Garza Rodriguez, Carlos

Pavier, Martyn

Shterenlikht, Anton

Smith, David

The deep-hole drilling (DHD) method is a residual stress measuring technique commonly used in isotropic materials. This paper provides an investigation into using DHD to determine residual stress fields in orthotropic laminated composite materials. In this method, a reference hole with a small diameter is drilled through a component that has residual stresses. The diameter of the hole is carefully measured using an air probe as a function of depth and angular position inside the hole. The residual stresses are then released by trepanning a core of larger diameter from around the hole. The diameter of the hole is afterwards re-measured at the same angular positions and depths as in the original measurements. Changes in the shape of the hole are related to the residual stresses that were present before the hole was drilled. For orthotropic materials, the calculation of residual stresses requires the evaluation of distortion coefficients which rely on the mechanical properties of the components. In this work, the finite element method is used to determine these coefficients. Using this technique, the in-plane residual stresses in an AS4/8552 composite laminate are experimentally measured and compared to finite element predictions as well as to classical lamination theory. It was determined that when using DHD in laminated materials the ratio between the thickness of the layers and the reference hole and trepan diameter needs to be sufficiently high, otherwise remaining interlaminar shear stresses in the trepanned core leads to inaccurate measurements.</p

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                          Garza Rodriguez, C., Smith, D., Shterenlikht, A., & Pavier, M. (2015).Measurement of in-plane residual stresses in an AS4/8552 compositelaminate using the deep hole drilling method. In Proceedings of the 20thInternational Conference on Composite Materials, Copenhagen, Denmark,19-24 July 2015. (Vol. 20). International Conference on CompositeMaterials, ICCM.Peer reviewed versionLink to publication record in Explore Bristol ResearchPDF-documentUniversity of Bristol - Explore Bristol ResearchGeneral rightsThis document is made available in accordance with publisher policies. Please cite only the publishedversion using the reference above. Full terms of use are available:http://www.bristol.ac.uk/pure/about/ebr-terms.htmlTake down policyExplore Bristol Research is a digital archive and the intention is that deposited content should not beremoved. However, if you believe that this version of the work breaches copyright law please contactopen-access@bristol.ac.uk and include the following information in your message:• Your contact details• Bibliographic details for the item, including a URL• An outline of the nature of the complaintOn receipt of your message the Open Access Team will immediately investigate your claim, make aninitial judgement of the validity of the claim and, where appropriate, withdraw the item in questionfrom public view.20th International Conference on Composite Materials Copenhagen, 19-24th July 2015 MEASUREMENT OF IN-PLANE RESIDUAL STRESSES IN AN AS4/8552 COMPOSITE LAMINATE USING THE DEEP-HOLE DRILLING METHOD  C. Garza, D.J. Smith, A. Shterenlikht and M.J. Pavier  Department of Mechanical Engineering, University of Bristol Queen's Building, University Walk, Bristol, BS8 1TR, United Kingdom Email: carlos.garza@bristol.ac.uk     Keywords: Composite Laminates, Deep Hole Drilling, Finite Element Analysis, Residual Stress   ABSTRACT The deep-hole drilling (DHD) method is a residual stress measuring technique commonly used in isotropic materials. This paper provides an investigation into using DHD to determine residual stress fields in orthotropic laminated composite materials. In this method, a reference hole with a small diameter is drilled through a component that has residual stresses. The diameter of the hole is carefully measured using an air probe as a function of depth and angular position inside the hole. The residual stresses are then released by trepanning a core of larger diameter from around the hole. The diameter of the hole is afterwards re-measured at the same angular positions and depths as in the original measurements. Changes in the shape of the hole are related to the residual stresses that were present before the hole was drilled. For orthotropic materials, the calculation of residual stresses requires the evaluation of distortion coefficients which rely on the mechanical properties of the components. In this work, the finite element method is used to determine these coefficients. Using this technique, the in-plane residual stresses in an AS4/8552 composite laminate are experimentally measured and compared to finite element predictions as well as to classical lamination theory. It was determined that when using DHD in laminated materials the ratio between the thickness of the layers and the reference hole and trepan diameter needs to be sufficiently high, otherwise remaining interlaminar shear stresses in the trepanned core leads to inaccurate measurements.   