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You searched for subject:(Composites Design Optimization). Showing records 1 – 10 of 10 total matches.

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University of South Carolina

1. Bahamonde Jácome, Luis G. 3D Topology Optimization of Spatially Reinforced Composites.

Degree: PhD, Mechanical Engineering, 2019, University of South Carolina

  Topology optimization is a numerical design tool used to generate structural concepts that present optimal load paths for a given set of functional requirements.… (more)

Subjects/Keywords: Engineering; Mechanical Engineering; 3D topology optimization; spatially reinforced composites; functional generative design; macromechanical model; stable coupling algorithm; scalable optimization algorithm

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APA (6th Edition):

Bahamonde Jácome, L. G. (2019). 3D Topology Optimization of Spatially Reinforced Composites. (Doctoral Dissertation). University of South Carolina. Retrieved from https://scholarcommons.sc.edu/etd/5457

Chicago Manual of Style (16th Edition):

Bahamonde Jácome, Luis G. “3D Topology Optimization of Spatially Reinforced Composites.” 2019. Doctoral Dissertation, University of South Carolina. Accessed March 05, 2021. https://scholarcommons.sc.edu/etd/5457.

MLA Handbook (7th Edition):

Bahamonde Jácome, Luis G. “3D Topology Optimization of Spatially Reinforced Composites.” 2019. Web. 05 Mar 2021.

Vancouver:

Bahamonde Jácome LG. 3D Topology Optimization of Spatially Reinforced Composites. [Internet] [Doctoral dissertation]. University of South Carolina; 2019. [cited 2021 Mar 05]. Available from: https://scholarcommons.sc.edu/etd/5457.

Council of Science Editors:

Bahamonde Jácome LG. 3D Topology Optimization of Spatially Reinforced Composites. [Doctoral Dissertation]. University of South Carolina; 2019. Available from: https://scholarcommons.sc.edu/etd/5457


Université de Bordeaux I

2. Mouton, Serge. Intégration des contraintes d’industrialisation des pièces en matériaux composites pour l’aide à la décision en conception préliminaire appliquée au procédé RTM : Transmission and appropriation of language in a postcolonial context : the case of Haïti.

Degree: Docteur es, Mécanique, 2010, Université de Bordeaux I

 L’intégration des contraintes d’industrialisation, des pièces en matériaux composites, en conception préliminaire, est un enjeu majeur de la compétitivité des entreprises, et s’inscrit dans une… (more)

Subjects/Keywords: Conception préliminaire; Simulations éléments finis; Optimisation; Assemblage; Matériaux composites; Resin transfer molding; Preliminary design; Resin transfer molding; Finite element simulations; Optimization; Composite materials; Assembly; Design for manufacturing

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APA (6th Edition):

Mouton, S. (2010). Intégration des contraintes d’industrialisation des pièces en matériaux composites pour l’aide à la décision en conception préliminaire appliquée au procédé RTM : Transmission and appropriation of language in a postcolonial context : the case of Haïti. (Doctoral Dissertation). Université de Bordeaux I. Retrieved from http://www.theses.fr/2010BOR14029

Chicago Manual of Style (16th Edition):

Mouton, Serge. “Intégration des contraintes d’industrialisation des pièces en matériaux composites pour l’aide à la décision en conception préliminaire appliquée au procédé RTM : Transmission and appropriation of language in a postcolonial context : the case of Haïti.” 2010. Doctoral Dissertation, Université de Bordeaux I. Accessed March 05, 2021. http://www.theses.fr/2010BOR14029.

MLA Handbook (7th Edition):

Mouton, Serge. “Intégration des contraintes d’industrialisation des pièces en matériaux composites pour l’aide à la décision en conception préliminaire appliquée au procédé RTM : Transmission and appropriation of language in a postcolonial context : the case of Haïti.” 2010. Web. 05 Mar 2021.

