to polymer chain movement is created, and hence the composite stiffness is increased [2, 9, 14]. As the composite becomes stiffer, it produces more resistance to mechanical or thermal stresses and thus showed a decrease in strain properties.Similarly, heat deflection temperature (HDT) properties showed no response to WF loading levels. This is because lower crystalline polymers, such as PLA, show HDT nearly close to their glass transition temperature, while higher crystalline polymers show HDT around their melting temperature [18]. Higher filler content did not play any role in altering the HDT of lower crystalline polymers [23, 24].


## 3.2. Effect of Recycling on Fiber Length

The fiber length in WF 30 PLA and WF 50 PLA composites decreased with successive reprocessing. At cycle 0 and cycle 6, the average fiber lengths were, respectively, 253.24μm and 111.15 μm, which are noticeably lower than the fiber length of original wood flour (Table 1 and Figure 1). This could be due to two probable reasons, lower MFI of PLA (6 g/10 min) and higher screw rpm of the extruder (200 rev/min), both of which can lead to higher shear stress during extrusion which can result in high attrition causing lower average fiber length in the PLA composite. The results are in agreement with previously reported results [1, 22]. Figure 2 shows the normal distribution of fiber lengths of the composite at cycle 0 and cycle 6.Figure 1
Fibers of WF 30 PLA composite at (a) cycle 0 and (b) cycle 6 (magnification 10x).
(a)
(b)Figure 2
Normal distribution plot of fiber length of WF 30 PLA composite at cycle 0 and cycle 6.


## 3.3. Effect of Recycling on Molecular Weight of PLA

Table2 shows the average molecular weights of WF 30 PLA composite at cycle 0 and cycle 6. Both types of molecular weights, weight averaged (Mw) and number averaged (Mn), showed a decrease with successive recycling. These results agree with the work of other researchers [25]. The polydispersity index (PDI) showed an increase with increased number of reprocessing cycles. This increase in PDI also implies a decrease in molecular weights of PLA [26]. This could be attributed to the breakage of polymer chains due to thermal degradation. Recycling of polymer leads to decrease in Mn resulting in higher PDI.Table 2
Fiber length and molecular weight of WF 30 PLA composite at cycle 0 and cycle 6.
Property
Cycle 0
Cycle 6
Average fiber length (μm)
253.24
111.15
M
w (g/mole)
151,115
81,958
M
n (g/mole)
133,762
50,742
Polydispersity index (PDI)
1.13
1.62


