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Investigation of the effect of tufts contribution on the in-plane mechanical properties of flax fibre reinforced green biocomposite


Traditional laminated composites have fibres oriented only in the in-plane of the laminate due to their manufacturing process, and are therefore very susceptible to transverse cracking and delamination from out-of-plane actions. Delamination can considerably reduce the load bearing capacity of a structure hence several reinforcement solutions, based on the principle to add out-of-plane reinforcement to the 2D fabric, have been explored to enhance the delamination resistance. However, the usual textile technologies for Z-reinforcement such as weaving, knitting, stitching, z-pinning, and tufting generates perturbations that may alter the in-plane mechanical properties. Although tufting is a single needle and single thread based one side stitching (OSS) technique which can incorporate almost tension free through the thickness reinforcement in a material, various types of microstructural defects may be created during the manufacturing process and lead to a degradation of the in-plane properties of the composite. Moreover, due to awareness in environmental concerns, the development and use of eco-friendly biocomposites to replace synthetic ones has been increasing.

This research work investigates the effect on in plane mechanical properties of adding through the thickness reinforcement (TTR) by tufting in a flax based composite laminate to improve the transversal strength. The glass fibre tufted laminates of 550 g/m2 flax fibre were moulded using a 38% biobased thermoset resin by vacuum bag resin transfer moulding (VBRTM). The tufted and un-tufted in-plane mechanical properties of green biocomposite were determined in tension, compression and shear in accordance with ASTM 3039, ASTM D7137 and EN ISO 14130, using universal INSTRON 1186 and MTS 20 M testing machines. The quantification of the in-plane mechanical properties established a reduction of the in plane tensile mechanical properties, due to tufting, whereas the reduction effects are marginal in compression. As expected, the glass fibre tufts strength the connection between core and skin of the composite so that the interlaminar shear strength, deduced from flexural tests with small span-to-thickness ratio, is increased. Thanks to Digital Image Correlation (DIC) performed during shear tests, an increase in interlaminar shear modulus is highlighted.


Fibre reinforced polymer (FRP) composites are in high demand for manufacturing structural components of automotive, aerospace, marine and wind energy sector. Despite high investment and manufacturing cost as compared to metallic alloys, the rapid growing interest in the use of FRPs has arisen due to promising properties, such as high strength to weight ratio, high specific stiffness, and excellent resistance to fatigue, creep, rapture and corrosion [1,2,3]. Additionally, the shift towards FRPs as lighter structural material is unavoidable to meet environmental targets of 75% and 90% reduction in the levels of CO2 and NOx by 2050 for which the contribution of airframes is evaluated from 20 to 25% [4]. Conventional composite laminates (2D) are very efficient in distributing in-plane normal and shear loads since the alignment of fibres is along the load-bearing path. However, the lack of through the thickness reinforcing fibres is a disadvantage in terms of delamination toughness and impact damage resistance. Therefore, since the past four decades there has been a growing interest in the development of several methods in order to provide through-thickness strength and stiffness to preforms in the three-dimensional (3D) direction using through the thickness reinforcement techniques [5,6,7,8,9].

Among such developed methods, weaving, kitting, braiding were primarily used for manufacturing three-dimensional preforms. However, these adopted processes from textile industry could not be used for a long period due to lack of flexibility of semi-finished products, costly and complex machinery, and inflexible machine parameters. Furthermore, the choice of adopting a particular process for fabricating 3D preform depends on the end use of product [10,11,12,13,14,15,16,17]. Although Mouritz presented large data base on the in-plane and out of plane mechanical properties of stitched 3D composites manufactured using various textile technologies, yet it is very difficult to conclude the best textile technology to reinforce through the thickness due to various technical, economic and certification issues [18]. In this scenario, stitching has been assessed as a potential technique for sewing through the laminate structure using a high tensile strength yarn, such as glass, carbon and kevlar [19]. Three-dimensional composite structures manufactured using stitched laminates have received considerable attention in high tech industry. Aircraft structure including large parts of airframe, wing panels, fuselages and blade-stiffened components are built using 3D composite materials [10]. It is also used in load bearing structure such as I-beam. In automotive industry it is used for manufacturing doorframe, bumper bar and floor panels [20].