Vancouver:

Mouton S. Intégration des contraintes d’industrialisation des pièces en matériaux composites pour l’aide à la décision en conception préliminaire appliquée au procédé RTM : Transmission and appropriation of language in a postcolonial context : the case of Haïti. [Internet] [Doctoral dissertation]. Université de Bordeaux I; 2010. [cited 2021 Mar 05]. Available from: http://www.theses.fr/2010BOR14029.

Council of Science Editors:

Mouton S. Intégration des contraintes d’industrialisation des pièces en matériaux composites pour l’aide à la décision en conception préliminaire appliquée au procédé RTM : Transmission and appropriation of language in a postcolonial context : the case of Haïti. [Doctoral Dissertation]. Université de Bordeaux I; 2010. Available from: http://www.theses.fr/2010BOR14029


Virginia Tech

3. Henderson, Joseph Lynn. Combined structural and manufacturing optimization of stiffened composite panels.

Degree: MS, Aerospace Engineering, 1996, Virginia Tech

  Manufacturing considerations have been incorporated into the design optimization of a blade-stiffened composite panel. For the manufacturing analysis, a one-dimensional resin film infusion model… (more)

Subjects/Keywords: composites; structures; manufacturing; design optimization; genetic algorithms; stiffened panels; LD5655.V855 1996.H463

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APA (6th Edition):

Henderson, J. L. (1996). Combined structural and manufacturing optimization of stiffened composite panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44819

Chicago Manual of Style (16th Edition):

Henderson, Joseph Lynn. “Combined structural and manufacturing optimization of stiffened composite panels.” 1996. Masters Thesis, Virginia Tech. Accessed March 05, 2021. http://hdl.handle.net/10919/44819.

MLA Handbook (7th Edition):

Henderson, Joseph Lynn. “Combined structural and manufacturing optimization of stiffened composite panels.” 1996. Web. 05 Mar 2021.

Vancouver:

Henderson JL. Combined structural and manufacturing optimization of stiffened composite panels. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2021 Mar 05]. Available from: http://hdl.handle.net/10919/44819.

Council of Science Editors:

Henderson JL. Combined structural and manufacturing optimization of stiffened composite panels. [Masters Thesis]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/44819


Indian Institute of Science

4. Naik, G Narayana. Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion.

Degree: PhD, Faculty of Enginering, 2009, Indian Institute of Science

 In recent years, use of composites is increasing in most fields of engineering such as aerospace, automotive, civil construction, marine, prosthetics, etc., because of its… (more)

Subjects/Keywords: Structural Analysis; Laminated Composites; Composites - Design Optimization; Failure Mechanism Based Failure Criterion; Composite Laminates - Failure Mechanism Based Design; Vector Evaluated Particle Swarm Optimization; Genetic Algorithms; Composite Laminates; Composite Laminae; Composite Structures; Design Optimization; Failure Criterion; Structural Engineering

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APA (6th Edition):

Naik, G. N. (2009). Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/469

Chicago Manual of Style (16th Edition):

Naik, G Narayana. “Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion.” 2009. Doctoral Dissertation, Indian Institute of Science. Accessed March 05, 2021. http://etd.iisc.ac.in/handle/2005/469.

MLA Handbook (7th Edition):

Naik, G Narayana. “Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion.” 2009. Web. 05 Mar 2021.

Vancouver:

Naik GN. Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2009. [cited 2021 Mar 05]. Available from: http://etd.iisc.ac.in/handle/2005/469.

Council of Science Editors:

Naik GN. Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion. [Doctoral Dissertation]. Indian Institute of Science; 2009. Available from: http://etd.iisc.ac.in/handle/2005/469

5. Fontecha Dulcey, Gilberto. Modèle paramétrique, réduit et multi-échelle pour l’optimisation interactive de structures composites : Modelo paramétrico, reducido y multiescala para la optimización interactiva de estructuras compuestas.