1 INTRODUCTION Deep-hole drilling (DHD) is a technique that allows the measurement of residual stress fields through very thick components. This technique requires that a small diameter hole is drilled through a component that contains residual stresses. The hole diameter is accurately measured (generally using an air probe) as a function of both depth and angular position inside the hole. The residual stresses in the component are afterwards released by machining away a core of larger diameter from around the hole. The relaxation of residual stress distorts the shape of the reference hole. The reference hole diameter is subsequently re-measured at the same angular positions and depths. The reference hole distortion is lastly related to the residual stresses that existed in the component before drilling the hole.  The main assumption of this method is that the drilling of the reference hole has no effect on the residual stress state and that removing the core causes the residual stresses around the hole to be fully released [1, 2].  The deep hole drilling technique has usually been used on metal parts such as in welds [3-5] and railway tracks [6].  In metallic components, EDM can be used to trepan a central core around the reference hole since additional residual stresses introduced by this method are not significant.   An attempt to apply this technique to a laminated carbon-fibre composite was made by Bateman et al. [2]. In this investigation, EDM could not be used to machine the core around the reference hole because CFRP is not conductive and for this reason a diamond encrusted hole saw was selected  C. Garza,  D.J. Smith,  A. Shterenlikht  and  M.J. Pavier  instead. Moreover, the analytical model to allow the change in hole shape to be related to the original residual stresses was extended to take into account the use of an orthotropic material.  2 ANALYTICAL MODEL The DHD technique is based on the measured radial distortion to determine the components of the residual stress from the reference hole.  The formulation to the case of far field biaxial stresses plus shear stress can be stated as   1 	  	  	 (1) where for isotropic materials 	  1  2 cos 2 	  1  2 cos 2 	  4 sin 2  and   1 …   is the measurement angle.  In the case of orthotropic materials these distortion coefficients depend on the mechanical properties of the component. Additionally, the relationship between the longitudinal direction of the material (fibre direction) and the measurement angle (air probe angular position during experiments) must be taken into consideration, see Figure 1.    Figure 1: Unidirectional laminate showing the relationship between the fibre direction !  and measurement   angles in reference to the global axes.  For this analysis, these coefficients for the studied material (AS4/8852) were calculated using the finite element software ABAQUS considering the mechanical properties given in Table 1 and the following values were determined  	  1.49  5.21 cos 2 	  15.89  19.51 cos 2 	  30.04 sin 2      20th International Conference on Composite Materials Copenhagen, 19-24th July 2015 Engineering constant  Value E1 [GPa] 135 E2 [GPa] 9.6 E3 [GPa] 9.6 σ12 – 0.3 σ13 – 0.3 σ23 – 0.435 G12 [GPa] 5.2 G13 [GPa] 5.2 G23 [GPa] 3.4  Table 1: Mechanical properties of AS4/8552.  The radial distortion is normally measured at nine different angles and at least three measurements are required to obtain accurate results.  The relation of the measured radial distortions and the residual stress is given by ()   1* + · - (2) The use of the minus sign is required because the radial distortions are measured after releasing the residual stresses. The matrices are expressed as  () .///0 1|343561|343	61|34378999: + .////03563	3563	3563	6 6 637 37 3789999:  -  ; <  where N is the number of angular measurements. Lastly, the residual stresses are determined from the measurements of the radial distortions of the hole by -   += ·  () (3) where +=  +> · + ?@ · +> is the pseudo-inverse of +.    3 EXPERIMENTAL PROCEDURES AND RESULTS An AS4/8552 composite laminate of 18 mm in thickness consisting of 10 layers with different orientations was used to perform the DHD measurement, see Figure 2. To allow the measurement of residual stress using DHD, front and rear bushes were bonded using high strength adhesive to the specimen, centred on the location of the measurement.  The use of bushes has several benefits provide a setup for the fixation of the essential components for gun drilling and air probing and contribute to guide the hole saw perpendicularly to the specimen. Additionally, they decrease the effects of the air probe entrance and exit during the measurements of the diameters and help to avoid fibres delamination when the drill enters and exits the specimen.          C. Garza,  D.J. Smith,  A. Shterenlikht  and  M.J. Pavier           (a) (b)  Figure 2: (a) Illustration showing the layer arrangement specimens and the bushes required for a DHD experiment (b) Composite laminate after conducting the DHD experiment  After drilling the reference hole, the air probe was introduced to measure precisely the hole diameter every 22.5° around it and at every 0.1 mm through it, resulting in nine measurements of diameter in total for every axial position. The air probe is not able measure accurately near a surface, nevertheless the front and rear bushes allow measurements near the surface of the specimens.  A hole saw was selected to perform the trepanning process which has the advantages of being faster than electrical discharge machining (EDM) and not requiring an electrolyte to be used. The hole saw used during the experiment has a diameter of 10 mm and was diamond tipped. Following the trepanning procedure, the diameter of the hole was re-measured using the air probe.  