Unfortunately, the manufacturing complexity of accessing the needle from downside to form the stitch and the resulting tension due to formation of loops and knots (chain stich and lockstitch) may degrade the in-plane mechanical properties especially bending and compression due to constrictions and undulations formed in the laminates [21, 22]. However, a variety of possible stitching parameters, such as type of needle, stitching material, stitching density, stitching geometry, stitching method, type of stitching, type of laminate, machine parameters, and thread tension makes it a highly flexible technology. Hence, keeping the pros of stitching technology in view, an extensive R&D is pursued to address the drawbacks of this technology to achieve desirable three-dimensional properties of a material without degrading the exceptional mechanical in-place properties.

In this regard, DLR Institute of Structural Mechanics at German Space Centre in Brunswick developed “Single-Sided Tufting Method” as the potential method to meet structural and cost effective efficiency requirements. Tufting was developed as the befitting structural stitching means to bring significant improvement in the energy absorption behaviours particularly the energy release rate, crack propagation, and damage tolerance [23]. In contrast to conventional stitching techniques that employ a dual threading system, “tufting” is a single thread method that makes tension free insertion of the thread needle in dry fabric laminates and removal of the needle from fabric laminates along the same trajectory [24, 25]. In this process, loose and tension free loops form on the downward side without adversely affecting the laminates material. Furthermore, tufting is beneficial as compared to conventional stitching methods because the material to be sewn needs to be only accessible from one side therefore there would be no need of complex and costly construction with lift tables [26, 27].

It was realised by the authors after making a thorough literature review that there are few results related to the degree to which through-thickness reinforcement degrades in-plane mechanical properties of tufted fibre reinforced composites [1, 28,29,30,31,32,33,34] [35,36,37], and even fewer related to in-plane mechanical properties of tufted green biocomposites. Natural fibre based green biocomposites are the material of future in structural, automotive and aerospace industry due to their environmental merits, low density, high specific strength, stiffness, low energy consumption in fabrication, CO2 neutrality and sound proofing characteristics [38]. Since a degradation in the in-plane properties may arise due to local damage to fibres resulting from tufting needle, fibre kink and resin rich areas, this work presents the effect of tufting on the in-plane mechanical properties like tension, shear and compressive strengths of green biocomposites based on flax fibre reinforced with glass fibre tufts.

Material and methodology for manufacturing green biocomposite


The flax fibre was procured from Eco-technilin. It consists of 2 × 2 twill weave flax fibre with an areal density of 550 g/m2and a linear density of 0.0045 g/m. The epoxy resin used was InfuGreen 810 with SD 8822 curing agent, a 38% biobased epoxy, procured from Sicomin. Glass fibre thread having a linear density of 0.179 g/m and a twist level of 136 turns/m was supplied by Tissafil. KUKA 6-axis robot arm (KR 100–2 HA 2000) was employed to carry out tufting of six plies of flax fibre stacked on top of each other using glass fibre thread. The thread of glass fibre was inserted in a needle of 2 mm diameter to tuft the dry preform of flax fibre sheets [39]. The end tabs used to grip the specimen in tensile testing were fabricated by infusing InfuGreen 810 in bidirectional laminates of glass fibre.

Methodology for manufacturing green biocomposite

Six plies of flax fibre sheets were placed horizontally on top of each other with a stacking sequence of [0]6 to manufacture the reference and tufted plates. The stitching process is characterised by insertion of glass fibre thread transversally by employing KUKA 6-axis robot at ±90° to the normal plane of traditional 2D dry preform to reinforce flax fibre with a tufting density of 5 × 5 mm in a transversal square geometry pattern as shown in Fig. 1 [40]. Once the tufting needle arrives at the selected depth, the needle is pulled back from dry preform, and a retention mechanism let the tufts to remain in the laminates. A ringlet is formed on the recto face of the 2D dry preform as shown in Fig. 2a and b. The volume fraction of flax fibre reduces from 35% to 34.5% in tufted composite as compared the untufted one. The average length of tuft loops was fixed to 10 mm and a sheet of polyurethane form was placed as a support beneath the dry laminates of flax fibre sheets to hold the tuft loops of glass fibre and to keep them in place [31]. The areal density of untufted and tufted stacked preforms were estimated to be 2870 g/m2 and 3060 g/m2 respectively.

