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You searched for subject:(stiffened panels). Showing records 1 – 16 of 16 total matches.

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Virginia Tech

1. Uzman, Burak Jr. Thermal Analysis and Response of Grid-Stiffened Composite Panels.

Degree: MS, Engineering Science and Mechanics, 1997, Virginia Tech

 A study aimed at determining the thermal deformation response and thermal buckling loads of rectangular grid-stiffened composite panels is presented. Two edge conditions are considered… (more)

Subjects/Keywords: Grid; Stiffened; Buckling; Composite Panels

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APA (6th Edition):

Uzman, B. J. (1997). Thermal Analysis and Response of Grid-Stiffened Composite Panels. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31381

Chicago Manual of Style (16th Edition):

Uzman, Burak Jr. “Thermal Analysis and Response of Grid-Stiffened Composite Panels.” 1997. Masters Thesis, Virginia Tech. Accessed April 11, 2021. http://hdl.handle.net/10919/31381.

MLA Handbook (7th Edition):

Uzman, Burak Jr. “Thermal Analysis and Response of Grid-Stiffened Composite Panels.” 1997. Web. 11 Apr 2021.

Vancouver:

Uzman BJ. Thermal Analysis and Response of Grid-Stiffened Composite Panels. [Internet] [Masters thesis]. Virginia Tech; 1997. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10919/31381.

Council of Science Editors:

Uzman BJ. Thermal Analysis and Response of Grid-Stiffened Composite Panels. [Masters Thesis]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/31381


Virginia Tech

2. Beji, Faycel Ben Hedi. Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure.

Degree: MS, Aerospace Engineering, 2018, Virginia Tech

 Stiffeners attached to composite panels and shells may significantly increase the overall buckling load of the resultant stiffened structure. Initially, an extensive literature review was… (more)

Subjects/Keywords: Aerospace Material; Composites; Buckling analysis of Stiffened Panels; Buckling analysis of Isogrid Stiffened Shells; Parametric Study

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APA (6th Edition):

Beji, F. B. H. (2018). Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/81620

Chicago Manual of Style (16th Edition):

Beji, Faycel Ben Hedi. “Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure.” 2018. Masters Thesis, Virginia Tech. Accessed April 11, 2021. http://hdl.handle.net/10919/81620.

MLA Handbook (7th Edition):

Beji, Faycel Ben Hedi. “Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure.” 2018. Web. 11 Apr 2021.

Vancouver:

Beji FBH. Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10919/81620.

Council of Science Editors:

Beji FBH. Buckling Analysis of Composite Stiffened Panels and Shells in Aerospace Structure. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/81620


Delft University of Technology

3. Cabot Talens, E. (author). Semi-analytical solutions for buckling and post-buckling of composite plates: Application to stiffened Panels.

Degree: 2016, Delft University of Technology

This MSc thesis addresses the study of buckling and post-buckling of composite plates with elastic restraints at the edges and under any combination of in-plane… (more)

Subjects/Keywords: buckling; post-buckling; plates; semi-analytical; composite laminates; combined loading; rotationally-restrained; stiffened panels

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APA (6th Edition):

Cabot Talens, E. (. (2016). Semi-analytical solutions for buckling and post-buckling of composite plates: Application to stiffened Panels. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:deb7f375-e5ae-4711-8b1f-41153444d5b5

Chicago Manual of Style (16th Edition):

Cabot Talens, E (author). “Semi-analytical solutions for buckling and post-buckling of composite plates: Application to stiffened Panels.” 2016. Masters Thesis, Delft University of Technology. Accessed April 11, 2021. http://resolver.tudelft.nl/uuid:deb7f375-e5ae-4711-8b1f-41153444d5b5.

MLA Handbook (7th Edition):

Cabot Talens, E (author). “Semi-analytical solutions for buckling and post-buckling of composite plates: Application to stiffened Panels.” 2016. Web. 11 Apr 2021.

Vancouver:

Cabot Talens E(. Semi-analytical solutions for buckling and post-buckling of composite plates: Application to stiffened Panels. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Apr 11]. Available from: http://resolver.tudelft.nl/uuid:deb7f375-e5ae-4711-8b1f-41153444d5b5.

Council of Science Editors:

Cabot Talens E(. Semi-analytical solutions for buckling and post-buckling of composite plates: Application to stiffened Panels. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:deb7f375-e5ae-4711-8b1f-41153444d5b5


Virginia Tech

4. Ragon, Scott Alan II. Development of a Global/Local Approach and a Geometrically Non-linear Local Panel Analysis for Structural Design.

