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You searched for subject:(compression after impact). Showing records 1 – 23 of 23 total matches.

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California State University – Sacramento

1. Butler, Adalbert E. Peridynamic prediction of compression and impact strength of carbon fiber reinforced plastic panels.

Degree: MS, Mechanical Engineeering, 2013, California State University – Sacramento

 Peridynamic theory is an alternative theory of continuum mechanics that utilizes integral equations in place of problematic spatial derivatives in areas of material discontinuity. By… (more)

Subjects/Keywords: CAI; Compression after impact; Carbon fiber panel

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APA (6th Edition):

Butler, A. E. (2013). Peridynamic prediction of compression and impact strength of carbon fiber reinforced plastic panels. (Masters Thesis). California State University – Sacramento. Retrieved from http://hdl.handle.net/10211.9/2048

Chicago Manual of Style (16th Edition):

Butler, Adalbert E. “Peridynamic prediction of compression and impact strength of carbon fiber reinforced plastic panels.” 2013. Masters Thesis, California State University – Sacramento. Accessed October 23, 2020. http://hdl.handle.net/10211.9/2048.

MLA Handbook (7th Edition):

Butler, Adalbert E. “Peridynamic prediction of compression and impact strength of carbon fiber reinforced plastic panels.” 2013. Web. 23 Oct 2020.

Vancouver:

Butler AE. Peridynamic prediction of compression and impact strength of carbon fiber reinforced plastic panels. [Internet] [Masters thesis]. California State University – Sacramento; 2013. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/10211.9/2048.

Council of Science Editors:

Butler AE. Peridynamic prediction of compression and impact strength of carbon fiber reinforced plastic panels. [Masters Thesis]. California State University – Sacramento; 2013. Available from: http://hdl.handle.net/10211.9/2048


Cornell University

2. Hasseldine, Benjamin. Compression After Impact Of Sandwich Composite Panels With Thick Facesheets.

Degree: PhD, Mechanical Engineering, 2015, Cornell University

 Despite the numerous advantages that sandwich composites offer in transport structures over traditional metallic structures, they remain highly susceptible to low-energy impact damage, resulting in… (more)

Subjects/Keywords: sandwich composites; compression after impact; low energy impact

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APA (6th Edition):

Hasseldine, B. (2015). Compression After Impact Of Sandwich Composite Panels With Thick Facesheets. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/40605

Chicago Manual of Style (16th Edition):

Hasseldine, Benjamin. “Compression After Impact Of Sandwich Composite Panels With Thick Facesheets.” 2015. Doctoral Dissertation, Cornell University. Accessed October 23, 2020. http://hdl.handle.net/1813/40605.

MLA Handbook (7th Edition):

Hasseldine, Benjamin. “Compression After Impact Of Sandwich Composite Panels With Thick Facesheets.” 2015. Web. 23 Oct 2020.

Vancouver:

Hasseldine B. Compression After Impact Of Sandwich Composite Panels With Thick Facesheets. [Internet] [Doctoral dissertation]. Cornell University; 2015. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/1813/40605.

Council of Science Editors:

Hasseldine B. Compression After Impact Of Sandwich Composite Panels With Thick Facesheets. [Doctoral Dissertation]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/40605

3. GARCíA PEREZ, Pablo. Méthodologie expérimentale et numérique pour la tenue résiduelle post impact des structures composites à matrice thermoplastique : Experimental and numerical analysis of the residual strength of impacted thermoplastic composites.

Degree: Docteur es, Mécanique-matériaux, 2018, Paris, ENSAM

Les composites thermoplastiques sont de plus en plus privilégiées dans les structures aérospatiales au vue de leur tolérance aux dommages améliorée par rapport aux résines… (more)

Subjects/Keywords: Thermoplastiques; Endommagement; Thermographie infrarouge; Impact; Compression après impact; Thermoplastics; Damage criteria; Infra-Red thermography; Impact; Compression after impact

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APA (6th Edition):

GARCíA PEREZ, P. (2018). Méthodologie expérimentale et numérique pour la tenue résiduelle post impact des structures composites à matrice thermoplastique : Experimental and numerical analysis of the residual strength of impacted thermoplastic composites. (Doctoral Dissertation). Paris, ENSAM. Retrieved from http://www.theses.fr/2018ENAM0050

Chicago Manual of Style (16th Edition):

GARCíA PEREZ, Pablo. “Méthodologie expérimentale et numérique pour la tenue résiduelle post impact des structures composites à matrice thermoplastique : Experimental and numerical analysis of the residual strength of impacted thermoplastic composites.” 2018. Doctoral Dissertation, Paris, ENSAM. Accessed October 23, 2020. http://www.theses.fr/2018ENAM0050.

MLA Handbook (7th Edition):

GARCíA PEREZ, Pablo. “Méthodologie expérimentale et numérique pour la tenue résiduelle post impact des structures composites à matrice thermoplastique : Experimental and numerical analysis of the residual strength of impacted thermoplastic composites.” 2018. Web. 23 Oct 2020.