Degree: Docteur es, Mécanique, 2018, Bordeaux

Concevoir une structure composite consiste à relever un défi de taille : alors qu'un ingénieur qui conçoit un produit mécanique à base de matériau métallique… (more)

Subjects/Keywords: Modèle réduit et paramétrique; Optimization interactive; Aide à la décision en conception; PGD; Viscoélasticité; Matériaux composites; Parametric and reduced model; Interactive optimization; Design support system; PGD; Viscoelasticity; Composite materials; Modelo reducido y paramétrico; Optimización interactiva; Ayuda a la decisión en diseño; PGD; Viscoelasticidad; Materiales compuestos

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APA (6th Edition):

Fontecha Dulcey, G. (2018). Modèle paramétrique, réduit et multi-échelle pour l’optimisation interactive de structures composites : Modelo paramétrico, reducido y multiescala para la optimización interactiva de estructuras compuestas. (Doctoral Dissertation). Bordeaux. Retrieved from http://www.theses.fr/2018BORD0247

Chicago Manual of Style (16th Edition):

Fontecha Dulcey, Gilberto. “Modèle paramétrique, réduit et multi-échelle pour l’optimisation interactive de structures composites : Modelo paramétrico, reducido y multiescala para la optimización interactiva de estructuras compuestas.” 2018. Doctoral Dissertation, Bordeaux. Accessed March 05, 2021. http://www.theses.fr/2018BORD0247.

MLA Handbook (7th Edition):

Fontecha Dulcey, Gilberto. “Modèle paramétrique, réduit et multi-échelle pour l’optimisation interactive de structures composites : Modelo paramétrico, reducido y multiescala para la optimización interactiva de estructuras compuestas.” 2018. Web. 05 Mar 2021.

Vancouver:

Fontecha Dulcey G. Modèle paramétrique, réduit et multi-échelle pour l’optimisation interactive de structures composites : Modelo paramétrico, reducido y multiescala para la optimización interactiva de estructuras compuestas. [Internet] [Doctoral dissertation]. Bordeaux; 2018. [cited 2021 Mar 05]. Available from: http://www.theses.fr/2018BORD0247.

Council of Science Editors:

Fontecha Dulcey G. Modèle paramétrique, réduit et multi-échelle pour l’optimisation interactive de structures composites : Modelo paramétrico, reducido y multiescala para la optimización interactiva de estructuras compuestas. [Doctoral Dissertation]. Bordeaux; 2018. Available from: http://www.theses.fr/2018BORD0247

6. Brooks, Timothy. Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 In the last 30 years since their introduction into aerospace applications, composites have become increasingly used, making up as much as 50% of modern aircraft… (more)

Subjects/Keywords: Multi-disciplinary design optimization; Tow-steered composites; Aeroelastic wing design; Aerospace Engineering; Engineering

…stencil . . . . . . . . . . . . . . . . . . . . . . . . . . 3.7 Design optimization… …specifications . . . . . . . . . . . . . . . . . . . . . . . 3.8 uCRM-13.5 optimization design… …variables. . . . . . . . . . . . . . . . . . . 3.9 uCRM-13.5 optimization design constraints… …for the composites used on skin, ribs, and spars Structural optimization problem… …Fuel burn optimization design variables . . . . . . . . . . . . . . . . Fuel burn… 

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APA (6th Edition):

Brooks, T. (2018). Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/145830

Chicago Manual of Style (16th Edition):

Brooks, Timothy. “Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites.” 2018. Doctoral Dissertation, University of Michigan. Accessed March 05, 2021. http://hdl.handle.net/2027.42/145830.

MLA Handbook (7th Edition):

Brooks, Timothy. “Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites.” 2018. Web. 05 Mar 2021.

Vancouver:

Brooks T. Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Mar 05]. Available from: http://hdl.handle.net/2027.42/145830.

