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You searched for subject:(stiffened panel). Showing records 1 – 15 of 15 total matches.

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Cranfield University

1. Liu, Yifei. Optimum design of a composite outer wing subject to stiffness and strength constraints.

Degree: MSc by Research, 2011, Cranfield University

 Composite materials have been more and more used in aircraft primary structures such as wing and fuselage. The aim of this thesis is to identify… (more)

Subjects/Keywords: Stiffened panel; Buckling; Compressive load; Optimization

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APA (6th Edition):

Liu, Y. (2011). Optimum design of a composite outer wing subject to stiffness and strength constraints. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/6833

Chicago Manual of Style (16th Edition):

Liu, Yifei. “Optimum design of a composite outer wing subject to stiffness and strength constraints.” 2011. Masters Thesis, Cranfield University. Accessed January 24, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/6833.

MLA Handbook (7th Edition):

Liu, Yifei. “Optimum design of a composite outer wing subject to stiffness and strength constraints.” 2011. Web. 24 Jan 2020.

Vancouver:

Liu Y. Optimum design of a composite outer wing subject to stiffness and strength constraints. [Internet] [Masters thesis]. Cranfield University; 2011. [cited 2020 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/6833.

Council of Science Editors:

Liu Y. Optimum design of a composite outer wing subject to stiffness and strength constraints. [Masters Thesis]. Cranfield University; 2011. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/6833


University of Adelaide

2. Huang, Liang. Innovative multi-level methodology incorporating the techniques of finite element modelling and multimodal optimization for concept design of advanced grid stiffened composite panels against buckling.

Degree: 2015, University of Adelaide

 Since the Second World War fiber reinforced polymer (FRP) composites have become more attractive as a structural material in a variety of engineering practices, such… (more)

Subjects/Keywords: stiffened composite panel; concept design; FEM; multimodal optimization; buckling

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APA (6th Edition):

Huang, L. (2015). Innovative multi-level methodology incorporating the techniques of finite element modelling and multimodal optimization for concept design of advanced grid stiffened composite panels against buckling. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/98727

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):

Huang, Liang. “Innovative multi-level methodology incorporating the techniques of finite element modelling and multimodal optimization for concept design of advanced grid stiffened composite panels against buckling.” 2015. Thesis, University of Adelaide. Accessed January 24, 2020. http://hdl.handle.net/2440/98727.

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

MLA Handbook (7th Edition):

Huang, Liang. “Innovative multi-level methodology incorporating the techniques of finite element modelling and multimodal optimization for concept design of advanced grid stiffened composite panels against buckling.” 2015. Web. 24 Jan 2020.

Vancouver:

Huang L. Innovative multi-level methodology incorporating the techniques of finite element modelling and multimodal optimization for concept design of advanced grid stiffened composite panels against buckling. [Internet] [Thesis]. University of Adelaide; 2015. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/2440/98727.

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

Council of Science Editors:

Huang L. Innovative multi-level methodology incorporating the techniques of finite element modelling and multimodal optimization for concept design of advanced grid stiffened composite panels against buckling. [Thesis]. University of Adelaide; 2015. Available from: http://hdl.handle.net/2440/98727

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


Delft University of Technology

3. Bos, R.W. Hydrodynamic load simplification: Through Ultimate Strength of a Stiffened Panel:.

Degree: 2015, Delft University of Technology

Stiffened panels at the water line of a ship experience in-plane loads due to ship bending and torsion, as well as out-of-plane loads due to… (more)

Subjects/Keywords: stiffened panel; wave impact; ultimate strength; load simplification

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APA (6th Edition):

Bos, R. W. (2015). Hydrodynamic load simplification: Through Ultimate Strength of a Stiffened Panel:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0ca23d29-2338-46fc-b55e-35613372586c

Chicago Manual of Style (16th Edition):

Bos, R W. “Hydrodynamic load simplification: Through Ultimate Strength of a Stiffened Panel:.” 2015. Masters Thesis, Delft University of Technology. Accessed January 24, 2020. http://resolver.tudelft.nl/uuid:0ca23d29-2338-46fc-b55e-35613372586c.

MLA Handbook (7th Edition):

Bos, R W. “Hydrodynamic load simplification: Through Ultimate Strength of a Stiffened Panel:.” 2015. Web. 24 Jan 2020.

Vancouver:

Bos RW. Hydrodynamic load simplification: Through Ultimate Strength of a Stiffened Panel:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:0ca23d29-2338-46fc-b55e-35613372586c.