Vancouver:

GARCíA PEREZ P. Méthodologie expérimentale et numérique pour la tenue résiduelle post impact des structures composites à matrice thermoplastique : Experimental and numerical analysis of the residual strength of impacted thermoplastic composites. [Internet] [Doctoral dissertation]. Paris, ENSAM; 2018. [cited 2020 Oct 23]. Available from: http://www.theses.fr/2018ENAM0050.

Council of Science Editors:

GARCíA PEREZ P. Méthodologie expérimentale et numérique pour la tenue résiduelle post impact des structures composites à matrice thermoplastique : Experimental and numerical analysis of the residual strength of impacted thermoplastic composites. [Doctoral Dissertation]. Paris, ENSAM; 2018. Available from: http://www.theses.fr/2018ENAM0050


Loughborough University

4. Lloyd, James C. Impact damage and damage tolerance of fibre reinforced advanced composite laminate structures.

Degree: PhD, 2002, Loughborough University

 The primary objective of this work is to experimentally examine the effect of various geometric parameters on the impact damage and damage tolerance of thin… (more)

Subjects/Keywords: 620; Compression after impact

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APA (6th Edition):

Lloyd, J. C. (2002). Impact damage and damage tolerance of fibre reinforced advanced composite laminate structures. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/6891

Chicago Manual of Style (16th Edition):

Lloyd, James C. “Impact damage and damage tolerance of fibre reinforced advanced composite laminate structures.” 2002. Doctoral Dissertation, Loughborough University. Accessed October 23, 2020. http://hdl.handle.net/2134/6891.

MLA Handbook (7th Edition):

Lloyd, James C. “Impact damage and damage tolerance of fibre reinforced advanced composite laminate structures.” 2002. Web. 23 Oct 2020.

Vancouver:

Lloyd JC. Impact damage and damage tolerance of fibre reinforced advanced composite laminate structures. [Internet] [Doctoral dissertation]. Loughborough University; 2002. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/2134/6891.

Council of Science Editors:

Lloyd JC. Impact damage and damage tolerance of fibre reinforced advanced composite laminate structures. [Doctoral Dissertation]. Loughborough University; 2002. Available from: http://hdl.handle.net/2134/6891


Loughborough University

5. James, Chris T. Numerical modelling of the compression-after-impact behaviour of composite sandwich panels.

Degree: PhD, 2015, Loughborough University

 Sandwich panels using fibre-reinforced composite skins and low-density cores are being increasingly used in the aerospace industry due to their superior specific strength and stiffness,… (more)

Subjects/Keywords: 629.1; Composite sandwich panels; Compression-after-impact; Numerical modelling; Delamination

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APA (6th Edition):

James, C. T. (2015). Numerical modelling of the compression-after-impact behaviour of composite sandwich panels. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/17994

Chicago Manual of Style (16th Edition):

James, Chris T. “Numerical modelling of the compression-after-impact behaviour of composite sandwich panels.” 2015. Doctoral Dissertation, Loughborough University. Accessed October 23, 2020. http://hdl.handle.net/2134/17994.

MLA Handbook (7th Edition):

James, Chris T. “Numerical modelling of the compression-after-impact behaviour of composite sandwich panels.” 2015. Web. 23 Oct 2020.

Vancouver:

James CT. Numerical modelling of the compression-after-impact behaviour of composite sandwich panels. [Internet] [Doctoral dissertation]. Loughborough University; 2015. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/2134/17994.

Council of Science Editors:

James CT. Numerical modelling of the compression-after-impact behaviour of composite sandwich panels. [Doctoral Dissertation]. Loughborough University; 2015. Available from: http://hdl.handle.net/2134/17994


University of New South Wales

6. Aryal, Binod. Mechanical Behaviour of Carbon Fibre Reinforced Laminates and Honeycomb Sandwich Panels Subjected to Low-Velocity and High-Velocity Ballistic Impacts.

Degree: Engineering & Information Technology, 2019, University of New South Wales

 Structural response of composite structures subjected to different impact loadings is studied. The low-velocity and high-velocity ballistic impacts, and residual structural response are analysed. First,… (more)

Subjects/Keywords: Compression-after-impact testing; Ballistic impact; Honeycomb sandwich panels; Finite-element analysis; Low-velocity impact; Damage analysis; Equivalent-energy impact; Delamination

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APA (6th Edition):

Aryal, B. (2019). Mechanical Behaviour of Carbon Fibre Reinforced Laminates and Honeycomb Sandwich Panels Subjected to Low-Velocity and High-Velocity Ballistic Impacts. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/64861 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:62810/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Aryal, Binod. “Mechanical Behaviour of Carbon Fibre Reinforced Laminates and Honeycomb Sandwich Panels Subjected to Low-Velocity and High-Velocity Ballistic Impacts.” 2019. Doctoral Dissertation, University of New South Wales. Accessed October 23, 2020. http://handle.unsw.edu.au/1959.4/64861 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:62810/SOURCE02?view=true.

MLA Handbook (7th Edition):

Aryal, Binod. “Mechanical Behaviour of Carbon Fibre Reinforced Laminates and Honeycomb Sandwich Panels Subjected to Low-Velocity and High-Velocity Ballistic Impacts.” 2019. Web. 23 Oct 2020.