Council of Science Editors:

Brooks T. Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/145830

7. Silva, João. Design and optimization of a wing structure for a UAS class I 145 kg.

Degree: 2017, RCAAP

Alferes Aluno ENGAER 137735-D. Estabelecimentos de ensino superior: AFA/IST

In the context of air power in a Global scale, unmanned aerial systems (UAS) are a… (more)

Subjects/Keywords: Air power; FAP; UAS class I; Wing structural design; Structural optimization; Composites; Poder aéreo; FAP; UAS class I; Design estrutural de asa; Otimização estrutural; Compósitos; Domínio/Área Científica::Engenharia e Tecnologia::Engenharia dos Materiais

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APA (6th Edition):

Silva, J. (2017). Design and optimization of a wing structure for a UAS class I 145 kg. (Thesis). RCAAP. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/23156

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):

Silva, João. “Design and optimization of a wing structure for a UAS class I 145 kg.” 2017. Thesis, RCAAP. Accessed March 05, 2021. https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/23156.

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

MLA Handbook (7th Edition):

Silva, João. “Design and optimization of a wing structure for a UAS class I 145 kg.” 2017. Web. 05 Mar 2021.

Vancouver:

Silva J. Design and optimization of a wing structure for a UAS class I 145 kg. [Internet] [Thesis]. RCAAP; 2017. [cited 2021 Mar 05]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/23156.

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

Council of Science Editors:

Silva J. Design and optimization of a wing structure for a UAS class I 145 kg. [Thesis]. RCAAP; 2017. Available from: https://www.rcaap.pt/detail.jsp?id=oai:comum.rcaap.pt:10400.26/23156

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

8. Nielsen, Mark. Design of aerospace laminates for multi-axis loading and damage tolerance.

Degree: PhD, 2018, University of Bath

 Acknowledging the goal of reduced aircraft weight, there is a need to improve on conservative design techniques used in industry. Minimisation of laminate in-plane elastic… (more)

Subjects/Keywords: 621; Laminate; Design; Composites; Optimization; Damage tolerance; stiffness tailoring; Design Rules; Forming; Minimum mass; Uncertainty; Robust Design

…118 5.5.2 Minimum Energy design strategies and non-uniqueness of designs… …119 5.5.3 5.6 Industrial design rules versus designing for uncertainty . . . . 121… …Work and Preliminary Damage Tolerance Design 164 9.1 Future Objectives… …Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 165 9.4 Design… …168 9.4.3 Design Independent of Thickness . . . . . . . . . . . . . . . . 168 9.5… 

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APA (6th Edition):

Nielsen, M. (2018). Design of aerospace laminates for multi-axis loading and damage tolerance. (Doctoral Dissertation). University of Bath. Retrieved from https://researchportal.bath.ac.uk/en/studentthesis/design-of-aerospace-laminates-for-multiaxis-loading-and-damage-tolerance(3248c9d9-ed8a-4f50-914a-c12277bf942e).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.760971

Chicago Manual of Style (16th Edition):

Nielsen, Mark. “Design of aerospace laminates for multi-axis loading and damage tolerance.” 2018. Doctoral Dissertation, University of Bath. Accessed March 05, 2021. https://researchportal.bath.ac.uk/en/studentthesis/design-of-aerospace-laminates-for-multiaxis-loading-and-damage-tolerance(3248c9d9-ed8a-4f50-914a-c12277bf942e).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.760971.

MLA Handbook (7th Edition):

Nielsen, Mark. “Design of aerospace laminates for multi-axis loading and damage tolerance.” 2018. Web. 05 Mar 2021.

Vancouver:

Nielsen M. Design of aerospace laminates for multi-axis loading and damage tolerance. [Internet] [Doctoral dissertation]. University of Bath; 2018. [cited 2021 Mar 05]. Available from: https://researchportal.bath.ac.uk/en/studentthesis/design-of-aerospace-laminates-for-multiaxis-loading-and-damage-tolerance(3248c9d9-ed8a-4f50-914a-c12277bf942e).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.760971.

Council of Science Editors:

Nielsen M. Design of aerospace laminates for multi-axis loading and damage tolerance. [Doctoral Dissertation]. University of Bath; 2018. Available from: https://researchportal.bath.ac.uk/en/studentthesis/design-of-aerospace-laminates-for-multiaxis-loading-and-damage-tolerance(3248c9d9-ed8a-4f50-914a-c12277bf942e).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.760971

9. Tita, Volnei. Análise dinâmica teórica e experimental de vigas fabricadas a partir de materiais compósitos poliméricos reforçados.

