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You searched for subject:(Damage tolerance). Showing records 1 – 30 of 97 total matches.

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University of Bath

1. Baker, Neil. Techniques for optimisation and analysis of composite structures for damage tolerance and buckling stiffness.

Degree: PhD, 2012, University of Bath

 This thesis explores methods by which carbon fibre reinforced polymers may be fficiently designed with the inclusion of damage tolerance criteria. An efficient method of… (more)

Subjects/Keywords: 620.1920287; composites; structures; damage tolerance

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APA (6th Edition):

Baker, N. (2012). Techniques for optimisation and analysis of composite structures for damage tolerance and buckling stiffness. (Doctoral Dissertation). University of Bath. Retrieved from https://researchportal.bath.ac.uk/en/studentthesis/techniques-for-optimisation-and-analysis-of-composite-structures-for-damage-tolerance-and-buckling-stiffness(fce73472-2619-4b82-82b1-5d74312e613d).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.558887

Chicago Manual of Style (16th Edition):

Baker, Neil. “Techniques for optimisation and analysis of composite structures for damage tolerance and buckling stiffness.” 2012. Doctoral Dissertation, University of Bath. Accessed April 17, 2021. https://researchportal.bath.ac.uk/en/studentthesis/techniques-for-optimisation-and-analysis-of-composite-structures-for-damage-tolerance-and-buckling-stiffness(fce73472-2619-4b82-82b1-5d74312e613d).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.558887.

MLA Handbook (7th Edition):

Baker, Neil. “Techniques for optimisation and analysis of composite structures for damage tolerance and buckling stiffness.” 2012. Web. 17 Apr 2021.

Vancouver:

Baker N. Techniques for optimisation and analysis of composite structures for damage tolerance and buckling stiffness. [Internet] [Doctoral dissertation]. University of Bath; 2012. [cited 2021 Apr 17]. Available from: https://researchportal.bath.ac.uk/en/studentthesis/techniques-for-optimisation-and-analysis-of-composite-structures-for-damage-tolerance-and-buckling-stiffness(fce73472-2619-4b82-82b1-5d74312e613d).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.558887.

Council of Science Editors:

Baker N. Techniques for optimisation and analysis of composite structures for damage tolerance and buckling stiffness. [Doctoral Dissertation]. University of Bath; 2012. Available from: https://researchportal.bath.ac.uk/en/studentthesis/techniques-for-optimisation-and-analysis-of-composite-structures-for-damage-tolerance-and-buckling-stiffness(fce73472-2619-4b82-82b1-5d74312e613d).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.558887


Delft University of Technology

2. Lagerweij, Bram (author). Topology Optimization for Damage Tolerance.

Degree: 2019, Delft University of Technology

Complex structural shapes can be produced with additive manufacturing. The geometrical complexity that can be achieved translates into an increase in possible designs. Designing these… (more)

Subjects/Keywords: Fatigue; Optimization Algorithm; Damage Tolerance

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APA (6th Edition):

Lagerweij, B. (. (2019). Topology Optimization for Damage Tolerance. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5a158c8c-a2b2-4eeb-a4df-e8d73924e308

Chicago Manual of Style (16th Edition):

Lagerweij, Bram (author). “Topology Optimization for Damage Tolerance.” 2019. Masters Thesis, Delft University of Technology. Accessed April 17, 2021. http://resolver.tudelft.nl/uuid:5a158c8c-a2b2-4eeb-a4df-e8d73924e308.

MLA Handbook (7th Edition):

Lagerweij, Bram (author). “Topology Optimization for Damage Tolerance.” 2019. Web. 17 Apr 2021.

Vancouver:

Lagerweij B(. Topology Optimization for Damage Tolerance. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://resolver.tudelft.nl/uuid:5a158c8c-a2b2-4eeb-a4df-e8d73924e308.

Council of Science Editors:

Lagerweij B(. Topology Optimization for Damage Tolerance. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:5a158c8c-a2b2-4eeb-a4df-e8d73924e308


Brno University of Technology

3. Rakovský, Kristián. Metodika analýz Damage Tolerance letecké konstrukce s využitím programu AFGROW: Aircraft structure Damage Tolerance analysis method aided by AFGROW software.

Degree: 2019, Brno University of Technology

 Master’s thesis deals with a methodology proposal for the calculation of the dependent growth of cracks in multiple structural components using AFGROW software. The presented… (more)

Subjects/Keywords: Damage tolerance analýza; závislé šíření trhlin; analýza zbytkové pevnosti; Damage tolerance analysis; dependent crack growth; residual strength analysis

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APA (6th Edition):

Rakovský, K. (2019). Metodika analýz Damage Tolerance letecké konstrukce s využitím programu AFGROW: Aircraft structure Damage Tolerance analysis method aided by AFGROW software. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/59590

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):

Rakovský, Kristián. “Metodika analýz Damage Tolerance letecké konstrukce s využitím programu AFGROW: Aircraft structure Damage Tolerance analysis method aided by AFGROW software.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/59590.

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

MLA Handbook (7th Edition):

Rakovský, Kristián. “Metodika analýz Damage Tolerance letecké konstrukce s využitím programu AFGROW: Aircraft structure Damage Tolerance analysis method aided by AFGROW software.” 2019. Web. 17 Apr 2021.

Vancouver:

Rakovský K. Metodika analýz Damage Tolerance letecké konstrukce s využitím programu AFGROW: Aircraft structure Damage Tolerance analysis method aided by AFGROW software. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/59590.

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

Council of Science Editors:

Rakovský K. Metodika analýz Damage Tolerance letecké konstrukce s využitím programu AFGROW: Aircraft structure Damage Tolerance analysis method aided by AFGROW software. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/59590

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

4. Kermi, Chames. Interaction fontionnelle entre le système de tolérance des lésions et le checkpoint des dommages à l'ADN : conséquences sur la stabilité du génome et l'oncogenèse : Functional interaction between the DNA damage tolerance pathway and the DNA damage checkpoint : implications for genome stability and oncogenesis.