Fig. 1
figure 1

a Schematic of transversal tufted specimens. b Tufting reinforcement in the Sheets of flax

Fig. 2
figure 2

Front and back of tufted sheets of flax

The technique of vacuum bag resin transfer moulding process as shown in the schematic of Fig. 3 developed by Francis W. Bailey in 1996 was used to manufacture the green biocomposite using InfuGreen 810 epoxy resin system [41].

Fig. 3
figure 3

Vacuum bag resin transfer moulding process [40]

Figure 4 shows the moulding of flax fibre sheets performed under a vacuum pressure of − 0.9 bar at room temperature. The infused plates were cured for 24 h at room temperature and post cured in an oven for 8 h at 80 °C. The average final thickness of plates was estimated 6.5 mm for untufted and 7 mm for the tufted plates. A thickness of 0.5 mm was added in tufted plate due the presence of carbon tufts on the surface of flax sheets. The plates were cut to the specimens’ size as per the requirements of ASTM or ISO standards for each mechanical test. The specimens are referred to as REF for non-tufted and TUF for tufted in this study.

Fig. 4
figure 4

Vacuum infusion process of flax fibre sheets

Determination of in-plane mechanical properties

The in-plane properties of tufted and untufted specimens were experimentally characterised in tension, compression, shear, and compared afterwards. The geometric specifications of the specimens were chosen according to the ASTM or ISO standards designated for each type of test. The experiments were conducted on a universal INSTRON 1186 for tensile and compressive tests and on MTS 20 M testing machines for short beam shear test.

Three point bending-short beam shear test

Short beam shear test is widely employed for screening and quality control of materials due to ease of sample preparation and testing [42]. The interlaminar shear properties of matrix obtained by short beam test provide important information on long-term degradation of the matrix [43,44,45].

The preparation of REF and TUF specimens and the procedure of carrying out three point bending test followed ASTM D2344–16 [46]. For the REF and TUF specimens, length and width were the same: 60 mm and 30 mm respectively, whereas the thickness for REF and TUF specimens was slightly different: 6.5 mm and 7 mm respectively. The loading configuration was defined by a span length of 32 mm, support cylinder diameter of 3 mm and loading nose diameter of 6 mm. A Digital imaging camera (DIC) was placed in front of loaded specimens to perform in situ non-destructive testing and to capture the images during tests. The specimens of three point bending tests were analysed with scanning electron microscope (SEM) to observe the pattern of crack propagation.

Boeing compression test

Boeing compression test (BCT) are performed to evaluate the effect of tufting on the in-plane compressive strength of composites while preventing buckling. The specimens were prepared according to ASTM D7137–07 [47] and universal testing machine was employed to perform BCT following modified D695 compression test method [48]. The length and width of specimens for BCT were 150 mm and 100 mm respectively for both REF and TUF materials, and the thicknesses of samples were 6.5 mm for REF and 7 mm for TUF material. Three specimens of each i.e. REF and TUF were subjected to BCT loading to calculate ultimate compressive strength and compression modulus.

Tensile test

Tensile strength test is used to determine the in-plane properties of composites materials. However, this test is limited to such polymer matrix composites that are reinforced with high modulus fibre, and where the laminates are symmetric and balanced with respect to the test direction. The tensile property data produced from this test is extensively used for quality assurance, and structural design and analysis.