Degree: Mestrado, Engenharia Mecânica, 1999, University of São Paulo

Os materiais compósitos (composites) poliméricos reforçados são bem conhecidos por sua excelente combinação de alta rigidez estrutural e baixo peso. Sua inerente anisotropia permite ao… (more)

Subjects/Keywords: amortecimento; análise modal; composites; compósitos; damping; design optimization; finite element method; método dos elementos finitos; modal analysis; vibrações; vibration

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APA (6th Edition):

Tita, V. (1999). Análise dinâmica teórica e experimental de vigas fabricadas a partir de materiais compósitos poliméricos reforçados. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18135/tde-01062001-171428/ ;

Chicago Manual of Style (16th Edition):

Tita, Volnei. “Análise dinâmica teórica e experimental de vigas fabricadas a partir de materiais compósitos poliméricos reforçados.” 1999. Masters Thesis, University of São Paulo. Accessed March 05, 2021. http://www.teses.usp.br/teses/disponiveis/18/18135/tde-01062001-171428/ ;.

MLA Handbook (7th Edition):

Tita, Volnei. “Análise dinâmica teórica e experimental de vigas fabricadas a partir de materiais compósitos poliméricos reforçados.” 1999. Web. 05 Mar 2021.

Vancouver:

Tita V. Análise dinâmica teórica e experimental de vigas fabricadas a partir de materiais compósitos poliméricos reforçados. [Internet] [Masters thesis]. University of São Paulo; 1999. [cited 2021 Mar 05]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18135/tde-01062001-171428/ ;.

Council of Science Editors:

Tita V. Análise dinâmica teórica e experimental de vigas fabricadas a partir de materiais compósitos poliméricos reforçados. [Masters Thesis]. University of São Paulo; 1999. Available from: http://www.teses.usp.br/teses/disponiveis/18/18135/tde-01062001-171428/ ;

10. Gencturk, Bora. Multi-objective optimal seismic design of buildings using advanced engineering materials.

Degree: PhD, 0106, 2011, University of Illinois – Urbana-Champaign

 Although seismic safety remains a major concern of society – and unfortunately this observation has been underpinned by recent earthquakes – economy and sustainability in seismic design(more)

Subjects/Keywords: Engineered Cementitious Composites (ECC); Reinforced Concrete; Sustainability; Small-Scale Testing; Life-Cycle Cost Analysis; Optimization; Taboo Search; Dynamic Analysis; Finite Element Analysis; Constitutive Model; Performance-Based Seismic Design; Probabilistic Seismic Hazard Analysis; Spectrum Matching; Ground Motion Selection

…123 5.1.5. Optimization in Structural Design… …9 2.1.1. Evolution of Fiber Reinforced Cementitious Composites and Development of ECC… …47 3.2.2. Engineered Cementitious Composites… …53 3.3. DESIGN OF EXPERIMENTAL COLUMNS AND THE STRUCTURAL FRAME… …60 3.4.1. Formwork Design… 

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APA (6th Edition):

Gencturk, B. (2011). Multi-objective optimal seismic design of buildings using advanced engineering materials. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/26252

Chicago Manual of Style (16th Edition):

Gencturk, Bora. “Multi-objective optimal seismic design of buildings using advanced engineering materials.” 2011. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed March 05, 2021. http://hdl.handle.net/2142/26252.

MLA Handbook (7th Edition):

Gencturk, Bora. “Multi-objective optimal seismic design of buildings using advanced engineering materials.” 2011. Web. 05 Mar 2021.

Vancouver:

Gencturk B. Multi-objective optimal seismic design of buildings using advanced engineering materials. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2011. [cited 2021 Mar 05]. Available from: http://hdl.handle.net/2142/26252.

Council of Science Editors:

Gencturk B. Multi-objective optimal seismic design of buildings using advanced engineering materials. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/26252

.