Council of Science Editors:

Bos RW. Hydrodynamic load simplification: Through Ultimate Strength of a Stiffened Panel:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:0ca23d29-2338-46fc-b55e-35613372586c


Washington University in St. Louis

4. Kim, Sunjung. Piezoelectric Control of Structures Prone to Instabilities.

Degree: PhD, Mechanical Engineering and Materials Science, 2010, Washington University in St. Louis

 Thin-walled structures such as stiffened panels fabricated out of high strength materials are ubiquitous in aerospace structures. These are prone to buckle in a variety… (more)

Subjects/Keywords: Applied Mechanics; Engineering, Mechanical; Engineering, Aerospace; control, flutter, instability, piezoelectricity, stiffened panel

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APA (6th Edition):

Kim, S. (2010). Piezoelectric Control of Structures Prone to Instabilities. (Doctoral Dissertation). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/etd/183

Chicago Manual of Style (16th Edition):

Kim, Sunjung. “Piezoelectric Control of Structures Prone to Instabilities.” 2010. Doctoral Dissertation, Washington University in St. Louis. Accessed January 24, 2020. https://openscholarship.wustl.edu/etd/183.

MLA Handbook (7th Edition):

Kim, Sunjung. “Piezoelectric Control of Structures Prone to Instabilities.” 2010. Web. 24 Jan 2020.

Vancouver:

Kim S. Piezoelectric Control of Structures Prone to Instabilities. [Internet] [Doctoral dissertation]. Washington University in St. Louis; 2010. [cited 2020 Jan 24]. Available from: https://openscholarship.wustl.edu/etd/183.

Council of Science Editors:

Kim S. Piezoelectric Control of Structures Prone to Instabilities. [Doctoral Dissertation]. Washington University in St. Louis; 2010. Available from: https://openscholarship.wustl.edu/etd/183


Virginia Tech

5. Zhao, Wei. Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings.

Degree: PhD, Aerospace and Ocean Engineering, 2017, Virginia Tech

 Large-aspect-ratio wings and composite structures both have been considered for the next-generation civil transport aircraft to achieve improved aerodynamic efficiency and to save aircraft structural… (more)

Subjects/Keywords: SpaRibs; bilevel programming optimization; aeroelastic tailoring; active aeroelastic wing; curvilinearly stiffened composite panel

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APA (6th Edition):

Zhao, W. (2017). Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/79143

Chicago Manual of Style (16th Edition):

Zhao, Wei. “Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings.” 2017. Doctoral Dissertation, Virginia Tech. Accessed January 24, 2020. http://hdl.handle.net/10919/79143.

MLA Handbook (7th Edition):

Zhao, Wei. “Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings.” 2017. Web. 24 Jan 2020.

Vancouver:

Zhao W. Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings. [Internet] [Doctoral dissertation]. Virginia Tech; 2017. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/10919/79143.

Council of Science Editors:

Zhao W. Optimal Design and Analysis of Bio-inspired, Curvilinearly Stiffened Composite Flexible Wings. [Doctoral Dissertation]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/79143


Virginia Tech

6. Liu, Qiang. EBF3GLWingOpt: A Framework for Multidisciplinary Design Optimization of Wings Using SpaRibs.

Degree: PhD, Engineering Science and Mechanics, 2014, Virginia Tech

 A global/local framework for multidisciplinary optimization of generalized aircraft wing structure has been developed. The concept of curvilinear stiffening members (spars, ribs and stiffeners) has… (more)

Subjects/Keywords: Structural Optimization; Global-local Optimization; Wing Optimization; Multidisciplinary Design Optimization; SpaRibs; Stiffened Panel Optimization

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APA (6th Edition):

Liu, Q. (2014). EBF3GLWingOpt: A Framework for Multidisciplinary Design Optimization of Wings Using SpaRibs. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/49665

Chicago Manual of Style (16th Edition):

Liu, Qiang. “EBF3GLWingOpt: A Framework for Multidisciplinary Design Optimization of Wings Using SpaRibs.” 2014. Doctoral Dissertation, Virginia Tech. Accessed January 24, 2020. http://hdl.handle.net/10919/49665.

MLA Handbook (7th Edition):

Liu, Qiang. “EBF3GLWingOpt: A Framework for Multidisciplinary Design Optimization of Wings Using SpaRibs.” 2014. Web. 24 Jan 2020.

Vancouver:

Liu Q. EBF3GLWingOpt: A Framework for Multidisciplinary Design Optimization of Wings Using SpaRibs. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/10919/49665.