Degree: Docteur es, Biologie Santé, 2016, Montpellier

 Notre génome subit constamment les effets néfastes des agents endommageant de l'ADN. Afin de se protéger de ces effets délétères, les cellules disposent d’un système… (more)

Subjects/Keywords: Système de tolérance; Checkpoint; Oncogenèse; DNA damage tolerance pathway; DNA damage checkpoint; Oncogenesis; 577

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APA (6th Edition):

Kermi, C. (2016). Interaction fontionnelle entre le système de tolérance des lésions et le checkpoint des dommages à l'ADN : conséquences sur la stabilité du génome et l'oncogenèse : Functional interaction between the DNA damage tolerance pathway and the DNA damage checkpoint : implications for genome stability and oncogenesis. (Doctoral Dissertation). Montpellier. Retrieved from http://www.theses.fr/2016MONT3520

Chicago Manual of Style (16th Edition):

Kermi, Chames. “Interaction fontionnelle entre le système de tolérance des lésions et le checkpoint des dommages à l'ADN : conséquences sur la stabilité du génome et l'oncogenèse : Functional interaction between the DNA damage tolerance pathway and the DNA damage checkpoint : implications for genome stability and oncogenesis.” 2016. Doctoral Dissertation, Montpellier. Accessed April 17, 2021. http://www.theses.fr/2016MONT3520.

MLA Handbook (7th Edition):

Kermi, Chames. “Interaction fontionnelle entre le système de tolérance des lésions et le checkpoint des dommages à l'ADN : conséquences sur la stabilité du génome et l'oncogenèse : Functional interaction between the DNA damage tolerance pathway and the DNA damage checkpoint : implications for genome stability and oncogenesis.” 2016. Web. 17 Apr 2021.

Vancouver:

Kermi C. Interaction fontionnelle entre le système de tolérance des lésions et le checkpoint des dommages à l'ADN : conséquences sur la stabilité du génome et l'oncogenèse : Functional interaction between the DNA damage tolerance pathway and the DNA damage checkpoint : implications for genome stability and oncogenesis. [Internet] [Doctoral dissertation]. Montpellier; 2016. [cited 2021 Apr 17]. Available from: http://www.theses.fr/2016MONT3520.

Council of Science Editors:

Kermi C. Interaction fontionnelle entre le système de tolérance des lésions et le checkpoint des dommages à l'ADN : conséquences sur la stabilité du génome et l'oncogenèse : Functional interaction between the DNA damage tolerance pathway and the DNA damage checkpoint : implications for genome stability and oncogenesis. [Doctoral Dissertation]. Montpellier; 2016. Available from: http://www.theses.fr/2016MONT3520


University of Utah

5. Heller, Randal Evan. Damage tolerance predictions for spar web cracking in a diminishing stress field.

Degree: MS, Mechanical Engineering, 2011, University of Utah

 Current United States Air Force (USAF) Damage Tolerance Analysis (DTA) methodology yields short crack growth lives for webs in built-up beams as used in the… (more)

Subjects/Keywords: Web cracking; Damage tolerance; Fatigue; Fracture mechanics; Airplanes  – Maintenance and repair

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APA (6th Edition):

Heller, R. E. (2011). Damage tolerance predictions for spar web cracking in a diminishing stress field. (Masters Thesis). University of Utah. Retrieved from http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/482/rec/602

Chicago Manual of Style (16th Edition):

Heller, Randal Evan. “Damage tolerance predictions for spar web cracking in a diminishing stress field.” 2011. Masters Thesis, University of Utah. Accessed April 17, 2021. http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/482/rec/602.

MLA Handbook (7th Edition):

Heller, Randal Evan. “Damage tolerance predictions for spar web cracking in a diminishing stress field.” 2011. Web. 17 Apr 2021.

Vancouver:

Heller RE. Damage tolerance predictions for spar web cracking in a diminishing stress field. [Internet] [Masters thesis]. University of Utah; 2011. [cited 2021 Apr 17]. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/482/rec/602.

Council of Science Editors:

Heller RE. Damage tolerance predictions for spar web cracking in a diminishing stress field. [Masters Thesis]. University of Utah; 2011. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd3/id/482/rec/602

6. Tom, Louis-Georges. Contribution à l'étude numérique de la propagation d'un défaut de collage dans une structure sandwich Nida : Contribution to the numerical analysis of disbond growth in honeycomb core sandwich structure.

Degree: Docteur es, Génie mécanique et productique, 2014, Le Mans

SAFRAN Aircelle produit des panneaux sandwiches constitués de peaux composites collées sur une âme nid d’abeille (« Nida ») en aluminium pour des applications de… (more)

Subjects/Keywords: Sandwich; Composite; Décollement; Non-propagation; Nida; Disbond; Damage tolerance; Honeycomb; 620.112

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APA (6th Edition):

Tom, L. (2014). Contribution à l'étude numérique de la propagation d'un défaut de collage dans une structure sandwich Nida : Contribution to the numerical analysis of disbond growth in honeycomb core sandwich structure. (Doctoral Dissertation). Le Mans. Retrieved from http://www.theses.fr/2014LEMA1036

Chicago Manual of Style (16th Edition):

Tom, Louis-Georges. “Contribution à l'étude numérique de la propagation d'un défaut de collage dans une structure sandwich Nida : Contribution to the numerical analysis of disbond growth in honeycomb core sandwich structure.” 2014. Doctoral Dissertation, Le Mans. Accessed April 17, 2021. http://www.theses.fr/2014LEMA1036.

MLA Handbook (7th Edition):

Tom, Louis-Georges. “Contribution à l'étude numérique de la propagation d'un défaut de collage dans une structure sandwich Nida : Contribution to the numerical analysis of disbond growth in honeycomb core sandwich structure.” 2014. Web. 17 Apr 2021.

Vancouver:

Tom L. Contribution à l'étude numérique de la propagation d'un défaut de collage dans une structure sandwich Nida : Contribution to the numerical analysis of disbond growth in honeycomb core sandwich structure. [Internet] [Doctoral dissertation]. Le Mans; 2014. [cited 2021 Apr 17]. Available from: http://www.theses.fr/2014LEMA1036.

Council of Science Editors:

Tom L. Contribution à l'étude numérique de la propagation d'un défaut de collage dans une structure sandwich Nida : Contribution to the numerical analysis of disbond growth in honeycomb core sandwich structure. [Doctoral Dissertation]. Le Mans; 2014. Available from: http://www.theses.fr/2014LEMA1036


University of Manchester

7. Wu, Zijie. Damage Tolerance Study of Carbon Fibre/RTM6 Composites Toughened with Thermoplastic-coated Fabric Reinforcement.