## 3.4. Effect of Recycling on Composite Strength Properties

Strength properties of WF 30 PLA composite (tensile strength, flexural strength, and impact strength) decreased sharply at cycle 6, while they did not exhibit any shift in the previous cycles (Table3). Strength properties of biocomposites primarily depend on fiber length (or aspect ratio), fiber content, void content, interfacial adhesion, and molecular weight of polymer. In this case, fiber length and molecular weight of polymer possibly decreased by a greater extent at cycle 6 than the previous cycles. In addition, crack propagation and fiber pull-outs are observed at cycle 6 that indicate lower interfacial adhesion between the fiber and matrix (Figures 3(a) and 3(b)). This lower interfacial adhesion, attributable to repeated heat and shear stress history due to extrusion, probably results in lower strength properties of the composite [1].Table 3
Physical and mechanical properties of WF-PLA composites after six reprocessing cycles.
(a)
Composite with 30% wood flour
Properties
WF 30 PLA
Cycle 0
Cycle 1
Cycle 2
Cycle 3
Cycle 4
Cycle 5
Cycle 6
Tensile strength (MPa)
55.46 (2.96)AB
55.89(0.73)A
56.55 (0.68)A
53.73 (1.53)AB
52.54 (1.49)BC
50.58 (1.52)C
29.21 (3.23)D
Flexural strength (MPa)
90.96 (2.54)A
89.23 (2.21)A
87.06 (2.72)A
86.70 (2.70)A
87.40 (2.08)A
81.07 (2.94)B
26.81 (3.93)C
Impact resistance (J/m)
47.18 (5.48)A
45.56 (9.62)A
35.36 (6.09)B
34.90 (6.05)B
34.51 (4.45)B
28.91 (7.17)B
13.13 (3.73)C
Tensile modulus (MPa)
6949.95 (332)A
6361.13 (267.86)AB
6484.70 (490.03)AB
6185.56 (792.19)AB
6533.57 (594.27)AB
5978.74 (541.50)B
6303.36 (759.82)AB
Flexural modulus (MPa)
5811.89 (273.48)A
5424.19 (138.78)B
5368.78 (81.01)B
5288.02 (205.17)B
5347.51 (144.87)B
5256.00 (94.96)B
4163.17 (74.57)C
Storage modulus (MPa)
6405.88 (303.48)A
6179.75 (88.9)ABC
6237.50 (144.73)AB
6365.25 (101.37)A
5927.38 (302.9)BCD
5844.25 (274.45)CD
5721.88 (271.06)D
Heat deflection temperature (°C)
56.78 (0.39)A
56.58 (0.27)A
56.73 (0.21)A
56.52 (0.10)A
56.65 (0.24)A
56.15 (0.63)A
54.83 (0.26)B
Failure strain (%)
1.59 (0.27)B
2.05 (0.10)A
2.32 (0.05)A
2.19 (0.25)A
2.20 (0.18)A
2.21 (0.22)A
0.46 (0.05)C
Coefficient of thermal expansion (mm/mm/°C)× 10−5
0.68 (0.31)D
1.22 (0.23)BC
1.31 (0.22)BC
1.19 (0.25)C
1.63 (0.46)ABC
1.69 (0.24)AB
1.90 (0.33)A
Melt flow index (g/10 min)
2.85 (0.26)F
6.45 (0.20)E
7.84 (0.59)D
12.00 (0.36)C
14.26 (0.92)B
14.62 (0.50)B
21.09 (0.13)A
(b)
Composite with 50% wood flour
Properties
WF 50 PLA
Cycle 0
Cycle 1
Cycle 2
Cycle 3
Cycle 4
Cycle 5
Cycle 6
Tensile strength (MPa)
53.98 (3.61)A
53.20 (2.90)A
32.78 (5.17)B
36.84 (6.19)B
27.86 (6.08)B
34.34 (8.15)B
31.38 (9.56)B
Flexural strength (MPa)
91.24 (5.81)A
92.16 (2.71)A
28.57 (1.45)C
36.63 (8.83)B
31.74 (3.73)BC
30.74 (1.87)BC
27.26 (2.16)C
Impact resistance (J/m)
31.32 (6.13)A
31.33 (3.65)A
22.06 (5.46)B
20.48 (6.19)B
18.93 (4.90)B
15.71 (5.45)B
18.76 (4.15)B
Tensile modulus (MPa)
8487.95 (698.60)A
8847.76 (894.24)A
6925.42 (1428.47)AB
5251.07 (1326)BCD
6156.28 (2333.36)BC
4660.82 (1572.32)CD
3907.93 (725.54)D
Flexural modulus (MPa)
6685.00 (480.84)AB
5936.28 (547.61)C
6582.87 (440.04)AB
6850.69 (243.49)A
6713.83 (104.07)AB
6428.03 (293.98)ABC
6284.67 (135.05)BC
Storage modulus (MPa)
7347.88 (498.78)A
7286.13 (476.55)A
7060.13 (825.99)AB
7391 (199.80)A
7106.13 (653.38)AB
6622.25 (589.05)AB
6317.00 (288.40)B
Heat deflection temperature (°C)
56.07 (0.33)A
55.71 (0.59)AB
54.49 (0.43)D
54.58 (0.33)D
54.71 (0.33)CD
55.18 (0.28)BC
54.62 (0.20)CD
Failure strain (%)
1.41 (0.15)AB
1.26 (0.18)B
1.31 (0.52)B
1.84 (0.43)AB
1.41 (0.24)AB
1.93 (0.45)A
1.83 (0.55)AB
Coefficient of thermal expansion (mm/mm/°C)× 10−5
1.29 (0.48)A
0.91 (0.54)AB
0.49 (0.15)B
0.57 (0.23)B
0.54 (0.17)B
0.64 (0.21)B
0.76 (0.19)B
Melt flow index (g/10 min)
2.50 (0.21)F
3.15 (0.12)EF
15.34 (0.99)E
25.09 (0.55)D
28.85 (0.59)C
32.73 (0.56)B
36.67 (0.58)A
Values are shown as the mean with standard deviation in parenthesis. Means with different letters are significantly different (P<0.05).Figure 3
SEM of WF-PLA composite at (a) cycle 0 (WF 30 PLA), (b) cycle 6 (WF 30 PLA), and (c) cycle 2 (WF 50 PLA).
(a)
(b)
(c)On the contrary, strength properties of WF 50 PLA composite decreased vastly after cycle 2 and then became somewhat constant up to cycle 6 (Tables3(a) and 3(b)). This could be due to the higher degradation in fiber and polymer, coupled with lower interfacial adhesion due to higher filler content at cycle 2. Microvoids were also observed in the composite matrix at cycle 2 (Figure 3) that could significantly contribute towards lower strength properties. Strength properties of composites were almost constant from cycle 2 to cycle 6, as the number of pores at cycle 2 and cycle 6 remained equivalent.The sudden change in strength properties for WF 50 PLA at cycle 2 can be related to higher amount of shear stress during extrusion as well as inherent moisture content due to higher amount of wood flour. It is reported that PLA is highly sensitive to shear stress and moisture, which can lead to a rapid decrease in strength properties in highly filled composites [1].