Vancouver:

Aryal B. Mechanical Behaviour of Carbon Fibre Reinforced Laminates and Honeycomb Sandwich Panels Subjected to Low-Velocity and High-Velocity Ballistic Impacts. [Internet] [Doctoral dissertation]. University of New South Wales; 2019. [cited 2020 Oct 23]. Available from: http://handle.unsw.edu.au/1959.4/64861 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:62810/SOURCE02?view=true.

Council of Science Editors:

Aryal B. Mechanical Behaviour of Carbon Fibre Reinforced Laminates and Honeycomb Sandwich Panels Subjected to Low-Velocity and High-Velocity Ballistic Impacts. [Doctoral Dissertation]. University of New South Wales; 2019. Available from: http://handle.unsw.edu.au/1959.4/64861 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:62810/SOURCE02?view=true


Virginia Tech

7. Mcquigg, Thomas Dale. Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets.

Degree: PhD, Aerospace and Ocean Engineering, 2011, Virginia Tech

 A better understanding of the effect of impact damage on composite structures is necessary to give the engineer an ability to design safe, efficient structures.… (more)

Subjects/Keywords: Honeycomb Core Sandwich Panels; Compression After Impact; Damage Tolerance; Finite Element Analysis; Multicontinuum Failure Theory

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APA (6th Edition):

Mcquigg, T. D. (2011). Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77106

Chicago Manual of Style (16th Edition):

Mcquigg, Thomas Dale. “Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets.” 2011. Doctoral Dissertation, Virginia Tech. Accessed October 23, 2020. http://hdl.handle.net/10919/77106.

MLA Handbook (7th Edition):

Mcquigg, Thomas Dale. “Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets.” 2011. Web. 23 Oct 2020.

Vancouver:

Mcquigg TD. Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/10919/77106.

Council of Science Editors:

Mcquigg TD. Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/77106

8. Hongkarnjanakul, Natthawat. Modélisation numérique pour la tolérance aux dommages d’impact sur stratifié composite : de l’impact à la résistance résiduelle en compression : Numerical modeling for impact damage tolerance on composite laminate : from impact to compressive residual strength.

Degree: Docteur es, Génie mécanique, mécanique des matériaux, 2013, Toulouse, ISAE

Les impacts sur structures composites peuvent fortement diminuer leur résistance résiduelle sans laisser de marque visible sur la surface extérieure. Dans le domaine aéronautique, un… (more)

Subjects/Keywords: Tolérance aux dommages; Impact; Composite; Compression après impact; Indentation permanente; Eléments finis; Damage tolerance; Impact; Composite; Compression after impact; Permanent indentation; Finite element; 620.1

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APA (6th Edition):

Hongkarnjanakul, N. (2013). Modélisation numérique pour la tolérance aux dommages d’impact sur stratifié composite : de l’impact à la résistance résiduelle en compression : Numerical modeling for impact damage tolerance on composite laminate : from impact to compressive residual strength. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2013ESAE0037

Chicago Manual of Style (16th Edition):

Hongkarnjanakul, Natthawat. “Modélisation numérique pour la tolérance aux dommages d’impact sur stratifié composite : de l’impact à la résistance résiduelle en compression : Numerical modeling for impact damage tolerance on composite laminate : from impact to compressive residual strength.” 2013. Doctoral Dissertation, Toulouse, ISAE. Accessed October 23, 2020. http://www.theses.fr/2013ESAE0037.

MLA Handbook (7th Edition):

Hongkarnjanakul, Natthawat. “Modélisation numérique pour la tolérance aux dommages d’impact sur stratifié composite : de l’impact à la résistance résiduelle en compression : Numerical modeling for impact damage tolerance on composite laminate : from impact to compressive residual strength.” 2013. Web. 23 Oct 2020.

Vancouver:

Hongkarnjanakul N. Modélisation numérique pour la tolérance aux dommages d’impact sur stratifié composite : de l’impact à la résistance résiduelle en compression : Numerical modeling for impact damage tolerance on composite laminate : from impact to compressive residual strength. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2013. [cited 2020 Oct 23]. Available from: http://www.theses.fr/2013ESAE0037.

Council of Science Editors:

Hongkarnjanakul N. Modélisation numérique pour la tolérance aux dommages d’impact sur stratifié composite : de l’impact à la résistance résiduelle en compression : Numerical modeling for impact damage tolerance on composite laminate : from impact to compressive residual strength. [Doctoral Dissertation]. Toulouse, ISAE; 2013. Available from: http://www.theses.fr/2013ESAE0037


University of Manchester

9. Selver, Erdem. Tow level hybridisation for damage tolerant composites.

Degree: PhD, 2014, University of Manchester

 Fibre reinforced composites have higher specific strength and stiffness in comparison to metals. However, composites are susceptible to impact damage resulting in degradation of mechanical… (more)

Subjects/Keywords: 620.1; Hybrid yarns; Commingling; Core-wrapping; Impact tolerance; Damage tolerance; Composite healing; Polypropylene; High modulus polypropylene; Glass fibre; Non-crimp; Low velocity impact; High velocity impact; Compression after impact

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APA (6th Edition):

Selver, E. (2014). Tow level hybridisation for damage tolerant composites. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/tow-level-hybridisation-for-damage-tolerant-composites(8cf53f8c-165f-4e8b-b67f-f8fd34c327e2).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.677727

Chicago Manual of Style (16th Edition):

Selver, Erdem. “Tow level hybridisation for damage tolerant composites.” 2014. Doctoral Dissertation, University of Manchester. Accessed October 23, 2020. https://www.research.manchester.ac.uk/portal/en/theses/tow-level-hybridisation-for-damage-tolerant-composites(8cf53f8c-165f-4e8b-b67f-f8fd34c327e2).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.677727.