Degree: 2016, University of Manchester

 RTM6 has for more than 20 years been the main commercial epoxy system for infusion processing qualified by the aerospace industry. In common with other… (more)

Subjects/Keywords: Composites; Damage Tolerance; Carbon Fibre; Toughened; RTM6; Epoxy; PAEK; Aerospace

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APA (6th Edition):

Wu, Z. (2016). Damage Tolerance Study of Carbon Fibre/RTM6 Composites Toughened with Thermoplastic-coated Fabric Reinforcement. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:300959

Chicago Manual of Style (16th Edition):

Wu, Zijie. “Damage Tolerance Study of Carbon Fibre/RTM6 Composites Toughened with Thermoplastic-coated Fabric Reinforcement.” 2016. Doctoral Dissertation, University of Manchester. Accessed April 17, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:300959.

MLA Handbook (7th Edition):

Wu, Zijie. “Damage Tolerance Study of Carbon Fibre/RTM6 Composites Toughened with Thermoplastic-coated Fabric Reinforcement.” 2016. Web. 17 Apr 2021.

Vancouver:

Wu Z. Damage Tolerance Study of Carbon Fibre/RTM6 Composites Toughened with Thermoplastic-coated Fabric Reinforcement. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Apr 17]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:300959.

Council of Science Editors:

Wu Z. Damage Tolerance Study of Carbon Fibre/RTM6 Composites Toughened with Thermoplastic-coated Fabric Reinforcement. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:300959


Cranfield University

8. Liddel, Paul Daniel. Transforming composite design by use of structural health monitoring.

Degree: PhD, 2016, Cranfield University

 Commercial composite aerospace structure is required to be designed and managed under the damage tolerant principle. Airworthiness is maintained through a process of regulated inspections… (more)

Subjects/Keywords: Bonded Joint; Damage tolerance; DIC; FEA; SHM enabled design; Strain

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APA (6th Edition):

Liddel, P. D. (2016). Transforming composite design by use of structural health monitoring. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/12380

Chicago Manual of Style (16th Edition):

Liddel, Paul Daniel. “Transforming composite design by use of structural health monitoring.” 2016. Doctoral Dissertation, Cranfield University. Accessed April 17, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/12380.

MLA Handbook (7th Edition):

Liddel, Paul Daniel. “Transforming composite design by use of structural health monitoring.” 2016. Web. 17 Apr 2021.

Vancouver:

Liddel PD. Transforming composite design by use of structural health monitoring. [Internet] [Doctoral dissertation]. Cranfield University; 2016. [cited 2021 Apr 17]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12380.

Council of Science Editors:

Liddel PD. Transforming composite design by use of structural health monitoring. [Doctoral Dissertation]. Cranfield University; 2016. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12380


Cranfield University

9. Liddel, Paul Daniel. Transforming composite design by use of structural health monitoring.

Degree: PhD, 2016, Cranfield University

 Commercial composite aerospace structure is required to be designed and managed under the damage tolerant principle. Airworthiness is maintained through a process of regulated inspections… (more)

Subjects/Keywords: 629.1; Bonded Joint; Damage tolerance; DIC; FEA; SHM enabled design; Strain

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Liddel, P. D. (2016). Transforming composite design by use of structural health monitoring. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/12380 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.723673

Chicago Manual of Style (16th Edition):

Liddel, Paul Daniel. “Transforming composite design by use of structural health monitoring.” 2016. Doctoral Dissertation, Cranfield University. Accessed April 17, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/12380 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.723673.

MLA Handbook (7th Edition):

Liddel, Paul Daniel. “Transforming composite design by use of structural health monitoring.” 2016. Web. 17 Apr 2021.

Vancouver:

Liddel PD. Transforming composite design by use of structural health monitoring. [Internet] [Doctoral dissertation]. Cranfield University; 2016. [cited 2021 Apr 17]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12380 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.723673.

Council of Science Editors:

Liddel PD. Transforming composite design by use of structural health monitoring. [Doctoral Dissertation]. Cranfield University; 2016. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12380 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.723673


University of Manchester

10. Wu, Zijie. Damage tolerance study of carbon fibre/RTM6 composites toughened with thermoplastic-coated fabric reinforcement.

Degree: PhD, 2016, University of Manchester

 RTM6 has for more than 20 years been the main commercial epoxy system for infusion processing qualified by the aerospace industry. In common with other… (more)

Subjects/Keywords: 620.1; Composites; Damage Tolerance; Carbon Fibre; Toughened; RTM6; Epoxy; PAEK; Aerospace

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Wu, Z. (2016). Damage tolerance study of carbon fibre/RTM6 composites toughened with thermoplastic-coated fabric reinforcement. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/damage-tolerance-study-of-carbon-fibrertm6-composites-toughened-with-thermoplasticcoated-fabric-reinforcement(0a596f56-3143-4bf0-993f-34ee773518c9).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694276

Chicago Manual of Style (16th Edition):

Wu, Zijie. “Damage tolerance study of carbon fibre/RTM6 composites toughened with thermoplastic-coated fabric reinforcement.” 2016. Doctoral Dissertation, University of Manchester. Accessed April 17, 2021. https://www.research.manchester.ac.uk/portal/en/theses/damage-tolerance-study-of-carbon-fibrertm6-composites-toughened-with-thermoplasticcoated-fabric-reinforcement(0a596f56-3143-4bf0-993f-34ee773518c9).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694276.

MLA Handbook (7th Edition):

Wu, Zijie. “Damage tolerance study of carbon fibre/RTM6 composites toughened with thermoplastic-coated fabric reinforcement.” 2016. Web. 17 Apr 2021.

Vancouver:

Wu Z. Damage tolerance study of carbon fibre/RTM6 composites toughened with thermoplastic-coated fabric reinforcement. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Apr 17]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/damage-tolerance-study-of-carbon-fibrertm6-composites-toughened-with-thermoplasticcoated-fabric-reinforcement(0a596f56-3143-4bf0-993f-34ee773518c9).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694276.