## 3.5. Effect of Recycling on Composite Stiffness Properties

Composite stiffness properties experimented in this study include tensile modulus, flexural modulus, storage modulus, and heat deflection temperature (HDT). All these properties showed a gradual decrease with increasing number of reprocessing cycles for both composites (Tables3(a) and 3(b)). This may be due to the less efficient stress transfer from the matrix to fiber, that is, caused by (1) fiber and polymer degradation, (2) increased number of microvoids, (3) less polymer chain entanglement by fibers, and (4) poor fiber-matrix interfacial adhesion with successive recycling [22, 27].Overall, most stiffness properties showed minor decrease, from cycle 0 to cycle 6 for both formulations of composites, as compared to the corresponding strength properties (Tables3(a) and 3(b)). For example, after reprocessing six times, flexural modulus for higher and lower filler composite decreased by 6% and 28%, respectively, while both flexural strengths decreased approximately 70% (Table 4). As mentioned earlier (Section 3.1), fiber content is the most important parameter to determine stiffness properties of biocomposites [7, 14]. Since the fiber content was constant for each formulation during reprocessing, the amount of polymer chain entanglement decreased less, which contributed to decrease in composite stiffness properties. These findings are consistent with the findings of other research workers [1, 22].Table 4
Relative difference in means of properties of WF/PLA composites between cycle 0 and cycle 6.
Properties
WF 30 PLA composite (%)
WF 50 PLA composite (%)
Tensile strength (MPa)
−47.34
−41.86
Tensile modulus (MPa)
−9.30
−53.96
Failure strain (%)
−71.22
29.20
Flexural strength (MPa)
−70.53
−70.12
Flexural modulus (MPa)
−28.37
−5.99
Impact resistance (J/m)
−72.18
−40.10
Heat deflection temperature (°C)
−3.43
−2.58
Storage modulus (MPa)
−10.68
−14.03
Coefficient of thermal expansion (mm/mm/°C)
175.94
−40.93
Melt flow index (g/10 min)
640.37
1364.60
Negative sign shows a decrease and a positive one shows an increase in the value of the property.The tensile modulus of WF 50 PLA composites from cycle 0 and cycle 6 showed a much higher decrease (54%) than the corresponding flexural modulus (6%) (Tables3(a) and 3(b)). The difference in the property values could be due to the difference in testing methods since tensile test is thickness dependent and flexural test is surface property dependent [19].


## 3.6. Effect of Recycling on Composite Strain Properties

The impact of reprocessing was investigated on the thermomechanical strain properties of composites such as failure strain, coefficient of thermal expansion (CTE), and melt flow index (MFI). For both composites, most of these strain properties showed an increase with repetitive extrusion cycles (Tables3(a) and 3(b)). This increase in composite strain is caused by the same factors (or change in factors) that have reduced composite stiffness with successive recycling (Section 3.5).However, for WF 30 PLA composite, although CTE increased with consecutive recycling, failure strain first increased from cycle 0 to cycle 5 but then sharply decreased at cycle 6 (Table3(a)). This could be attributed to the fact that failure strain was measured with a tensile load while CTE was measured with no preload force and is temperature dependent. At cycle 6, the composite may have degraded to the extent that it could not withstand higher load (Table 3(a)) and failed earlier as compared to the previous cycles. As the composite failed earlier, its failure strain decreased instead of increasing. In contrast, CTE showed a higher value at cycle 6 due to the absence of external force that resulted in no failure of the composite.