MLA Handbook (7th Edition):

Selver, Erdem. “Tow level hybridisation for damage tolerant composites.” 2014. Web. 23 Oct 2020.

Vancouver:

Selver E. Tow level hybridisation for damage tolerant composites. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2020 Oct 23]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/tow-level-hybridisation-for-damage-tolerant-composites(8cf53f8c-165f-4e8b-b67f-f8fd34c327e2).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.677727.

Council of Science Editors:

Selver E. Tow level hybridisation for damage tolerant composites. [Doctoral Dissertation]. University of Manchester; 2014. Available from: https://www.research.manchester.ac.uk/portal/en/theses/tow-level-hybridisation-for-damage-tolerant-composites(8cf53f8c-165f-4e8b-b67f-f8fd34c327e2).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.677727


Loughborough University

10. Nash, Peter. Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels.

Degree: PhD, 2016, Loughborough University

 This thesis presents the work of an experimental investigation into the impact damage resistance and damage tolerance for symmetrical and unsymmetrical composite honeycomb sandwich panels… (more)

Subjects/Keywords: 629.134; Unsymmetrical sandwich panel; Honeycomb; Carbon fibre; E-glass fibre; Impact damage; Damage mechanisms; Energy absorption; Damage tolerance; Compression-after-impact; In-plane compression; Skin-core interaction

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APA (6th Edition):

Nash, P. (2016). Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/21748

Chicago Manual of Style (16th Edition):

Nash, Peter. “Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels.” 2016. Doctoral Dissertation, Loughborough University. Accessed October 23, 2020. http://hdl.handle.net/2134/21748.

MLA Handbook (7th Edition):

Nash, Peter. “Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels.” 2016. Web. 23 Oct 2020.

Vancouver:

Nash P. Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels. [Internet] [Doctoral dissertation]. Loughborough University; 2016. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/2134/21748.

Council of Science Editors:

Nash P. Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels. [Doctoral Dissertation]. Loughborough University; 2016. Available from: http://hdl.handle.net/2134/21748


Brigham Young University

11. Allen, Devin Nelson. Damage Tolerance of Unidirectional Basalt/Epoxy Composites In Co-Cured Aramid Sleeves.

Degree: MS, 2011, Brigham Young University

  Unidirectional basalt fiber rods consolidated with an aramid sleeve were measured for compression strength after impact at various energy levels and compared to undamaged… (more)

Subjects/Keywords: basalt composites; damage tolerance; IsoTruss; compression strength after impact; unidirectional; Kevlar sleeves; Civil and Environmental Engineering

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APA (6th Edition):

Allen, D. N. (2011). Damage Tolerance of Unidirectional Basalt/Epoxy Composites In Co-Cured Aramid Sleeves. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4157&context=etd

Chicago Manual of Style (16th Edition):

Allen, Devin Nelson. “Damage Tolerance of Unidirectional Basalt/Epoxy Composites In Co-Cured Aramid Sleeves.” 2011. Masters Thesis, Brigham Young University. Accessed October 23, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4157&context=etd.

MLA Handbook (7th Edition):

Allen, Devin Nelson. “Damage Tolerance of Unidirectional Basalt/Epoxy Composites In Co-Cured Aramid Sleeves.” 2011. Web. 23 Oct 2020.

Vancouver:

Allen DN. Damage Tolerance of Unidirectional Basalt/Epoxy Composites In Co-Cured Aramid Sleeves. [Internet] [Masters thesis]. Brigham Young University; 2011. [cited 2020 Oct 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4157&context=etd.

Council of Science Editors:

Allen DN. Damage Tolerance of Unidirectional Basalt/Epoxy Composites In Co-Cured Aramid Sleeves. [Masters Thesis]. Brigham Young University; 2011. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4157&context=etd


Brigham Young University

12. Sika, Charles Andrew. Damage Tolerance of Unidirectional Carbon and Fiberglass Composites with Aramid Sleeves.

Degree: MS, 2012, Brigham Young University

  Unidirectional carbon fiber and fiberglass epoxy composite elements consolidated with aramid sleeves were radially impacted at 5 J (3.7 ft-lbs) and 10 J (7.4… (more)

Subjects/Keywords: carbon; fiberglass; fiber/epoxy composite; damage tolerance; IsoTruss®; compression strength after impact (CSAI); unidirectional; kevlar/aramid sleeves; Civil and Environmental Engineering

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APA (6th Edition):

Sika, C. A. (2012). Damage Tolerance of Unidirectional Carbon and Fiberglass Composites with Aramid Sleeves. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4430&context=etd

Chicago Manual of Style (16th Edition):

Sika, Charles Andrew. “Damage Tolerance of Unidirectional Carbon and Fiberglass Composites with Aramid Sleeves.” 2012. Masters Thesis, Brigham Young University. Accessed October 23, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4430&context=etd.