Council of Science Editors:

Wu Z. Damage tolerance study of carbon fibre/RTM6 composites toughened with thermoplastic-coated fabric reinforcement. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/damage-tolerance-study-of-carbon-fibrertm6-composites-toughened-with-thermoplasticcoated-fabric-reinforcement(0a596f56-3143-4bf0-993f-34ee773518c9).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694276


University of Bath

11. Kinawy, Moustafa. Static and fatigue propagation of buckle-driven delaminations under bending and compressive loads.

Degree: PhD, 2011, University of Bath

Subjects/Keywords: 620.110287; delamination; damage tolerance; fatigue

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APA (6th Edition):

Kinawy, M. (2011). Static and fatigue propagation of buckle-driven delaminations under bending and compressive loads. (Doctoral Dissertation). University of Bath. Retrieved from https://researchportal.bath.ac.uk/en/studentthesis/static-and-fatigue-propagation-of-buckledriven-delaminations-under-bending-and-compressive-loads(527392b9-c845-4a2a-a4dd-4f4b64cc690b).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.545324

Chicago Manual of Style (16th Edition):

Kinawy, Moustafa. “Static and fatigue propagation of buckle-driven delaminations under bending and compressive loads.” 2011. Doctoral Dissertation, University of Bath. Accessed April 17, 2021. https://researchportal.bath.ac.uk/en/studentthesis/static-and-fatigue-propagation-of-buckledriven-delaminations-under-bending-and-compressive-loads(527392b9-c845-4a2a-a4dd-4f4b64cc690b).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.545324.

MLA Handbook (7th Edition):

Kinawy, Moustafa. “Static and fatigue propagation of buckle-driven delaminations under bending and compressive loads.” 2011. Web. 17 Apr 2021.

Vancouver:

Kinawy M. Static and fatigue propagation of buckle-driven delaminations under bending and compressive loads. [Internet] [Doctoral dissertation]. University of Bath; 2011. [cited 2021 Apr 17]. Available from: https://researchportal.bath.ac.uk/en/studentthesis/static-and-fatigue-propagation-of-buckledriven-delaminations-under-bending-and-compressive-loads(527392b9-c845-4a2a-a4dd-4f4b64cc690b).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.545324.

Council of Science Editors:

Kinawy M. Static and fatigue propagation of buckle-driven delaminations under bending and compressive loads. [Doctoral Dissertation]. University of Bath; 2011. Available from: https://researchportal.bath.ac.uk/en/studentthesis/static-and-fatigue-propagation-of-buckledriven-delaminations-under-bending-and-compressive-loads(527392b9-c845-4a2a-a4dd-4f4b64cc690b).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.545324

12. Chattunyakit, Sarun. Self-recovery Strategy for Multi-legged Robot with Damaged Legs.

Degree: 博士(工学), 工学, 2019, Hokkaido University

 Due to the exibility of multi-legged robots, they can be applied in several applications in which regular wheel-based robots are not suitable to perform. However,… (more)

Subjects/Keywords: Legged Robot; Damage Detection; Reinforcement Learning; Gait Adaptation; Fault Tolerance

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APA (6th Edition):

Chattunyakit, S. (2019). Self-recovery Strategy for Multi-legged Robot with Damaged Legs. (Doctoral Dissertation). Hokkaido University. Retrieved from http://hdl.handle.net/2115/74971

Chicago Manual of Style (16th Edition):

Chattunyakit, Sarun. “Self-recovery Strategy for Multi-legged Robot with Damaged Legs.” 2019. Doctoral Dissertation, Hokkaido University. Accessed April 17, 2021. http://hdl.handle.net/2115/74971.

MLA Handbook (7th Edition):

Chattunyakit, Sarun. “Self-recovery Strategy for Multi-legged Robot with Damaged Legs.” 2019. Web. 17 Apr 2021.

Vancouver:

Chattunyakit S. Self-recovery Strategy for Multi-legged Robot with Damaged Legs. [Internet] [Doctoral dissertation]. Hokkaido University; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/2115/74971.

Council of Science Editors:

Chattunyakit S. Self-recovery Strategy for Multi-legged Robot with Damaged Legs. [Doctoral Dissertation]. Hokkaido University; 2019. Available from: http://hdl.handle.net/2115/74971


Delft University of Technology

13. de Boer, T. (author). Fracture Toughness of Aerospace Structures: On the Use of Redundant Lattice Structures.

Degree: 2017, Delft University of Technology

Both experimental and numerical studies have shown that the crack-bridging is one of the most significant mechanism contributing to the fracture toughness of natural materials… (more)

Subjects/Keywords: Additive Manufacturing; Fracture Toughness; Damage Tolerance; 3D Printing; Lattice Structures

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

de Boer, T. (. (2017). Fracture Toughness of Aerospace Structures: On the Use of Redundant Lattice Structures. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:27e9dcc3-8422-485e-9926-1868f8900749

Chicago Manual of Style (16th Edition):

de Boer, T (author). “Fracture Toughness of Aerospace Structures: On the Use of Redundant Lattice Structures.” 2017. Masters Thesis, Delft University of Technology. Accessed April 17, 2021. http://resolver.tudelft.nl/uuid:27e9dcc3-8422-485e-9926-1868f8900749.

MLA Handbook (7th Edition):

de Boer, T (author). “Fracture Toughness of Aerospace Structures: On the Use of Redundant Lattice Structures.” 2017. Web. 17 Apr 2021.

Vancouver:

de Boer T(. Fracture Toughness of Aerospace Structures: On the Use of Redundant Lattice Structures. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Apr 17]. Available from: http://resolver.tudelft.nl/uuid:27e9dcc3-8422-485e-9926-1868f8900749.

Council of Science Editors:

de Boer T(. Fracture Toughness of Aerospace Structures: On the Use of Redundant Lattice Structures. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:27e9dcc3-8422-485e-9926-1868f8900749


Delft University of Technology

14. Michielssen, J. (author). Fatigue crack growth in Selective Laser Melted Ti-6Al-4V.

Degree: 2017, Delft University of Technology

This research investigates the effect of a varying build orientation and different heat treatment on the crack propagation properties of SLM Ti-6Al-4V. Both crack propagation… (more)

Subjects/Keywords: Fatigue; Damage Tolerance; Ti-6Al-4V; SLM; Additive Manufacturing

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Michielssen, J. (. (2017). Fatigue crack growth in Selective Laser Melted Ti-6Al-4V. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c62fc3a4-6aea-4180-b125-ac54fede0762

Chicago Manual of Style (16th Edition):

Michielssen, J (author). “Fatigue crack growth in Selective Laser Melted Ti-6Al-4V.” 2017. Masters Thesis, Delft University of Technology. Accessed April 17, 2021. http://resolver.tudelft.nl/uuid:c62fc3a4-6aea-4180-b125-ac54fede0762.