Council of Science Editors:

Liu Q. EBF3GLWingOpt: A Framework for Multidisciplinary Design Optimization of Wings Using SpaRibs. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/49665


Cranfield University

7. Wang, Yang. Virtual testing of post-buckling behaviour of metallic stiffened panel.

Degree: MSc by Research, 2011, Cranfield University

 The aim of the project presented in this thesis is to demonstrate a modelling method for predicting the variability in the ultimate load of stiffened(more)

Subjects/Keywords: Buckling and Postbuckling; Stiffened panel; Geometric Imperfection; FE method; ABAQUS; FE modelling; Compression

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APA (6th Edition):

Wang, Y. (2011). Virtual testing of post-buckling behaviour of metallic stiffened panel. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7291

Chicago Manual of Style (16th Edition):

Wang, Yang. “Virtual testing of post-buckling behaviour of metallic stiffened panel.” 2011. Masters Thesis, Cranfield University. Accessed January 24, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/7291.

MLA Handbook (7th Edition):

Wang, Yang. “Virtual testing of post-buckling behaviour of metallic stiffened panel.” 2011. Web. 24 Jan 2020.

Vancouver:

Wang Y. Virtual testing of post-buckling behaviour of metallic stiffened panel. [Internet] [Masters thesis]. Cranfield University; 2011. [cited 2020 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7291.

Council of Science Editors:

Wang Y. Virtual testing of post-buckling behaviour of metallic stiffened panel. [Masters Thesis]. Cranfield University; 2011. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7291


Virginia Tech

8. Dippold, Samuel Mark. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels.

Degree: MS, Aerospace and Ocean Engineering, 2005, Virginia Tech

 This thesis presents the results of 67 ABAQUS elasto-plastic Riks ultimate strength analyses of cross-stiffened panels. These panels cover a wide range of typical geometries.… (more)

Subjects/Keywords: Stiffened Panel Ultimate Strength; Finite Element Simulation Panel Collapse; Panel Buckling and Collapse

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APA (6th Edition):

Dippold, S. M. (2005). Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33965

Chicago Manual of Style (16th Edition):

Dippold, Samuel Mark. “Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels.” 2005. Masters Thesis, Virginia Tech. Accessed January 24, 2020. http://hdl.handle.net/10919/33965.

MLA Handbook (7th Edition):

Dippold, Samuel Mark. “Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels.” 2005. Web. 24 Jan 2020.

Vancouver:

Dippold SM. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels. [Internet] [Masters thesis]. Virginia Tech; 2005. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/10919/33965.

Council of Science Editors:

Dippold SM. Validation of the ULSAP Closed-Form Method for Ultimate Strength Analysis of Cross-Stiffened Panels. [Masters Thesis]. Virginia Tech; 2005. Available from: http://hdl.handle.net/10919/33965

9. Jrad, Mohamed. Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures.

Degree: PhD, Engineering Science and Mechanics, 2015, Virginia Tech

 The structural optimization of a cantilever aircraft wing with curvilinear spars and ribs and stiffeners is described. The design concept of reinforcing the wing structure… (more)

Subjects/Keywords: Multidisciplinary optimization; stiffened panels; damage tolerance; stress intensity factor; composite panel; buckling; crack; global/local approach; finite element method; parallel computing

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APA (6th Edition):

Jrad, M. (2015). Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/52276

Chicago Manual of Style (16th Edition):

Jrad, Mohamed. “Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures.” 2015. Doctoral Dissertation, Virginia Tech. Accessed January 24, 2020. http://hdl.handle.net/10919/52276.

MLA Handbook (7th Edition):

Jrad, Mohamed. “Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures.” 2015. Web. 24 Jan 2020.

Vancouver:

Jrad M. Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/10919/52276.

Council of Science Editors:

Jrad M. Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/52276

10. Noevere, August T. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 In modern conceptual/preliminary design of aerospace vehicles it is common for a large number of concepts and configurations to be rapidly explored. For each configuration,… (more)

Subjects/Keywords: Structural optimization; Stiffened panel optimization; Conceptual design

…4.1.2 Accuracy for Metallic I-Stiffened Panel . . . . . . . . . . . . . . . . 144 4.1.3… …Stiffened Panel . . . . . . . . . . . . . . . . 149 4.2.3 Sources of Error… …Objective Function for the I-Stiffened Panel . . . . . . . . . . . . . 179 Stiffness-Based… …Stiffened Panel . . . . . . . . . . . . . . . 182 Validation of Mass Optimization… …5.4.2 5.5 Optimization Validation for the I-Stiffened Panel . . . . . . . . . . 184… 

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APA (6th Edition):

Noevere, A. T. (2016). Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55638

Chicago Manual of Style (16th Edition):

Noevere, August T. “Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.” 2016. Doctoral Dissertation, Georgia Tech. Accessed January 24, 2020. http://hdl.handle.net/1853/55638.