MLA Handbook (7th Edition):

Sika, Charles Andrew. “Damage Tolerance of Unidirectional Carbon and Fiberglass Composites with Aramid Sleeves.” 2012. Web. 23 Oct 2020.

Vancouver:

Sika CA. Damage Tolerance of Unidirectional Carbon and Fiberglass Composites with Aramid Sleeves. [Internet] [Masters thesis]. Brigham Young University; 2012. [cited 2020 Oct 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4430&context=etd.

Council of Science Editors:

Sika CA. Damage Tolerance of Unidirectional Carbon and Fiberglass Composites with Aramid Sleeves. [Masters Thesis]. Brigham Young University; 2012. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4430&context=etd


Loughborough University

13. Rivera, Luis A. In-plane compression of preconditioned carbon/epoxy panels.

Degree: PhD, 2004, Loughborough University

 This thesis investigates the effects of damage characteristics on residual compressive strength (RCS) of 4-mm thick preconditioned carbon/epoxy quasi-isotropic panels through the study of their… (more)

Subjects/Keywords: 620.193; Composite panels; Impact damage; Delamination; Topology change; Open hole; Buckling; Compression-after-impact; Damage tolerance; Compression-after-impact prediction

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APA (6th Edition):

Rivera, L. A. (2004). In-plane compression of preconditioned carbon/epoxy panels. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/20136

Chicago Manual of Style (16th Edition):

Rivera, Luis A. “In-plane compression of preconditioned carbon/epoxy panels.” 2004. Doctoral Dissertation, Loughborough University. Accessed October 23, 2020. http://hdl.handle.net/2134/20136.

MLA Handbook (7th Edition):

Rivera, Luis A. “In-plane compression of preconditioned carbon/epoxy panels.” 2004. Web. 23 Oct 2020.

Vancouver:

Rivera LA. In-plane compression of preconditioned carbon/epoxy panels. [Internet] [Doctoral dissertation]. Loughborough University; 2004. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/2134/20136.

Council of Science Editors:

Rivera LA. In-plane compression of preconditioned carbon/epoxy panels. [Doctoral Dissertation]. Loughborough University; 2004. Available from: http://hdl.handle.net/2134/20136


Wayne State University

14. Dhaliwal, Gurpinder Singh. Static And Dynamic Behavior Of Carbon Fiber Reinforced Aluminum (carall) Laminates.

Degree: PhD, Mechanical Engineering, 2016, Wayne State University

  STATIC AND DYNAMIC BEHAVIOUR OF CARBON FIBER REINFORCED ALUMINUM (CARALL) LAMINATES by GURPINDER SINGH DHALIWAL Advisor: Dr. Golam Newaz Major: Mechanical Engineering Degree: Doctor… (more)

Subjects/Keywords: Carbon Fiber Reinforced Aluminum Laminates; Compression after Impact; C-scan; Finite element Modeling; Low velocity Impact; Materials Science and Engineering; Mechanical Engineering; Other Mechanical Engineering

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APA (6th Edition):

Dhaliwal, G. S. (2016). Static And Dynamic Behavior Of Carbon Fiber Reinforced Aluminum (carall) Laminates. (Doctoral Dissertation). Wayne State University. Retrieved from https://digitalcommons.wayne.edu/oa_dissertations/1525

Chicago Manual of Style (16th Edition):

Dhaliwal, Gurpinder Singh. “Static And Dynamic Behavior Of Carbon Fiber Reinforced Aluminum (carall) Laminates.” 2016. Doctoral Dissertation, Wayne State University. Accessed October 23, 2020. https://digitalcommons.wayne.edu/oa_dissertations/1525.

MLA Handbook (7th Edition):

Dhaliwal, Gurpinder Singh. “Static And Dynamic Behavior Of Carbon Fiber Reinforced Aluminum (carall) Laminates.” 2016. Web. 23 Oct 2020.

Vancouver:

Dhaliwal GS. Static And Dynamic Behavior Of Carbon Fiber Reinforced Aluminum (carall) Laminates. [Internet] [Doctoral dissertation]. Wayne State University; 2016. [cited 2020 Oct 23]. Available from: https://digitalcommons.wayne.edu/oa_dissertations/1525.

Council of Science Editors:

Dhaliwal GS. Static And Dynamic Behavior Of Carbon Fiber Reinforced Aluminum (carall) Laminates. [Doctoral Dissertation]. Wayne State University; 2016. Available from: https://digitalcommons.wayne.edu/oa_dissertations/1525


Louisiana State University

15. Muthyala, Venkata Dinesh. Composite sandwich structure with grid stiffened core.

Degree: MSME, Mechanical Engineering, 2007, Louisiana State University

 Composite sandwich structures have been widely used in aerospace structures, ship building, infrastructure, etc. due to their light weight and high strength to weight ratio.… (more)

Subjects/Keywords: Grids; Sandwich Structures; Compression After impact; Impact Testing; C-Scan

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APA (6th Edition):

Muthyala, V. D. (2007). Composite sandwich structure with grid stiffened core. (Masters Thesis). Louisiana State University. Retrieved from etd-11162007-094553 ; https://digitalcommons.lsu.edu/gradschool_theses/552

Chicago Manual of Style (16th Edition):

Muthyala, Venkata Dinesh. “Composite sandwich structure with grid stiffened core.” 2007. Masters Thesis, Louisiana State University. Accessed October 23, 2020. etd-11162007-094553 ; https://digitalcommons.lsu.edu/gradschool_theses/552.