Degree: PhD, Engineering Mechanics, 1998, Virginia Tech

 A computationally efficient analysis capability for the geometrically non-linear response of compressively loaded prismatic plate structures was developed. Both a "full" finite strip solution procedure… (more)

Subjects/Keywords: non-linear analysis; postbuckling; stiffened panels; design optimization

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APA (6th Edition):

Ragon, S. A. I. (1998). Development of a Global/Local Approach and a Geometrically Non-linear Local Panel Analysis for Structural Design. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30761

Chicago Manual of Style (16th Edition):

Ragon, Scott Alan II. “Development of a Global/Local Approach and a Geometrically Non-linear Local Panel Analysis for Structural Design.” 1998. Doctoral Dissertation, Virginia Tech. Accessed April 11, 2021. http://hdl.handle.net/10919/30761.

MLA Handbook (7th Edition):

Ragon, Scott Alan II. “Development of a Global/Local Approach and a Geometrically Non-linear Local Panel Analysis for Structural Design.” 1998. Web. 11 Apr 2021.

Vancouver:

Ragon SAI. Development of a Global/Local Approach and a Geometrically Non-linear Local Panel Analysis for Structural Design. [Internet] [Doctoral dissertation]. Virginia Tech; 1998. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10919/30761.

Council of Science Editors:

Ragon SAI. Development of a Global/Local Approach and a Geometrically Non-linear Local Panel Analysis for Structural Design. [Doctoral Dissertation]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/30761

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

Degree: PhD, Engineering 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 April 11, 2021. http://hdl.handle.net/10919/52276.

MLA Handbook (7th Edition):

Jrad, Mohamed. “Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures.” 2015. Web. 11 Apr 2021.

Vancouver:

Jrad M. Multidisciplinary Optimization and Damage Tolerance of Stiffened Structures. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2021 Apr 11]. 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


University of Kentucky

6. Navalpakkam, Prathik. MODELING AND TESTING ULTRA-LIGHTWEIGHT THERMOFORM-STIFFENED PANELS.

Degree: 2005, University of Kentucky

 Ultra-lightweight thermoformed stiffened structures are emerging as a viable option for spacecraft applications due to their advantage over inflatable structures. Although pressurization may be used… (more)

Subjects/Keywords: Thermoformed stiffened panels; conical stiffener units; modal testing

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APA (6th Edition):

Navalpakkam, P. (2005). MODELING AND TESTING ULTRA-LIGHTWEIGHT THERMOFORM-STIFFENED PANELS. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/gradschool_theses/350

Chicago Manual of Style (16th Edition):

Navalpakkam, Prathik. “MODELING AND TESTING ULTRA-LIGHTWEIGHT THERMOFORM-STIFFENED PANELS.” 2005. Masters Thesis, University of Kentucky. Accessed April 11, 2021. https://uknowledge.uky.edu/gradschool_theses/350.

MLA Handbook (7th Edition):

Navalpakkam, Prathik. “MODELING AND TESTING ULTRA-LIGHTWEIGHT THERMOFORM-STIFFENED PANELS.” 2005. Web. 11 Apr 2021.

Vancouver:

Navalpakkam P. MODELING AND TESTING ULTRA-LIGHTWEIGHT THERMOFORM-STIFFENED PANELS. [Internet] [Masters thesis]. University of Kentucky; 2005. [cited 2021 Apr 11]. Available from: https://uknowledge.uky.edu/gradschool_theses/350.

Council of Science Editors:

Navalpakkam P. MODELING AND TESTING ULTRA-LIGHTWEIGHT THERMOFORM-STIFFENED PANELS. [Masters Thesis]. University of Kentucky; 2005. Available from: https://uknowledge.uky.edu/gradschool_theses/350


University of Michigan

7. Mesa, Jose. Hydroelastic Analysis of Aluminum and Composite High-Speed Planing Craft Structures During Slamming.

Degree: PhD, Naval Architecture & Marine Engineering, 2018, University of Michigan

 The design of optimal planing craft structures is a challenging process that must take into account aspects such as cost, weight, operability, maintainability, manufacturability, and… (more)

Subjects/Keywords: Fluid-Structure Interaction; Flat-Plate Ditching; Slamming Finite-Span Effects; Composite Hydroelastic Analysis; Stiffened Panels Hydroelastic Assessment; Naval Architecture and Marine Engineering; Engineering

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APA (6th Edition):

Mesa, J. (2018). Hydroelastic Analysis of Aluminum and Composite High-Speed Planing Craft Structures During Slamming. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/147645

Chicago Manual of Style (16th Edition):

Mesa, Jose. “Hydroelastic Analysis of Aluminum and Composite High-Speed Planing Craft Structures During Slamming.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 11, 2021. http://hdl.handle.net/2027.42/147645.