MLA Handbook (7th Edition):

Noevere, August T. “Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.” 2016. Web. 24 Jan 2020.

Vancouver:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/1853/55638.

Council of Science Editors:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55638


Brno University of Technology

11. Jurek, Peter. Hmotnostní optimalizace kesonu křídla letounu L 410 NG .

Degree: 2013, Brno University of Technology

 Táto diplomová práca sa zaoberá parametrickou optimalizáciou kesónu krídla letúna L 410 NG za účelom zníženia jeho hmotnosti. Práca je zameraná najmä na popis a… (more)

Subjects/Keywords: Optimalizácia kesónu; hmotnostná optimalizácia; parametrická optimalizácia; kontrola únosnosti; integrálny vystužený panel krídla; L 410; Caisson optimization; weight optimization; parametric optimization; loading state check; integrally stiffened wing panel; L 410

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APA (6th Edition):

Jurek, P. (2013). Hmotnostní optimalizace kesonu křídla letounu L 410 NG . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27164

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):

Jurek, Peter. “Hmotnostní optimalizace kesonu křídla letounu L 410 NG .” 2013. Thesis, Brno University of Technology. Accessed January 24, 2020. http://hdl.handle.net/11012/27164.

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

MLA Handbook (7th Edition):

Jurek, Peter. “Hmotnostní optimalizace kesonu křídla letounu L 410 NG .” 2013. Web. 24 Jan 2020.

Vancouver:

Jurek P. Hmotnostní optimalizace kesonu křídla letounu L 410 NG . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/11012/27164.

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

Council of Science Editors:

Jurek P. Hmotnostní optimalizace kesonu křídla letounu L 410 NG . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/27164

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


Brno University of Technology

12. Vlček, Dalibor. Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance .

Degree: 2013, Brno University of Technology

 Diplomová práce se zabývá provedením damage tolerance analýzy dolního integrálního panelu křídla letounu L410 NG zahrnující výpočet růstových křivek únavových trhlin, analýzu zbytkové pevnosti konstrukce… (more)

Subjects/Keywords: damage tolerance analýza; analýza šíření únavové trhliny; analýza zbytkové pevnosti; program prohlídek; integrální vyztužený panel křídla; damage tolerance evaluation; crack growth analysis; residual strength analysis; inspection program; integrally stiffened wing panel

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APA (6th Edition):

Vlček, D. (2013). Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/24718

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):

Vlček, Dalibor. “Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance .” 2013. Thesis, Brno University of Technology. Accessed January 24, 2020. http://hdl.handle.net/11012/24718.

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

MLA Handbook (7th Edition):

Vlček, Dalibor. “Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance .” 2013. Web. 24 Jan 2020.

Vancouver:

Vlček D. Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/11012/24718.

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

Council of Science Editors:

Vlček D. Stanovení životnosti dolního integrálního panelu křídla letounu L410 NG filozofií damage tolerance . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/24718

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

13. Deklerck, M. Optimization of stiffened panels using a combination of FEM and a predictor-corrector interior point method:.

Degree: 2016, Delft University of Technology

 Structural optimization, first introduced by Schmidt in 1960, is a rapid growing factor in the development of new aerospace structures. This growth is established by… (more)

Subjects/Keywords: structural optimization; stiffened panel; interior point method; conservative approximation; sequential convex programming

…of the most important structures in distinct field of engineering is a stiffened panel. In… …Chapter 2 Literature Study Optimizing a stiffened panel requires some general information… …detail. The global buckling load of a stiffened panel under uni-axial compression can be… …4 2.4 Buckling failure modes for stiffened panels [10]… …5 2.5 Panel Buckling… 

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APA (6th Edition):

Deklerck, M. (2016). Optimization of stiffened panels using a combination of FEM and a predictor-corrector interior point method:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d0715121-d6d3-4816-95b1-4254af5a75c1

Chicago Manual of Style (16th Edition):

Deklerck, M. “Optimization of stiffened panels using a combination of FEM and a predictor-corrector interior point method:.” 2016. Masters Thesis, Delft University of Technology. Accessed January 24, 2020. http://resolver.tudelft.nl/uuid:d0715121-d6d3-4816-95b1-4254af5a75c1.

MLA Handbook (7th Edition):

Deklerck, M. “Optimization of stiffened panels using a combination of FEM and a predictor-corrector interior point method:.” 2016. Web. 24 Jan 2020.