MLA Handbook (7th Edition):

Muthyala, Venkata Dinesh. “Composite sandwich structure with grid stiffened core.” 2007. Web. 23 Oct 2020.

Vancouver:

Muthyala VD. Composite sandwich structure with grid stiffened core. [Internet] [Masters thesis]. Louisiana State University; 2007. [cited 2020 Oct 23]. Available from: etd-11162007-094553 ; https://digitalcommons.lsu.edu/gradschool_theses/552.

Council of Science Editors:

Muthyala VD. Composite sandwich structure with grid stiffened core. [Masters Thesis]. Louisiana State University; 2007. Available from: etd-11162007-094553 ; https://digitalcommons.lsu.edu/gradschool_theses/552


Brigham Young University

16. Oxborrow, Ian Michael. Axial Compression Behavior of Unidirectional Carbon/Epoxy Tubes and Rods Before and After Impact.

Degree: MS, 2014, Brigham Young University

Compression tests were performed on damaged and undamaged rods and tubes made from unidirectional carbon/epoxy composite and lightweight core materials. Tested samples represent local members… (more)

Subjects/Keywords: carbon; fiber/epoxy composite; damage tolerance; IsoTruss®; compression strength after impact (CSAI); unidirectional; tube; rod; buckling; length; Southwell plot; Civil and Environmental Engineering

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APA (6th Edition):

Oxborrow, I. M. (2014). Axial Compression Behavior of Unidirectional Carbon/Epoxy Tubes and Rods Before and After Impact. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6548&context=etd

Chicago Manual of Style (16th Edition):

Oxborrow, Ian Michael. “Axial Compression Behavior of Unidirectional Carbon/Epoxy Tubes and Rods Before and After Impact.” 2014. Masters Thesis, Brigham Young University. Accessed October 23, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6548&context=etd.

MLA Handbook (7th Edition):

Oxborrow, Ian Michael. “Axial Compression Behavior of Unidirectional Carbon/Epoxy Tubes and Rods Before and After Impact.” 2014. Web. 23 Oct 2020.

Vancouver:

Oxborrow IM. Axial Compression Behavior of Unidirectional Carbon/Epoxy Tubes and Rods Before and After Impact. [Internet] [Masters thesis]. Brigham Young University; 2014. [cited 2020 Oct 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6548&context=etd.

Council of Science Editors:

Oxborrow IM. Axial Compression Behavior of Unidirectional Carbon/Epoxy Tubes and Rods Before and After Impact. [Masters Thesis]. Brigham Young University; 2014. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=6548&context=etd


Brigham Young University

17. Embley, Michael D. Damage Tolerance of Buckling-Critical Unidirectional Carbon, Glass,and Basalt Fiber Composites in Co-Cured Aramid Sleeves.

Degree: MS, 2011, Brigham Young University

Compression strength after impact tests were conducted on unidirectional composite rods with sleeves. These elements represent local members of open three-dimensional composite lattice structures… (more)

Subjects/Keywords: carbon; glass; basalt; fiber/epoxy composite; damage tolerance; IsoTruss®; compression strength after impact (CSAI); unidirectional; aramid/kevlar sleeves; Civil and Environmental Engineering

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APA (6th Edition):

Embley, M. D. (2011). Damage Tolerance of Buckling-Critical Unidirectional Carbon, Glass,and Basalt Fiber Composites in Co-Cured Aramid Sleeves. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4184&context=etd

Chicago Manual of Style (16th Edition):

Embley, Michael D. “Damage Tolerance of Buckling-Critical Unidirectional Carbon, Glass,and Basalt Fiber Composites in Co-Cured Aramid Sleeves.” 2011. Masters Thesis, Brigham Young University. Accessed October 23, 2020. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4184&context=etd.

MLA Handbook (7th Edition):

Embley, Michael D. “Damage Tolerance of Buckling-Critical Unidirectional Carbon, Glass,and Basalt Fiber Composites in Co-Cured Aramid Sleeves.” 2011. Web. 23 Oct 2020.

Vancouver:

Embley MD. Damage Tolerance of Buckling-Critical Unidirectional Carbon, Glass,and Basalt Fiber Composites in Co-Cured Aramid Sleeves. [Internet] [Masters thesis]. Brigham Young University; 2011. [cited 2020 Oct 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4184&context=etd.

Council of Science Editors:

Embley MD. Damage Tolerance of Buckling-Critical Unidirectional Carbon, Glass,and Basalt Fiber Composites in Co-Cured Aramid Sleeves. [Masters Thesis]. Brigham Young University; 2011. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4184&context=etd


Loughborough University

18. Hill, Michelle Denise. Damage resistance and tolerance investigation of carbon/epoxy skinned honeycomb sandwich panels.