The tensile test was carried out on a universal testing machine as per the ASTM standard D3039/3039 M-17 [49]. The rectangular specimens of REF and TUF had a length of 200 mm and width of 35 mm, whereas the thickness of REF material was 6.5 mm and for TUF was 7 mm. To prevent failure in the grip while performing the tensile test, 40 mm tabs made up of glass fibre and InfuGreen 810 epoxy were attached on each end of the specimen. To measure the values of Young’s modulus and ultimate tensile strength strain gauge was placed in the centre of specimen. The load was applied to the specimen at a constant rate of 1 mm/min until the specimen fractured.

Results and discussion

The in-plane mechanical properties of tufted and untufted biocomposite samples were compared for tensile, compressive and shear strength of the material. The Investigation of tufting behaviour with respect to control specimen on the shear loading conditions was carried out on REF and TUF samples. Figure 5 represents a schematic of the direction of axis used in this study.

Fig. 5
figure 5

Schematic of axis direction

Short beam bending tests were conducted in order to compare these two materials in terms of interlaminar shear behaviour. Figure 6b displays the typical global response of the specimens subjected to the short beam shear tests.

Fig. 6
figure 6

a DIC carried out on short beam. b Load-Displacement curve of flexion for REF and TUF green biocomposite

For a linearly elastic beam with a rectangular cross section of width b and depth h, a parabolic stress distribution is assumed. This result is demonstrated with the use of the first kinematic Euler-Bernouilli assumption, which states that the cross-section of the beam remains plane after deformation, and on the meeting of equilibrium conditions. The shear stress distribution in terms of the applied shear force, \( V=\frac{P}{2\ } \) where P is the load in Newton (N), is:

$$ {\tau}_{xz}=\frac{3\ V}{2\ b\ h}\left[1-{\left(\frac{2\ z}{h}\right)}^2\right] $$

This assumption has been found to be valid for large parts of the beam between the loading and supporting rollers, especially for large loading roller diameter [50].

The maximum shear stress, found at the neutral axis (z = 0), shows the interlaminar shear strength (τxz) of the composite material that is reported in ISO 14130 or ASTM D2344–16. It is represented by eq. (2).

$$ {\tau}_{xz}=\frac{3}{4}\frac{P}{b\times h} $$

The maximum interlaminar shear strength (ILSS) of the REF and TUF material shown in Fig. 7 exhibits that tufting reinforcement increases shear strength of the flax fibre based green biocomposite by 8%. The literature review reports conflicting results [51,52,53,54,55,56] i.e. the stitches can become sites of stress concentration that can cause reduction in the interlaminar shear strength whereas the improvement in shear strength is possibly due to through-thickness interlocking which difficult shearing between the fabric plies. Microscopic observation of the specimen after short beam shear test was performed using SEM. It is shown in Fig. 8 how tufts arrests crack propagation in the tufted material. The specimen is loaded by shear force parallel to crack surfaces. The sliding of crack surfaces over each other in the x direction results in a skew symmetric deformation with respect to the plane i.e. perpendicular to the y and z axis. Delamination starts from the resin pocket on the outside region but the tufted thread arrests its propagation and improves fracture toughness of the materials. The bridging effect of tufts enhances local stiffness by precluding the sliding of inter-plies [57, 58].

Fig. 7
figure 7

Interlaminar shear strength for REF and TUF material

Fig. 8
figure 8

Observation of crack propagation around a stitch using SEM

Digital Image Correlation performed for three point bending short beam shear test, as shown in Fig. 6a, was used to calculate mean shear strain (γxz) and in turn interlaminar shear modulus (Gxz). As the shear stress is to be maximum on neutral plane (eq. (2)), to efficiently achieve the interlaminar shear strain, a small area centred in neutral plane (z = 0) was selected as shown in Fig. 9. To be consistent with the assumption of a parabolic shear stress distribution, this zone must be sufficiently far from the support and loading rollers and exhibit negligible principal strains (εxx and εzz ≈ 0).