## 3.7. FTIR Analysis

Figure4 and Table 5, respectively, show the FTIR spectra and FTIR analysis conducted on WF 30 PLA composite at cycle 0 and cycle 6. This analysis reveals the formation of different functional groups during extrusion that implies composite degradation caused by oxidation and weaker bond formation. Both composites show almost the same characteristic absorptions at cycle 0 and cycle 6. However, because of unequal thickness and heterogeneity of small samples, the relative degradation at cycle 6 as compared to cycle 0 could not be measured.Table 5
FTIR functional group analysis of WF 30 PLA composite at cycle 0 and cycle 6 [20, 21].
Characteristic absorption (cm−1)
Functional group
Indication by functional group
1769
Carboxylic acid
Oxidation
1505
Carboxylic acid
Oxidation
1454
Amine
Weaker bond
1370
Alcohols or phenols
Oxidation
1214
Ether/amine
Oxidation/weaker bond
1091
Ether/amine
Oxidation/weaker bond
1049
Ether/amine
Oxidation/weaker bond
870
Amine
Weaker bondFigure 4
FTIR spectra of WF 30 PLA composite at cycle 0 and cycle 6.


## 3.8. Effect of Recycling on Crystallinity and Thermal Stability

The percentage crystallinity of PLA in the WF 50 PLA composites was measured at cycle 0 and cycle 6 by the following equation [2]:(2)%Crystallinity=ΔHexpΔH×1W×100.Here, ΔHexp is the experimental heat of fusion provided by DSC, ΔH is the heat of fusion of pure PLA (93.1 J/g), and W is the mass fraction of PLA in the composite. The crystallinity of PLA in composite decreased with increased number of reprocessing cycles (Figure 5 and Table 6). This is because the fibers probably degraded at a relatively higher amount that PLA, at cycle 6. From cycle 0 to cycle 6, the average fiber length decreased approximately 56%, while the weight averaged molecular weight of PLA decreased 45.7% (Table 2). Similarly, the melting temperature of PLA, at cycle 6, decreased with successive reprocessing due to the molecular weight reduction of PLA [22].Table 6
DSC analysis of WF 50 PLA composite at cycle 0 and cycle 6.
Properties
Cycle 0
Cycle 6
Melting point (°C)
152.15
149.64
Crystallization temperature (°C)
145.33
144.24
Heat of fusion (J/g)
16.64
15.42
Crystallinity (%)
38.03
35.24Figure 5
DSC analysis curves of WF 50 PLA composite at cycle 0 and cycle 6.However, thermal stability of WF 50 PLA composite increased with consecutive recycling (Table7 and Figure 6) that was caused by the polymer degradation (molecular weight reduction) at cycle 6 [22]. Lower number of volatiles at cycle 6 could be a probable reason for increased thermal stability of the composites.Table 7
TGA of WF 50 PLA composite at cycle 0 and cycle 6.
Property
Cycle 0
Cycle 6
Onset thermal degradation Temperature (°C)
312.42
316.10
Fastest decomposition Temperature (°C)
327.06
337.22
Residue (%)
0
1.35Figure 6
TGA curve and its 1st derivative of WF 50 PLA composite at (a) cycle 0 and (b) cycle 6.
(a)
(b)


## 4. Summary

Two wood flour/PLA composites were formulated by extrusion, each of which contains 30 or 50 wt% filler, 3 wt% PLA-g-MA, and the rest amount of PLA. Both composites were separately reprocessed six times by extrusion. Samples for mechanical and thermomechanical tests were prepared by injection molding. Both 30 and 50 wt% filler composites showed a sharp decrease in tensile strength, flexural strength, and impact resistance at cycle 6 and cycle 2, respectively. Both composites also showed a decrease in tensile modulus, flexural modulus, and storage modulus with successive recycling, while they exhibited an increase in failure strain, coefficient of thermal expansion, and melt flow index. With consecutive reprocessing, composite thermal stability increased, while polymer crystallinity decreased. To sum up, composite strength and stiffness properties decreased, but strain properties increased with successive recycling due to the fiber length reduction and PLA degradation.



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*Source: 1430892-2017-07-27.xml*