MLA Handbook (7th Edition):

Mesa, Jose. “Hydroelastic Analysis of Aluminum and Composite High-Speed Planing Craft Structures During Slamming.” 2018. Web. 11 Apr 2021.

Vancouver:

Mesa J. Hydroelastic Analysis of Aluminum and Composite High-Speed Planing Craft Structures During Slamming. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/2027.42/147645.

Council of Science Editors:

Mesa J. Hydroelastic Analysis of Aluminum and Composite High-Speed Planing Craft Structures During Slamming. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/147645


Delft University of Technology

8. Verolme, J.L. The Development of a Design Tool for Fiber Metal Laminate Compression Panels.

Degree: 1995, Delft University of Technology

Subjects/Keywords: aeronautics; compressive loads; buckling; stiffened panels; failure; design; fiber metal laminates; aluminum

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APA (6th Edition):

Verolme, J. L. (1995). The Development of a Design Tool for Fiber Metal Laminate Compression Panels. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f

Chicago Manual of Style (16th Edition):

Verolme, J L. “The Development of a Design Tool for Fiber Metal Laminate Compression Panels.” 1995. Doctoral Dissertation, Delft University of Technology. Accessed April 11, 2021. http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f.

MLA Handbook (7th Edition):

Verolme, J L. “The Development of a Design Tool for Fiber Metal Laminate Compression Panels.” 1995. Web. 11 Apr 2021.

Vancouver:

Verolme JL. The Development of a Design Tool for Fiber Metal Laminate Compression Panels. [Internet] [Doctoral dissertation]. Delft University of Technology; 1995. [cited 2021 Apr 11]. Available from: http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f.

Council of Science Editors:

Verolme JL. The Development of a Design Tool for Fiber Metal Laminate Compression Panels. [Doctoral Dissertation]. Delft University of Technology; 1995. Available from: http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; urn:NBN:nl:ui:24-uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f ; http://resolver.tudelft.nl/uuid:e756a461-fd22-4406-9b1c-3afb76dbad9f


Virginia Tech

9. Chen, Yong. Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method.

Degree: PhD, Aerospace and Ocean Engineering, 2003, Virginia Tech

 An efficient beam-column approach, using an improved step-by-step numerical method, is developed in the current research for studying the ultimate strength problems of stiffened panels(more)

Subjects/Keywords: ultimate strength; orthotropic plate method; beam-column method; stiffened panels

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APA (6th Edition):

Chen, Y. (2003). Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26000

Chicago Manual of Style (16th Edition):

Chen, Yong. “Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method.” 2003. Doctoral Dissertation, Virginia Tech. Accessed April 11, 2021. http://hdl.handle.net/10919/26000.

MLA Handbook (7th Edition):

Chen, Yong. “Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method.” 2003. Web. 11 Apr 2021.

Vancouver:

Chen Y. Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method. [Internet] [Doctoral dissertation]. Virginia Tech; 2003. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10919/26000.

Council of Science Editors:

Chen Y. Ultimate Strength Analysis of Stiffened Panels Using a Beam-Column Method. [Doctoral Dissertation]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/26000


Virginia Tech

10. 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 April 11, 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. 11 Apr 2021.

Vancouver:

Henderson JL. Combined structural and manufacturing optimization of stiffened composite panels. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2021 Apr 11]. 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


Virginia Tech

11. Nelson, Erik Walter. Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication.

Degree: MS, Aerospace and Ocean Engineering, 2008, Virginia Tech

 Unitized aircraft structures have the potential to be more efficient than current aircraft structures. The Electron Beam Freeform Fabrication (EBF3) process can be used to… (more)

Subjects/Keywords: stiffener; buckling; stiffened panels; shear; compression; finite element analysis; Electron Beam Freeform Fabrication

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APA (6th Edition):

Nelson, E. W. (2008). Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43583

Chicago Manual of Style (16th Edition):

Nelson, Erik Walter. “Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication.” 2008. Masters Thesis, Virginia Tech. Accessed April 11, 2021. http://hdl.handle.net/10919/43583.