Degree: PhD, 2007, Loughborough University

 This thesis documents the findings of a three year experimental investigation into the impact damage resistance and damage tolerance of composite honeycomb sandwich panels. The… (more)

Subjects/Keywords: 629.1341; Sandwich panel; Honeycomb; Carbon fibre; Composite; Low-velocity impact; Damage mechanisms; Energy absorption; In-plane compression; Compression-after-impact

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APA (6th Edition):

Hill, M. D. (2007). Damage resistance and tolerance investigation of carbon/epoxy skinned honeycomb sandwich panels. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/10072

Chicago Manual of Style (16th Edition):

Hill, Michelle Denise. “Damage resistance and tolerance investigation of carbon/epoxy skinned honeycomb sandwich panels.” 2007. Doctoral Dissertation, Loughborough University. Accessed October 23, 2020. http://hdl.handle.net/2134/10072.

MLA Handbook (7th Edition):

Hill, Michelle Denise. “Damage resistance and tolerance investigation of carbon/epoxy skinned honeycomb sandwich panels.” 2007. Web. 23 Oct 2020.

Vancouver:

Hill MD. Damage resistance and tolerance investigation of carbon/epoxy skinned honeycomb sandwich panels. [Internet] [Doctoral dissertation]. Loughborough University; 2007. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/2134/10072.

Council of Science Editors:

Hill MD. Damage resistance and tolerance investigation of carbon/epoxy skinned honeycomb sandwich panels. [Doctoral Dissertation]. Loughborough University; 2007. Available from: http://hdl.handle.net/2134/10072


Universitat de Girona

19. Liv, Yi. A contribution to the understanding of compression after impact of composite laminates.

Degree: Departament de Física, 2017, Universitat de Girona

 Els impactes de baixa velocitat en estructures de materials compostos representen una greu amenaça per a la indústria aeroespacial i és un tema d'interès per… (more)

Subjects/Keywords: Impact; Impacte; Impacto; Non-destructive inspection; Assaig no destructiu; Ensayo no destructivo; Finite element analysis; Anàlisi d'elements finits; Análisis de elementos finitos; Compression after impact; Compressió després de l'impacte; Compresión después de impacto; Damage mechanisms; Mecanisme de danys; Mecanismo de daños; 53; 620

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APA (6th Edition):

Liv, Y. (2017). A contribution to the understanding of compression after impact of composite laminates. (Thesis). Universitat de Girona. Retrieved from http://hdl.handle.net/10803/461500

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Liv, Yi. “A contribution to the understanding of compression after impact of composite laminates.” 2017. Thesis, Universitat de Girona. Accessed October 23, 2020. http://hdl.handle.net/10803/461500.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Liv, Yi. “A contribution to the understanding of compression after impact of composite laminates.” 2017. Web. 23 Oct 2020.

Vancouver:

Liv Y. A contribution to the understanding of compression after impact of composite laminates. [Internet] [Thesis]. Universitat de Girona; 2017. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/10803/461500.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Liv Y. A contribution to the understanding of compression after impact of composite laminates. [Thesis]. Universitat de Girona; 2017. Available from: http://hdl.handle.net/10803/461500

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

20. Soto Masip, Albert. Development of efficient numerical models for the simulation of low velocity impact and compression after impact on composite structures.

Degree: Departament d'Enginyeria Mecànica i de la Construcció Industrial, 2018, Universitat de Girona

 Els materials compòsits són actualment utilitzats en diferents sectors industrials que busquen la reducció de pes estructural amb la finalitat de reduir el consum de… (more)

Subjects/Keywords: Composite materials; Materials compòsits; Materiales compuestos; Modelling; Modelatge; Modelado; Low velocity impact; Impactes a baixa velocitat; Impactos a baja velocidad; Compression after impact; Compressió després d'impacte; Compresión después de impacto; 620

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APA (6th Edition):

Soto Masip, A. (2018). Development of efficient numerical models for the simulation of low velocity impact and compression after impact on composite structures. (Thesis). Universitat de Girona. Retrieved from http://hdl.handle.net/10803/664503

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Soto Masip, Albert. “Development of efficient numerical models for the simulation of low velocity impact and compression after impact on composite structures.” 2018. Thesis, Universitat de Girona. Accessed October 23, 2020. http://hdl.handle.net/10803/664503.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Soto Masip, Albert. “Development of efficient numerical models for the simulation of low velocity impact and compression after impact on composite structures.” 2018. Web. 23 Oct 2020.

Vancouver:

Soto Masip A. Development of efficient numerical models for the simulation of low velocity impact and compression after impact on composite structures. [Internet] [Thesis]. Universitat de Girona; 2018. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/10803/664503.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Soto Masip A. Development of efficient numerical models for the simulation of low velocity impact and compression after impact on composite structures. [Thesis]. Universitat de Girona; 2018. Available from: http://hdl.handle.net/10803/664503

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Vanderbilt University

21. Krishnan, Arun. The Interfacial Failure of Bonded Materials and Composites.

Degree: PhD, Civil Engineering, 2010, Vanderbilt University

 Composites and adhesive joints are being increasingly used in modern structures. It becomes very important to characterize the failure in such materials especially at the… (more)

Subjects/Keywords: Mixed-mode Fracture; Compression-after-impact; Mode-II fracture toughness; Interfacial failure; composites; Multiscale Homogenization; Glass/Vinyl Ester composite

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APA (6th Edition):

Krishnan, A. (2010). The Interfacial Failure of Bonded Materials and Composites. (Doctoral Dissertation). Vanderbilt University. Retrieved from http://hdl.handle.net/1803/14970

Chicago Manual of Style (16th Edition):

Krishnan, Arun. “The Interfacial Failure of Bonded Materials and Composites.” 2010. Doctoral Dissertation, Vanderbilt University. Accessed October 23, 2020. http://hdl.handle.net/1803/14970.