MLA Handbook (7th Edition):

Michielssen, J (author). “Fatigue crack growth in Selective Laser Melted Ti-6Al-4V.” 2017. Web. 17 Apr 2021.

Vancouver:

Michielssen J(. Fatigue crack growth in Selective Laser Melted Ti-6Al-4V. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Apr 17]. Available from: http://resolver.tudelft.nl/uuid:c62fc3a4-6aea-4180-b125-ac54fede0762.

Council of Science Editors:

Michielssen J(. Fatigue crack growth in Selective Laser Melted Ti-6Al-4V. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:c62fc3a4-6aea-4180-b125-ac54fede0762


Delft University of Technology

15. Nagelsmit, M.H. Fibre Placement Architectures for Improved Damage Tolerance.

Degree: 2013, Delft University of Technology

 Composites are notorious for their poor impact behaviour. Delaminations seriously decrease the compressive strength of the material after impact. Laminates made from woven fabric show… (more)

Subjects/Keywords: composites; fibre placement; damage tolerance

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Nagelsmit, M. H. (2013). Fibre Placement Architectures for Improved Damage Tolerance. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673

Chicago Manual of Style (16th Edition):

Nagelsmit, M H. “Fibre Placement Architectures for Improved Damage Tolerance.” 2013. Doctoral Dissertation, Delft University of Technology. Accessed April 17, 2021. http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673.

MLA Handbook (7th Edition):

Nagelsmit, M H. “Fibre Placement Architectures for Improved Damage Tolerance.” 2013. Web. 17 Apr 2021.

Vancouver:

Nagelsmit MH. Fibre Placement Architectures for Improved Damage Tolerance. [Internet] [Doctoral dissertation]. Delft University of Technology; 2013. [cited 2021 Apr 17]. Available from: http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673.

Council of Science Editors:

Nagelsmit MH. Fibre Placement Architectures for Improved Damage Tolerance. [Doctoral Dissertation]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; urn:NBN:nl:ui:24-uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673 ; http://resolver.tudelft.nl/uuid:f8c8ad4e-5d52-4bfd-8449-2748bad26673

16. Ecault, Romain. Etude expérimentale et numérique du comportement dynamique de composites aéronautiques sous choc laser. Optimisation du test d'adhérence par ondes de choc sur les assemblages composites collés : Experimental and numerical investigations on the dynamic behaviour of aeronautic composites under laser shock - Optimization of a shock wave adhesion test for bonded composites.

Degree: Docteur es, Mécanique des solides, des matériaux, des structures et des surfaces, 2013, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique

Ce travail vise le développement d’une méthode non destructive permettant de contrôler la qualitémécanique des joints collés aéronautiques, en utilisant les ondes de choc générées… (more)

Subjects/Keywords: LASAT; Tolérance aux dommages; Laser adhesion test; Damage tolerance

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Ecault, R. (2013). Etude expérimentale et numérique du comportement dynamique de composites aéronautiques sous choc laser. Optimisation du test d'adhérence par ondes de choc sur les assemblages composites collés : Experimental and numerical investigations on the dynamic behaviour of aeronautic composites under laser shock - Optimization of a shock wave adhesion test for bonded composites. (Doctoral Dissertation). Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Retrieved from http://www.theses.fr/2013ESMA0031

Chicago Manual of Style (16th Edition):

Ecault, Romain. “Etude expérimentale et numérique du comportement dynamique de composites aéronautiques sous choc laser. Optimisation du test d'adhérence par ondes de choc sur les assemblages composites collés : Experimental and numerical investigations on the dynamic behaviour of aeronautic composites under laser shock - Optimization of a shock wave adhesion test for bonded composites.” 2013. Doctoral Dissertation, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique. Accessed April 17, 2021. http://www.theses.fr/2013ESMA0031.

MLA Handbook (7th Edition):

Ecault, Romain. “Etude expérimentale et numérique du comportement dynamique de composites aéronautiques sous choc laser. Optimisation du test d'adhérence par ondes de choc sur les assemblages composites collés : Experimental and numerical investigations on the dynamic behaviour of aeronautic composites under laser shock - Optimization of a shock wave adhesion test for bonded composites.” 2013. Web. 17 Apr 2021.

Vancouver:

Ecault R. Etude expérimentale et numérique du comportement dynamique de composites aéronautiques sous choc laser. Optimisation du test d'adhérence par ondes de choc sur les assemblages composites collés : Experimental and numerical investigations on the dynamic behaviour of aeronautic composites under laser shock - Optimization of a shock wave adhesion test for bonded composites. [Internet] [Doctoral dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2013. [cited 2021 Apr 17]. Available from: http://www.theses.fr/2013ESMA0031.

Council of Science Editors:

Ecault R. Etude expérimentale et numérique du comportement dynamique de composites aéronautiques sous choc laser. Optimisation du test d'adhérence par ondes de choc sur les assemblages composites collés : Experimental and numerical investigations on the dynamic behaviour of aeronautic composites under laser shock - Optimization of a shock wave adhesion test for bonded composites. [Doctoral Dissertation]. Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique; 2013. Available from: http://www.theses.fr/2013ESMA0031


Penn State University

17. Bossenbroek, Kirsten. Damage Tolerance of Layer-Wise Hybrid Laminates Consisting of Glass Reinforced Flexible and Rigid Epoxy Resins .