Lastly, the residual stresses were determined from the radial distortions of the reference hole to reveal the residual stress distributions shown in Fig 4. The principal material directions have been used in each layer. Therefore, for stresses within the 0° layers, the  ** stress component is the stress in the fibre direction while for stresses within the 90° layers, the stress component AA is the stress in the transverse direction. The experimental results are compared to Laminator (software based on classical laminate theory) predictions and DHD simulations using the same and different reference hole and trepan diameters as in the experiments.  The highest and lowest predicted stresses in the longitudinal direction are of the order of 20 and 65 MPa in compression, in the 0° and 90° plies respectively. On the other hand, the expected stresses in the transverse direction remained approximately on 36-38 MPa on the specimen. The predicted magnitude of the shear stress is very low throughout the entire laminate.     20th International Conference on Composite Materials Copenhagen, 19-24th July 2015       (a)               (b)                (c)      Figure 3: Comparison of the determined residual stresses ** (a), AA (b) and in-plane shear *A (c) using Laminator, DHD experiment and DHD simulations with different reference hole and trepan diameters.   C. Garza,  D.J. Smith,  A. Shterenlikht  and  M.J. Pavier  A comparison between the DHD experiment and the DHD simulation using a reference hole of 3 mm diameter and a trepan diameter of 10 mm shows a close agreement in the longitudinal and transverse components as well as the in-plane shear component. However, these values significantly disagree with residual stress predictions using Laminator, which suggests that a considerable amount of residual stresses were not relaxed after trepanning the core. This issue can be resolved by using a smaller dimension for the reference hole and trepan diameters. After selecting 0.5 mm and 1 mm for the reference hole and trepan diameters respectively in a further DHD simulation the disagreement between the obtained results and Laminator predictions did not exceed a value of 5 MPa in all cases.  4 CONCLUSIONS The deep-hole drilling technique has become a standard method for the measurement of residual stress in isotropic materials, especially for thick components. The work described here is an extension to the method to allow the measurement of residual stress in orthotropic materials such as thick composite laminates.  After conducting a deep-hole drilling experiment on an 18 mm thick AS4/8552 composite plate, measurements showed a good agreement with a simulation using the same reference hole and trepan parameters, but a significant discrepancy was found when compared with Laminator predictions. It was determined that, when using DHD in laminated materials, the reference hole and trepan diameters must be much smaller than the thickness of the layers in order to reduce the effect of remaining interlaminar shear stresses in trepanned cores which can significantly lead to inaccurate measurements.  ACKNOWLEDGEMENTS The authors would like to acknowledge VEQTER Ltd for providing technical support for the experimental study. The financial support from the National Council for Science and Technology (CONACyT), the Institute of Innovation and Technology Transfer (I2T2) and the Government of Nuevo León is likewise gratefully acknowledged.  REFERENCES [1]  A. Mirzaee-Sisan, A.J. Fookes, C.E. Truman, D.J. Smith, T.B. Brown, and T.A. Dauda. Residual stress measurement in a repair welded header in the as-welded condition and after advanced post weld treatment. International Journal of Pressure Vessels and Piping, 84(5):265–273, 2007. [2]  M.G. Bateman, O.H. Miller, T.J. Palmer, C.E.P. Breen, E.J. Kingston, D.J. Smith, and M.J. Pavier. Measurement of residual stress in thick section composite laminates using the deep-hole method. International Journal of Mechanical Sciences, 47(11):1718–1739, 2005. [3]  P.J. Bouchard, D. George, J.R. Santisteban, G. Bruno, M. Dutta, L. Edwards, E. Kingston, and D.J. Smith. Measurement of the residual stresses in a stainless steel pipe girth weld containing long and short repairs. International Journal of Pressure Vessels and Piping, 82(4):299–310, 2005. [4]  T.B. Brown, T.A. Dauda, C.E. Truman, D.J. Smith, D. Memhard, and W. Pfeiffer. Predictions and measurements of residual stress in repair welds in plates. International Journal of Pressure Vessels and Piping, 83(11-12):809–818, 2006. [5]  D. George and D.J. Smith. Through thickness measurement of residual stresses in a stainless steel cylinder containing shallow and deep weld repairs. International Journal of Pressure Vessels and Piping, 82(4):279–287, 2005. [6]  D. Stefanescu, P. Browne, C.E. Truman, and D.J. Smith. Residual stress measurement within a European UIC60 rail using integrated drilling techniques. Materials Science Forum, 440-441:85–92, 2003.  

Measurement of in-plane residual stresses in an AS4/8552 composite laminate using the deep-hole drilling method

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Measurement of in-plane residual stresses in an AS4/8552 composite laminate using the deep-hole drilling method

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