Fig. 9
figure 9

Virtual gage positioned on DIC longitudinal displacement field to calculate the mean strain

The virtual gauge was positioned in different places for different specimen since Song [59] has reported that for tufted specimen the mean shear strain differs considerably for a region containing tuft thread as compared to a region not including a tuft thread. Therefore, to homogenise the properties of the biocomposite material the choice of positioning the gauge must be carefully selected including the fabric preform and tufting thread.

Using DIC and virtual strain gauge rosettes gives us access to the longitudinal strain (εxx), out of-plane strain (εzz) and interlaminar shear strain (εxz) at any moment of the loading. These values, synchronised with the interlaminar shear (eq. (2)), are shown in Fig. 10.

Fig. 10
figure 10

Mean strains (εxx, εzz, and εxz) obtained by DIC images from REF and TUF specimens

The linear part in the interlaminar shear stress-strain curve in Fig. 10 gives the interlaminar shear moduli for REF and TUF samples. The interlaminar shear moduli of tufted specimens of flax based green biocomposite increases slightly by 5.7% (Fig. 11) as compared to untufted material. The values of interlaminar shear strength and shear modulus are reported in Table 1.

Fig. 11
figure 11

Interlaminar shear modulus (Gxz) for REF and TUF

Table 1 Interlaminar shear strength and flexural modulus of REF and TUF biocomposite

Boeing Compression test was performed to determine the compressive strength of the flax based green biocomposite materials. Three samples of each REF and TUF were subjected to compression loading as shown in Fig. 12a, and the linear part of the stress strain curve of Fig. 12b is used to calculate the compressive modulus. The results of ultimate compressive strength and compressive modulus are presented in Table 2.

Fig. 12
figure 12

a) Specimen in loading under compression b) Stress-Strain curve of REF and TUF green biocomposite

Table 2 Ultimate compressive strength and compressive modulus of REF and TUF green biocomposite

The results shown in Fig. 13a and b highlights that through the thickness reinforcement marginally improves the ultimate strength of the material. It is reported in a number of paper that tufting does not significantly affect the compressive strength of the fibre-reinforced composites [22, 52, 60,61,62,63,64,65,66,67,68,69,70]. Dow and smith [63] reported similar compressive strengths of carbon fibre reinforced polymer (CFRP) stitched with either glass, carbon or Kevlar® as compared to their unstitched counterpart [71]. Harris et al. [60] and Herzberg and Bannister [72] found similar behaviour of stitched and unstitched CFRP. Similarly, Du et al. [52] also did not observe any appreciable change to the compressive strength of CFRP after stitching with Kevlar®.

Fig. 13
figure 13

a Ultimate compressive strength and b Compressive modulus for REF and TUF green biocomposite

During the tensile tests, the values of load, displacement, strain and time were measured throughout the test as shown in Fig. 14a. The gradient of the linear part of stress-strain curve shown in Fig. 14b gives the Young’s modulus of the material and the ultimate tensile strength is determined from the failure load. The results are displayed in Table 3.

Fig. 14
figure 14

a Graphic of specimen under tensile loading. b Stress vs strain curve of specimen under tensile loading

Table 3 Young’s modulus and Ultimate tensile strength of REF and TUF green biocomposite

It can be seen in Fig. 15 that the Young’s modulus and ultimate tensile strength are reduced by 42% and 31% respectively.

Fig. 15
figure 15

Percentage decrease in the young’ modulus and ultimate tensile strength of Tufted green biocomposite

Reduction of the in-plane tensile properties could be due to misalignments and fibre rupture caused by tufting of laminated composite and concentration of stress around tufts [73]. Furthermore, tufting loops accumulate a thin layer of resin that gives rise to the thickness of sample. The formation of a thin layer of resin, with a low mechanical resistance, increases the cross section of material and thereby the strength of sample is reduced. Tufting changes the original architecture of the twill weave and form misaligned fibres as shown in Fig. 16a, it can be seen in the figure that glass fibre thread has moved the tows of flax fibre sideways causing a misalignment.