Degree: 2008, Penn State University

 The objective of this investigation is to develop and characterize co-curing rigid and flexible epoxies, develop and implement a fabrication process for filament winding layer-wise… (more)

Subjects/Keywords: layer-wise hybrid; damage resistance; damage tolerance; composite

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APA (6th Edition):

Bossenbroek, K. (2008). Damage Tolerance of Layer-Wise Hybrid Laminates Consisting of Glass Reinforced Flexible and Rigid Epoxy Resins . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/8750

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):

Bossenbroek, Kirsten. “Damage Tolerance of Layer-Wise Hybrid Laminates Consisting of Glass Reinforced Flexible and Rigid Epoxy Resins .” 2008. Thesis, Penn State University. Accessed April 17, 2021. https://submit-etda.libraries.psu.edu/catalog/8750.

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

MLA Handbook (7th Edition):

Bossenbroek, Kirsten. “Damage Tolerance of Layer-Wise Hybrid Laminates Consisting of Glass Reinforced Flexible and Rigid Epoxy Resins .” 2008. Web. 17 Apr 2021.

Vancouver:

Bossenbroek K. Damage Tolerance of Layer-Wise Hybrid Laminates Consisting of Glass Reinforced Flexible and Rigid Epoxy Resins . [Internet] [Thesis]. Penn State University; 2008. [cited 2021 Apr 17]. Available from: https://submit-etda.libraries.psu.edu/catalog/8750.

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

Council of Science Editors:

Bossenbroek K. Damage Tolerance of Layer-Wise Hybrid Laminates Consisting of Glass Reinforced Flexible and Rigid Epoxy Resins . [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/8750

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


Brno University of Technology

18. Pokorný, Pavel. Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES.

Degree: 2019, Brno University of Technology

 This Ph.D. thesis deals with methodology for determination of residual fatigue lifetime of railway axles based on damage tolerance approach. This approach accepts an existence… (more)

Subjects/Keywords: vlaková náprava; šíření únavové trhliny; damage tolerance koncept; zbytková únavová životnost; railway axle; fatigue crack propagation; damage tolerance concept; residual fatigue lifetime

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Pokorný, P. (2019). Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/63097

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):

Pokorný, Pavel. “Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/63097.

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

MLA Handbook (7th Edition):

Pokorný, Pavel. “Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES.” 2019. Web. 17 Apr 2021.

Vancouver:

Pokorný P. Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/63097.

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

Council of Science Editors:

Pokorný P. Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/63097

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


Brno University of Technology

19. Vaněk, David. Analýzy damage tolerance s uvážením interakce zatěžovacích kmitů: Damage tolerance analysis using load interaction models.

Degree: 2019, Brno University of Technology

 Master’s thesis deals with study of fatigue crack growth retardation models. This document presents description, evaluation, verification and finally application of retardation models demonstrated on… (more)

Subjects/Keywords: Damage tolerance analýza; retardační modely; analýza šíření únavové trhliny; program prohlídek; pásnice; Damage tolerance analysis; retardation models; fatigue crack growth analysis; inspection program; flange

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APA (6th Edition):

Vaněk, D. (2019). Analýzy damage tolerance s uvážením interakce zatěžovacích kmitů: Damage tolerance analysis using load interaction models. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/60745

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):

Vaněk, David. “Analýzy damage tolerance s uvážením interakce zatěžovacích kmitů: Damage tolerance analysis using load interaction models.” 2019. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/60745.

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

MLA Handbook (7th Edition):

Vaněk, David. “Analýzy damage tolerance s uvážením interakce zatěžovacích kmitů: Damage tolerance analysis using load interaction models.” 2019. Web. 17 Apr 2021.

Vancouver:

Vaněk D. Analýzy damage tolerance s uvážením interakce zatěžovacích kmitů: Damage tolerance analysis using load interaction models. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/60745.

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

Council of Science Editors:

Vaněk D. Analýzy damage tolerance s uvážením interakce zatěžovacích kmitů: Damage tolerance analysis using load interaction models. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/60745

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


Brno University of Technology

20. Pokorný, Pavel. Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES.

Degree: 2018, Brno University of Technology

 This Ph.D. thesis deals with methodology for determination of residual fatigue lifetime of railway axles based on damage tolerance approach. This approach accepts an existence… (more)

Subjects/Keywords: vlaková náprava; šíření únavové trhliny; damage tolerance koncept; zbytková únavová životnost; railway axle; fatigue crack propagation; damage tolerance concept; residual fatigue lifetime

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APA (6th Edition):

Pokorný, P. (2018). Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/63149

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):

Pokorný, Pavel. “Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES.” 2018. Thesis, Brno University of Technology. Accessed April 17, 2021. http://hdl.handle.net/11012/63149.

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

MLA Handbook (7th Edition):

Pokorný, Pavel. “Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES.” 2018. Web. 17 Apr 2021.

Vancouver:

Pokorný P. Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/11012/63149.

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

Council of Science Editors:

Pokorný P. Zbytková únavová životnost železničních náprav: RESIDUAL FATIGUE LIFETIME OF RAILWAY AXLES. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/63149

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


RMIT University

21. Burns, L. Bio-inspired design of aerospace composite joints.

Degree: 2012, RMIT University

 This PhD thesis utilises deep principles in nature governing the architecture of structural joints formed from biological materials, focusing on tree branch joints, in order… (more)

Subjects/Keywords: Fields of Research; Biomimetics; Bio-inspired; Composites; T-Joint; Damage tolerance; Optimization

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APA (6th Edition):

Burns, L. (2012). Bio-inspired design of aerospace composite joints. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161779

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):

Burns, L. “Bio-inspired design of aerospace composite joints.” 2012. Thesis, RMIT University. Accessed April 17, 2021. http://researchbank.rmit.edu.au/view/rmit:161779.

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

MLA Handbook (7th Edition):

Burns, L. “Bio-inspired design of aerospace composite joints.” 2012. Web. 17 Apr 2021.

Vancouver:

Burns L. Bio-inspired design of aerospace composite joints. [Internet] [Thesis]. RMIT University; 2012. [cited 2021 Apr 17]. Available from: http://researchbank.rmit.edu.au/view/rmit:161779.