Vancouver:

Deklerck M. Optimization of stiffened panels using a combination of FEM and a predictor-corrector interior point method:. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:d0715121-d6d3-4816-95b1-4254af5a75c1.

Council of Science Editors:

Deklerck M. Optimization of stiffened panels using a combination of FEM and a predictor-corrector interior point method:. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:d0715121-d6d3-4816-95b1-4254af5a75c1


McMaster University

14. Thanga, Tharani. DESIGN METHODS FOR LARGE RECTANGULAR INDUSTRIAL DUCTS.

Degree: PhD, 2012, McMaster University

A large rectangular industrial duct consists of plates stiffened with parallel wide flange sections. The plates along with stiffeners acts to resist the pressure… (more)

Subjects/Keywords: Large Rectangular industrial duct; Stiffened plate panel; Finite element model; Parametric study; Large deflection plate theory; Partial yielding; Stiffener spacing; Plate thickness; Initial Imperfection; Residual Stress; Plate buckling; Overall buckling; Distortional Buckling; Shear Buckling; Normalized ultimate Shear; Diagonal Tension Field; Dimensional Analysis; Dimensionless parameters; Structural Engineering; Structural Engineering

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APA (6th Edition):

Thanga, T. (2012). DESIGN METHODS FOR LARGE RECTANGULAR INDUSTRIAL DUCTS. (Doctoral Dissertation). McMaster University. Retrieved from http://hdl.handle.net/11375/12276

Chicago Manual of Style (16th Edition):

Thanga, Tharani. “DESIGN METHODS FOR LARGE RECTANGULAR INDUSTRIAL DUCTS.” 2012. Doctoral Dissertation, McMaster University. Accessed January 24, 2020. http://hdl.handle.net/11375/12276.

MLA Handbook (7th Edition):

Thanga, Tharani. “DESIGN METHODS FOR LARGE RECTANGULAR INDUSTRIAL DUCTS.” 2012. Web. 24 Jan 2020.

Vancouver:

Thanga T. DESIGN METHODS FOR LARGE RECTANGULAR INDUSTRIAL DUCTS. [Internet] [Doctoral dissertation]. McMaster University; 2012. [cited 2020 Jan 24]. Available from: http://hdl.handle.net/11375/12276.

Council of Science Editors:

Thanga T. DESIGN METHODS FOR LARGE RECTANGULAR INDUSTRIAL DUCTS. [Doctoral Dissertation]. McMaster University; 2012. Available from: http://hdl.handle.net/11375/12276

15. Fox, Elijah D. Residual Ultimate Buckling Strength of Steel Stiffened Panels Subjected to Corrosion Damage.

Degree: MSin Engineering, Civil Engineering, 2017, University of Akron

 Corrosion is a naturally occurring electro-chemical process that causes damage in the form of surface material deterioration on metal structures. In many industries, particularly naval… (more)

Subjects/Keywords: Civil Engineering; Engineering; A-572 steel, uniform corrosion, pitting corrosion, grooving corrosion, axial compression, lateral pressure, stiffened panel, FEA, combined loading

…12: typical stiffened panel section with a flange… …51 Figure 13: Typical stiffened panel arrangement in ship hull structures… …52 Figure 14: Uniaxial (longitudinal) stiffened panel… …53 Figure 15: Orthogonal stiffened panel… …53 Figure 16: Stiffened Panel terminology [35]… 

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APA (6th Edition):

Fox, E. D. (2017). Residual Ultimate Buckling Strength of Steel Stiffened Panels Subjected to Corrosion Damage. (Masters Thesis). University of Akron. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=akron1493987459107873

Chicago Manual of Style (16th Edition):

Fox, Elijah D. “Residual Ultimate Buckling Strength of Steel Stiffened Panels Subjected to Corrosion Damage.” 2017. Masters Thesis, University of Akron. Accessed January 24, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=akron1493987459107873.

MLA Handbook (7th Edition):

Fox, Elijah D. “Residual Ultimate Buckling Strength of Steel Stiffened Panels Subjected to Corrosion Damage.” 2017. Web. 24 Jan 2020.

Vancouver:

Fox ED. Residual Ultimate Buckling Strength of Steel Stiffened Panels Subjected to Corrosion Damage. [Internet] [Masters thesis]. University of Akron; 2017. [cited 2020 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=akron1493987459107873.

Council of Science Editors:

Fox ED. Residual Ultimate Buckling Strength of Steel Stiffened Panels Subjected to Corrosion Damage. [Masters Thesis]. University of Akron; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=akron1493987459107873

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