Fig. 16
figure 16

Schematic of stitching defects [20] a) in-plane fibres misalignment, b resin pocket created on the laminate surface between the stitched threads

This created space between the misaligned flax fibres and glass thread can be permeated with resin as shown in Fig. 16b. These two defects caused by tufting, i.e. fibre misalignment and resin rich region are mainly responsible for reduced in-plane properties reported in tensile testing of flax based green biocomposite [74].


This study deals with the effect of tufting on the in-plane mechanical properties and failure mechanisms of structurally tufted flax and its non-tufted counterpart loaded in tension, compression and shear. The distortion induced by glass fibre during tufting yields negative effect on the in-plane mechanical properties of the green biocomposite in tension, the effects are marginal in compression, whereas in shear a slight improvement in interlaminar shear strength and shear modulus is reported. It is essential to mention that there are only few similar studies on the characterisation of in-plane mechanical properties of green biocomposite composed of natural fibre and a bioepoxy resin. The reduction in the values of Young’s modulus of specimen in tension is certainly due to the distortion of in-plane fibres around the tufts that leads to their misalignment with the load applied and the formation of resin rich pockets. When the biocomposite tufted with a yarn of high modulus, such as glass, is loaded in compression, the failure due to Euler buckling is inhibited. However, tufted laminates of flax fail in compression by the formation of kink bands around the most distorted fibres [20]. This mechanism is considered to be primarily responsible for the marginal reduction in compressive modulus. In case of short beam shear test, tuft threads are responsible for concentration of stress, which leads to commencement of cracks from them and result in interlaminar propagation until they are arrested by the next tuft row. This crack bridging phenomenon and difficulty in shearing between plies is thought to improve the ILSS of the tufted material. The finding of this study reveals the complexity of reinforcing biocomposites in through the thickness direction. Hence, to improve their performance rigorous efforts are required in order to take the understanding of mechanical behaviour of 3D biocomposites to the level of understanding of mechanical behaviours of 2D laminated composites.

Availability of data and materials

All data generated or analysed during this study are included in this published article.



Boeing compression test


Carbon fibre reinforced polymer


Digital image correlation


Fibre reinforced polymer


Interlaminar shear strength


One side stitching




Scanning electron microscope


Through the thickness reinforcement






Vacuum bag resin transfer moulding


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The authors appreciate the generosity of Mr. Muddassir Abrar to perform a thorough reading of the paper several times to avoid any mistakes of language and citations, and for checking the coherence of the work in the manner, it is presented.


Higher Education Commission, Pakistan.

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MR selected the materials used in this study and manufactured the green biocomposite using flax fibre and InfuGreen 810 epoxy through VBRTM. She prepared the samples according to ASTM standards for testing of in-plane mechanical properties. She performed the tensile, bending and compression tests and analysed the results. She wrote the first draft of article, which kept, on improving with the input of other authors and she finalised the final version of the article presented here. J.LH carried out the three point bending test and Digital imaging correlation of the materials. He analysed the results of three point bending test, and contributed in writing the results of three point bending test. He did a thorough internal review of the article as well. KC supervised the study. He managed the procurement of the material used in this study and provided guidelines on selection of material for this study. He monitored the various steps involved during this study and contributed in internally reviewing the article at several stages. KK guided and helped in manufacturing of the green biocomposite. He was also involved in providing guidelines on performing the in-plane mechanical test correctly. He prepared the tabs used in tensile testing of the material. He provided his input in analysing the results of tensile and compression tests. ZA provided guideline in procurement of natural fibre for this study. He carried out the tufting of the material and provided guideline on carrying out tensile, bending and compression test according to specified ASTM standards. NG supervised the study. He did an internal review of the paper. He provided his input in analysing the results of in-plane mechanical properties and SEM analysis. The authors read and approved the final manuscript.

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Rashid, M., Hanus, J.L., Chetehouna, K. et al. Investigation of the effect of tufts contribution on the in-plane mechanical properties of flax fibre reinforced green biocomposite. Functional Composite Mater 2, 11 (2021).

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