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

Council of Science Editors:

Burns L. Bio-inspired design of aerospace composite joints. [Thesis]. RMIT University; 2012. Available from: http://researchbank.rmit.edu.au/view/rmit:161779

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


Temple University

22. Halbert, Keith. Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures.

Degree: PhD, 2014, Temple University

Statistics

The majority of aircraft structures are designed to be damage-tolerant such that safe operation can continue in the presence of minor damage. It is… (more)

Subjects/Keywords: Statistics; Aerospace engineering;

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APA (6th Edition):

Halbert, K. (2014). Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures. (Doctoral Dissertation). Temple University. Retrieved from http://digital.library.temple.edu/u?/p245801coll10,262194

Chicago Manual of Style (16th Edition):

Halbert, Keith. “Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures.” 2014. Doctoral Dissertation, Temple University. Accessed April 17, 2021. http://digital.library.temple.edu/u?/p245801coll10,262194.

MLA Handbook (7th Edition):

Halbert, Keith. “Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures.” 2014. Web. 17 Apr 2021.

Vancouver:

Halbert K. Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures. [Internet] [Doctoral dissertation]. Temple University; 2014. [cited 2021 Apr 17]. Available from: http://digital.library.temple.edu/u?/p245801coll10,262194.

Council of Science Editors:

Halbert K. Estimation of Probability of Failure for Damage-Tolerant Aerospace Structures. [Doctoral Dissertation]. Temple University; 2014. Available from: http://digital.library.temple.edu/u?/p245801coll10,262194


University of Manchester

23. Gong, Keyi. The effect of stacking sequence on impact resistance and damage tolerance in non-crimp carbon fabric composites.

Degree: 2015, University of Manchester

This project aims to better understand the influence of stacking sequence on the non-crimp carbon fabric composite laminates under low velocity impact and post impact… (more)

Subjects/Keywords: Non-crimp; carbon fibre; impact resistance; damage tolerance; C-scan; ply clustering

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APA (6th Edition):

Gong, K. (2015). The effect of stacking sequence on impact resistance and damage tolerance in non-crimp carbon fabric composites. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:268525

Chicago Manual of Style (16th Edition):

Gong, Keyi. “The effect of stacking sequence on impact resistance and damage tolerance in non-crimp carbon fabric composites.” 2015. Doctoral Dissertation, University of Manchester. Accessed April 17, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:268525.

MLA Handbook (7th Edition):

Gong, Keyi. “The effect of stacking sequence on impact resistance and damage tolerance in non-crimp carbon fabric composites.” 2015. Web. 17 Apr 2021.

Vancouver:

Gong K. The effect of stacking sequence on impact resistance and damage tolerance in non-crimp carbon fabric composites. [Internet] [Doctoral dissertation]. University of Manchester; 2015. [cited 2021 Apr 17]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:268525.

Council of Science Editors:

Gong K. The effect of stacking sequence on impact resistance and damage tolerance in non-crimp carbon fabric composites. [Doctoral Dissertation]. University of Manchester; 2015. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:268525


University of California – Irvine

24. Li, Xiaopeng. Multifunctional Cementitious Materials with Damage Tolerance and Self-Sensing Capacity for the Protection of Critical Infrastructure.

Degree: Civil Engineering, 2018, University of California – Irvine

 Early detection of damage in concrete infrastructure is critical to prolonging structural service life through timely maintenance, ensuring safety and preventing failure. Current management practices… (more)

Subjects/Keywords: Civil engineering; damage tolerance; electrical impedance tomography; multifunctional cementitious materials; self-sensing; strain-hardening

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APA (6th Edition):

Li, X. (2018). Multifunctional Cementitious Materials with Damage Tolerance and Self-Sensing Capacity for the Protection of Critical Infrastructure. (Thesis). University of California – Irvine. Retrieved from http://www.escholarship.org/uc/item/0dd2v2dn

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):

Li, Xiaopeng. “Multifunctional Cementitious Materials with Damage Tolerance and Self-Sensing Capacity for the Protection of Critical Infrastructure.” 2018. Thesis, University of California – Irvine. Accessed April 17, 2021. http://www.escholarship.org/uc/item/0dd2v2dn.

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

MLA Handbook (7th Edition):

Li, Xiaopeng. “Multifunctional Cementitious Materials with Damage Tolerance and Self-Sensing Capacity for the Protection of Critical Infrastructure.” 2018. Web. 17 Apr 2021.

Vancouver:

Li X. Multifunctional Cementitious Materials with Damage Tolerance and Self-Sensing Capacity for the Protection of Critical Infrastructure. [Internet] [Thesis]. University of California – Irvine; 2018. [cited 2021 Apr 17]. Available from: http://www.escholarship.org/uc/item/0dd2v2dn.

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

Council of Science Editors:

Li X. Multifunctional Cementitious Materials with Damage Tolerance and Self-Sensing Capacity for the Protection of Critical Infrastructure. [Thesis]. University of California – Irvine; 2018. Available from: http://www.escholarship.org/uc/item/0dd2v2dn

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


Colorado State University

25. Thurston, Alison K. Chromatin binding factor Spn1 contributes to genome instability in Saccharomyces cerevisiae, The.

Degree: PhD, Biochemistry and Molecular Biology, 2018, Colorado State University

 Maintaining the genetic information is the most important role of a cell. Alteration to the DNA sequence is generally thought of as harmful, as it… (more)

Subjects/Keywords: DNA damage tolerance; methyl methanesulfonate; yeast; genome instability; chromatin binding factor; Spn1

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APA (6th Edition):

Thurston, A. K. (2018). Chromatin binding factor Spn1 contributes to genome instability in Saccharomyces cerevisiae, The. (Doctoral Dissertation). Colorado State University. Retrieved from http://hdl.handle.net/10217/189371

Chicago Manual of Style (16th Edition):

Thurston, Alison K. “Chromatin binding factor Spn1 contributes to genome instability in Saccharomyces cerevisiae, The.” 2018. Doctoral Dissertation, Colorado State University. Accessed April 17, 2021. http://hdl.handle.net/10217/189371.

MLA Handbook (7th Edition):

Thurston, Alison K. “Chromatin binding factor Spn1 contributes to genome instability in Saccharomyces cerevisiae, The.” 2018. Web. 17 Apr 2021.

Vancouver:

Thurston AK. Chromatin binding factor Spn1 contributes to genome instability in Saccharomyces cerevisiae, The. [Internet] [Doctoral dissertation]. Colorado State University; 2018. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/10217/189371.