MLA Handbook (7th Edition):

Krishnan, Arun. “The Interfacial Failure of Bonded Materials and Composites.” 2010. Web. 23 Oct 2020.

Vancouver:

Krishnan A. The Interfacial Failure of Bonded Materials and Composites. [Internet] [Doctoral dissertation]. Vanderbilt University; 2010. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/1803/14970.

Council of Science Editors:

Krishnan A. The Interfacial Failure of Bonded Materials and Composites. [Doctoral Dissertation]. Vanderbilt University; 2010. Available from: http://hdl.handle.net/1803/14970

22. Selver, Erdem. TOW LEVEL HYBRIDISATION FOR DAMAGE TOLERANT COMPOSITES.

Degree: 2014, University of Manchester

 Fibre reinforced composites have higher specific strength and stiffness in comparison to metals. However, composites are susceptible to impact damage resulting in degradation of mechanical… (more)

Subjects/Keywords: Hybrid yarns; Commingling; Core-wrapping; Impact tolerance; Damage tolerance; Composite healing; Polypropylene; High modulus polypropylene; Glass fibre; Non-crimp; Low velocity impact; High velocity impact; Compression after impact

…Resistance Glass Fibres CAI Compression after Impact CF Carbon Fibres cN CentiNewton COM… …compared with pristine glass laminates. Compression after impact (CAI) tests showed… …performing drop-weight impact tests, compression after impact (CAI) tests, tensile tests… …demonstrate the effect of the impact event on the compression and the compression after impact… …impact induced damage areas are healed and how the compression after impact strength of the… 

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APA (6th Edition):

Selver, E. (2014). TOW LEVEL HYBRIDISATION FOR DAMAGE TOLERANT COMPOSITES. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:238478

Chicago Manual of Style (16th Edition):

Selver, Erdem. “TOW LEVEL HYBRIDISATION FOR DAMAGE TOLERANT COMPOSITES.” 2014. Doctoral Dissertation, University of Manchester. Accessed October 23, 2020. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:238478.

MLA Handbook (7th Edition):

Selver, Erdem. “TOW LEVEL HYBRIDISATION FOR DAMAGE TOLERANT COMPOSITES.” 2014. Web. 23 Oct 2020.

Vancouver:

Selver E. TOW LEVEL HYBRIDISATION FOR DAMAGE TOLERANT COMPOSITES. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2020 Oct 23]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:238478.

Council of Science Editors:

Selver E. TOW LEVEL HYBRIDISATION FOR DAMAGE TOLERANT COMPOSITES. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:238478


Universitat de Girona

23. Sasikumar, Aravind. Improving compression after impact response of composite laminates through ply level hybridization with thin plies and unsymmetrical designs.

Degree: Departament d'Enginyeria Mecànica i de la Construcció Industrial, 2019, Universitat de Girona

 Los materiales compuestos son vulnerables a las cargas de impacto principalmente a causa de la reducción de la resistencia a la compresión después de impacto… (more)

Subjects/Keywords: Composite materials; Materials compostos; Materiales compuestos; Compression after impact; Compressió després d'impacte; Compresión después de impacto; Hybrid laminates; Laminats híbrids; Laminados híbridos; Thin plies; Capes primes; Capas delgadas; Unsymetrical design; Disseny asimètric; Diseño asimétrico; Optimization; Optimització; Optimización; Finite element analysis; Anàlisi d'elements finits; Análisis de elementos finitos; 62; 620

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APA (6th Edition):

Sasikumar, A. (2019). Improving compression after impact response of composite laminates through ply level hybridization with thin plies and unsymmetrical designs. (Thesis). Universitat de Girona. Retrieved from http://hdl.handle.net/10803/668987

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sasikumar, Aravind. “Improving compression after impact response of composite laminates through ply level hybridization with thin plies and unsymmetrical designs.” 2019. Thesis, Universitat de Girona. Accessed October 23, 2020. http://hdl.handle.net/10803/668987.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sasikumar, Aravind. “Improving compression after impact response of composite laminates through ply level hybridization with thin plies and unsymmetrical designs.” 2019. Web. 23 Oct 2020.

Vancouver:

Sasikumar A. Improving compression after impact response of composite laminates through ply level hybridization with thin plies and unsymmetrical designs. [Internet] [Thesis]. Universitat de Girona; 2019. [cited 2020 Oct 23]. Available from: http://hdl.handle.net/10803/668987.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sasikumar A. Improving compression after impact response of composite laminates through ply level hybridization with thin plies and unsymmetrical designs. [Thesis]. Universitat de Girona; 2019. Available from: http://hdl.handle.net/10803/668987

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

.