3d-dic analysis in interlaminar shear impact test no. v025

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Application News No. V025 HPV-X2 High-Speed Video Camera HITS-T10 High-Speed Impact Testing Machine 3D-DIC Analysis in Interlaminar Shear Impact Test of Composite Materials LAAN-A-HV-E010 Composite materials feature higher specific strength and specific stiffness than metal materials. For this reason, yearly increasing amounts of composite materials are used in passenger and various transport aircraft in order to improve fuel efficiency through weight reduction. However, since the superior properties of composite laminated materials are limited to the fiber direction and layers are adhered only using matrix resin, these materials are very low in strength. If the strength between layers is low and an external load is applied, delamination will easily occur and cause a reduction in compressive strength. Therefore, evaluation of interlaminar properties is important when evaluating composite laminated materials. Furthermore, since these materials may be subject to impact loads when used in transport aircraft, it is also important to determine the impact properties in addition to static properties. In this research, strain distributions resulting from interlaminar shear impact test, which employed the short- beam method based on JIS-K7057, were visualized as an evaluation of interlaminar properties. Strain distribution was visualized using two HPV-X2 high-speed video cameras and 3D digital image correlation (DIC) analysis. F. Yano * DIC analysis This technique compares a random pattern on the sample surface before and after sample deformation to determine the amount of pattern movement. The random pattern used here was applied directly onto the specimen using a black marker pen. Measurement System Interlaminar shear impact test was performed using the HITS-T10 high-speed impact testing machine and the fracture process was observed using two HPV-X2 high- speed video cameras. Capturing video from two directions enables three-dimensional strain measurement and allows high accuracy strain measurement that takes out-of-plane deformations into account. Fig. 1 shows the picture of the test and Fig. 2 shows the test fixture with the specimen. Table 1 lists the system configuration. The video captured by the HPV-X2 cameras is analyzed using the VIC-3D DIC software to determine the strain distribution. Since VIC-3D can control the HPV-X2 cameras, calibration and analysis can be performed easily with no need for separate PCs for analysis and HPV-X2 control. Table 1 Testing System High-speed video camera : Two HPV-X2 high-speed video cameras Testing system : HITS-T10 high-speed impact testing machine Test fixture : Short-beam test fixture Illumination : Stroboscope DIC software : VIC-3D Picture of the Test Test Fixture with Specimen Mounted Test Conditions A GFRP unidirectional laminate was used as the specimen. Table 2 lists the details of the specimen. Table 3 lists the test conditions. Table 2 Measurement Conditions Specimen : GFRP unidirectional laminate Specimen dimensions [in] : 0.25 × 0.25 × 1.75 Table 3 Test Conditions Test speed : 10 m/s Recording speed : 670 kfps Support span : 1.2 in. Test fixture dimensions : Indenter radius: 1 in., support radius: 0.25 in. Test fixture Specimen Stroboscope HPV-X2 HPV-X2

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Page 1: 3D-DIC Analysis in Interlaminar Shear Impact Test No. V025

Application News

No. V025

HPV-X2 High-Speed Video Camera HITS-T10 High-Speed Impact Testing Machine

3D-DIC Analysis in Interlaminar Shear Impact Test

of Composite Materials

LAAN-A-HV-E010

Composite materials feature higher specific strength and specific stiffness than metal materials. For this reason, yearly increasing amounts of composite materials are used in passenger and various transport aircraft in order to improve fuel efficiency through weight reduction. However, since the superior properties of composite laminated materials are limited to the fiber direction and layers are adhered only using matrix resin, these materials are very low in strength. If the strength between layers is low and an external load is applied, delamination will easily occur and cause a reduction in compressive strength. Therefore, evaluation of interlaminar properties is important when evaluating composite laminated materials. Furthermore, since these materials may be subject to impact loads when used in transport aircraft, it is also important to determine the impact properties in addition to static properties. In this research, strain distributions resulting from interlaminar shear impact test, which employed the short-beam method based on JIS-K7057, were visualized as an evaluation of interlaminar properties. Strain distribution was visualized using two HPV-X2 high-speed video cameras and 3D digital image correlation (DIC) analysis.

F. Yano * DIC analysis

This technique compares a random pattern on the sample surface before and after sample deformation to determine the amount of pattern movement. The random pattern used here was applied directly onto the specimen using a black marker pen.