Council of Science Editors:

Thurston AK. Chromatin binding factor Spn1 contributes to genome instability in Saccharomyces cerevisiae, The. [Doctoral Dissertation]. Colorado State University; 2018. Available from: http://hdl.handle.net/10217/189371


University of Washington

26. Richard, Luke Ian. Delamination Arrest by Fasteners in Aircraft Structure Under Static and Fatigue Loading.

Degree: PhD, 2017, University of Washington

 Laminated composite structures convey tremendous benefits of specific strength and fatigue properties in plane, but are highly susceptible to interlaminar failures such as delaminations and… (more)

Subjects/Keywords: Composite Delamination; Damage Tolerance; Delamination arrest; Finite Element Analysis; Aerospace engineering; Aeronautics and astronautics

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APA (6th Edition):

Richard, L. I. (2017). Delamination Arrest by Fasteners in Aircraft Structure Under Static and Fatigue Loading. (Doctoral Dissertation). University of Washington. Retrieved from http://hdl.handle.net/1773/39923

Chicago Manual of Style (16th Edition):

Richard, Luke Ian. “Delamination Arrest by Fasteners in Aircraft Structure Under Static and Fatigue Loading.” 2017. Doctoral Dissertation, University of Washington. Accessed April 17, 2021. http://hdl.handle.net/1773/39923.

MLA Handbook (7th Edition):

Richard, Luke Ian. “Delamination Arrest by Fasteners in Aircraft Structure Under Static and Fatigue Loading.” 2017. Web. 17 Apr 2021.

Vancouver:

Richard LI. Delamination Arrest by Fasteners in Aircraft Structure Under Static and Fatigue Loading. [Internet] [Doctoral dissertation]. University of Washington; 2017. [cited 2021 Apr 17]. Available from: http://hdl.handle.net/1773/39923.

Council of Science Editors:

Richard LI. Delamination Arrest by Fasteners in Aircraft Structure Under Static and Fatigue Loading. [Doctoral Dissertation]. University of Washington; 2017. Available from: http://hdl.handle.net/1773/39923


Delft University of Technology

27. Bürger, D.B. Mixed-Mode Fatigue Disbond on Metallic Bonded Joints.

Degree: 2015, Delft University of Technology

 Aerospace structures have been long dealing with the safety versus weight issue. Lighter airplanes are cheaper to operate, however, they may face a safety issue… (more)

Subjects/Keywords: disbond; damage tolerance; fatigue; Mixed-Mode

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APA (6th Edition):

Bürger, D. B. (2015). Mixed-Mode Fatigue Disbond on Metallic Bonded Joints. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174

Chicago Manual of Style (16th Edition):

Bürger, D B. “Mixed-Mode Fatigue Disbond on Metallic Bonded Joints.” 2015. Doctoral Dissertation, Delft University of Technology. Accessed April 17, 2021. http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174.

MLA Handbook (7th Edition):

Bürger, D B. “Mixed-Mode Fatigue Disbond on Metallic Bonded Joints.” 2015. Web. 17 Apr 2021.

Vancouver:

Bürger DB. Mixed-Mode Fatigue Disbond on Metallic Bonded Joints. [Internet] [Doctoral dissertation]. Delft University of Technology; 2015. [cited 2021 Apr 17]. Available from: http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174.

Council of Science Editors:

Bürger DB. Mixed-Mode Fatigue Disbond on Metallic Bonded Joints. [Doctoral Dissertation]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; urn:NBN:nl:ui:24-uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174 ; http://resolver.tudelft.nl/uuid:ec4dbcd6-052d-4009-bf9e-cdcbf4614174


Virginia Tech

28. 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 April 17, 2021. 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. 17 Apr 2021.

Vancouver:

Mcquigg TD. Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2021 Apr 17]. 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


Delft University of Technology

29. Hofwegen, Mark (author). Damage Tolerant Design for Additive Manufacturing: An experimental study on the fatigue behaviour of stretch dominated AlSi10Mg multiple load path specimens.

Degree: 2021, Delft University of Technology

To expand the use of additive manufacturing in aerospace towards more critical applications, it is required to design parts in a damage tolerant context. Therefore,… (more)

Subjects/Keywords: Additive Manufacturing; Damage Tolerance; Fatigue; Design for Additive Manufacturing; SLM; L-PBF; Gradual failure

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APA (6th Edition):

Hofwegen, M. (. (2021). Damage Tolerant Design for Additive Manufacturing: An experimental study on the fatigue behaviour of stretch dominated AlSi10Mg multiple load path specimens. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:52f34a92-8937-4b51-b2e5-8cacfcd24d27

Chicago Manual of Style (16th Edition):

Hofwegen, Mark (author). “Damage Tolerant Design for Additive Manufacturing: An experimental study on the fatigue behaviour of stretch dominated AlSi10Mg multiple load path specimens.” 2021. Masters Thesis, Delft University of Technology. Accessed April 17, 2021. http://resolver.tudelft.nl/uuid:52f34a92-8937-4b51-b2e5-8cacfcd24d27.

MLA Handbook (7th Edition):

Hofwegen, Mark (author). “Damage Tolerant Design for Additive Manufacturing: An experimental study on the fatigue behaviour of stretch dominated AlSi10Mg multiple load path specimens.” 2021. Web. 17 Apr 2021.

Vancouver:

Hofwegen M(. Damage Tolerant Design for Additive Manufacturing: An experimental study on the fatigue behaviour of stretch dominated AlSi10Mg multiple load path specimens. [Internet] [Masters thesis]. Delft University of Technology; 2021. [cited 2021 Apr 17]. Available from: http://resolver.tudelft.nl/uuid:52f34a92-8937-4b51-b2e5-8cacfcd24d27.

Council of Science Editors:

Hofwegen M(. Damage Tolerant Design for Additive Manufacturing: An experimental study on the fatigue behaviour of stretch dominated AlSi10Mg multiple load path specimens. [Masters Thesis]. Delft University of Technology; 2021. Available from: http://resolver.tudelft.nl/uuid:52f34a92-8937-4b51-b2e5-8cacfcd24d27


Loughborough University

30. 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 April 17, 2021. 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. 17 Apr 2021.

Vancouver:

Nash P. Experimental impact damage resistance and tolerance study of symmetrical and unsymmetrical composite sandwich panels. [Internet] [Doctoral dissertation]. Loughborough University; 2016. [cited 2021 Apr 17]. 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

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