Measurement System Interlaminar shear impact test was performed using the HITS-T10 high-speed impact testing machine and the fracture process was observed using two HPV-X2 high-speed video cameras. Capturing video from two directions enables three-dimensional strain measurement and allows high accuracy strain measurement that takes out-of-plane deformations into account. Fig. 1 shows the picture of the test and Fig. 2 shows the test fixture with the specimen. Table 1 lists the system configuration. The video captured by the HPV-X2 cameras is analyzed using the VIC-3D DIC software to determine the strain distribution. Since VIC-3D can control the HPV-X2 cameras, calibration and analysis can be performed easily with no need for separate PCs for analysis and HPV-X2 control.

Table 1 Testing System

High-speed video camera : Two HPV-X2 high-speed video cameras Testing system : HITS-T10 high-speed impact testing

machine Test fixture : Short-beam test fixture Illumination : Stroboscope DIC software : VIC-3D

Picture of the Test

Test Fixture with Specimen Mounted

Test Conditions A GFRP unidirectional laminate was used as the specimen. Table 2 lists the details of the specimen. Table 3 lists the test conditions.

Table 2 Measurement Conditions

Specimen : GFRP unidirectional laminate Specimen dimensions [in] : 0.25 × 0.25 × 1.75

Table 3 Test Conditions

Test speed : 10 m/s Recording speed : 670 kfps Support span : 1.2 in. Test fixture dimensions : Indenter radius: 1 in.,

support radius: 0.25 in.

Test fixture

Specimen

Stroboscope

HPV-X2 HPV-X2

Page 2: 3D-DIC Analysis in Interlaminar Shear Impact Test No. V025

ApplicationNews

No. V025

First Edition: May 2017

For Research Use Only. Not for use in diagnostic procedure.

This publication may contain references to products that are not available in your country. Please contact us to check the availability of these products in your country. The content of this publication shall not be reproduced, altered or sold for any commercial purpose without the written approval of Shimadzu. Company names, product/service names and logos used in this publication are trademarks and trade names of Shimadzu Corporation or its affiliates, whether or not they are used with trademark symbol “TM” or “ ”. Third-party trademarks and trade names may be used in this publication to refer to either the entities or their products/services. Shimadzu disclaims any proprietary interest in trademarks and trade names other than its own. The information contained herein is provided to you "as is" without warranty of any kind including without limitation warranties as to its accuracy or completeness. Shimadzu does not assume any responsibility or liability for any damage, whether direct or indirect, relating to the use of this publication. This publication is based upon the information available to Shimadzu on or before the date of publication, and subject to change without notice.

© Shimadzu Corporation, 2017

www.shimadzu.com/an/

Measurement Results Fig. 3 shows the DIC analysis results of shear strain up to immediately before fracture. Immediately after starting the test, shear strain is concentrated directly below the supports, as shown in Fig. 3 (1). Next, shear strain occurs symmetrically from the supports to the indenter, and immediately before fracture, shear strain is distributed on the entire specimen. Fig. 4 shows delamination. In Fig.4 (2), delamination is occurring from the left side of the specimen. Delamination progresses from there and also occurs from the right side as shown in (4). Fig. 5 shows the DIC analysis results in sync with Fig. 4. Fig. 5 shows that delamination occurs from the positions where shear strain was concentrated. Performing DIC analysis also enables determination of the delamination positions, which were difficult to discern in Fig 4.

Conclusion In this research, we performed 3D-DIC analysis to measure the shear strain in interlaminar shear impact test of a GFRP unidirectional laminate using two HPV-X2 cameras. Performing 3D-DIC analysis allowed us to confirm the increase in shear strain during testing and the strain distribution when delamination occurred. The HPV-X2 is well-suited to observation of the fracture process in impact test such as that presented here, and proves useful in evaluating impact properties.

DIC Analysis Results of Shear Strain up to Immediately Before Fracture (time between images: 27 μs)

Progress of Delamination (time between images: 6 μs, white arrows indicate delamination positions)

DIC Analysis of Delamination (DIC analysis results of Fig. 4)

(1) Supports

Indenter

(2) (3)

(1) (2) (3) (4)

Delamination Delamination

(1) (2) (3) (4)