MLA Handbook (7th Edition):

Nelson, Erik Walter. “Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication.” 2008. Web. 11 Apr 2021.

Vancouver:

Nelson EW. Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication. [Internet] [Masters thesis]. Virginia Tech; 2008. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10919/43583.

Council of Science Editors:

Nelson EW. Combined Compression and Shear Structural Evaluation of Stiffened Panels Fabricated Using Electron Beam Freeform Fabrication. [Masters Thesis]. Virginia Tech; 2008. Available from: http://hdl.handle.net/10919/43583


Indian Institute of Science

12. Palani, G S. Numerically Integrated MVCCI Technique For Fracture Analysis Of Plates And Stiffened Panels.

Degree: PhD, Faculty of Engineering, 2011, Indian Institute of Science

Subjects/Keywords: Plates - Fracture Analysis; Fracture Mechanics; Numerical Analysis; NI-MVCCI Technique; Plates Panels; Cracked Plates; Stiffened Panels; Structural Engineering

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APA (6th Edition):

Palani, G. S. (2011). Numerically Integrated MVCCI Technique For Fracture Analysis Of Plates And Stiffened Panels. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1130

Chicago Manual of Style (16th Edition):

Palani, G S. “Numerically Integrated MVCCI Technique For Fracture Analysis Of Plates And Stiffened Panels.” 2011. Doctoral Dissertation, Indian Institute of Science. Accessed April 11, 2021. http://etd.iisc.ac.in/handle/2005/1130.

MLA Handbook (7th Edition):

Palani, G S. “Numerically Integrated MVCCI Technique For Fracture Analysis Of Plates And Stiffened Panels.” 2011. Web. 11 Apr 2021.

Vancouver:

Palani GS. Numerically Integrated MVCCI Technique For Fracture Analysis Of Plates And Stiffened Panels. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2011. [cited 2021 Apr 11]. Available from: http://etd.iisc.ac.in/handle/2005/1130.

Council of Science Editors:

Palani GS. Numerically Integrated MVCCI Technique For Fracture Analysis Of Plates And Stiffened Panels. [Doctoral Dissertation]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1130

13. Σταματέλος, Δημήτριος. Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών.

Degree: 2010, University of Patras

 O σχεδιασμός και η ανάπτυξη μιας σύγχρονης αεροναυπηγικής κατασκευής περιλαμβάνει ως επιμέρους φάσεις (μεταξύ άλλων) τον αρχικό και τον προκαταρκτικό σχεδιασμό. Οι φάσεις αυτές έχουν… (more)

Subjects/Keywords: Προκαταρκτικός σχεδιασμός; Πτέρυγες από σύνθετα υλικά; Πολυάριθμες κύριες δοκοί; Λυγισμός πλακών με δοκούς ενίσχυσης; Ανάλυση τάσεων; Πεπερασμένα στοιχεία; 629.12; Preliminary design; Composite wing; Multispar wing; Buckling of stiffened panels; Stress analysis; Finite element analysis

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APA (6th Edition):

Σταματέλος, . (2010). Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών. (Doctoral Dissertation). University of Patras. Retrieved from http://nemertes.lis.upatras.gr/jspui/handle/10889/4301

Chicago Manual of Style (16th Edition):

Σταματέλος, Δημήτριος. “Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών.” 2010. Doctoral Dissertation, University of Patras. Accessed April 11, 2021. http://nemertes.lis.upatras.gr/jspui/handle/10889/4301.

MLA Handbook (7th Edition):

Σταματέλος, Δημήτριος. “Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών.” 2010. Web. 11 Apr 2021.

Vancouver:

Σταματέλος . Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών. [Internet] [Doctoral dissertation]. University of Patras; 2010. [cited 2021 Apr 11]. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/4301.

Council of Science Editors:

Σταματέλος . Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών. [Doctoral Dissertation]. University of Patras; 2010. Available from: http://nemertes.lis.upatras.gr/jspui/handle/10889/4301


Universitat de Girona

14. Badalló i Cañellas, Pere. Analysis and optimization of composite stringers.

Degree: Departament d'Enginyeria Mecànica i de la Construcció Industrial, 2015, Universitat de Girona

 L'ús de panells rigiditzats a la indústria aeronàutica i aeroespacial ha anat creixent les darreres dècades. Per altra banda, el creixement exponencial de l'ús dels… (more)

Subjects/Keywords: Panells rigiditzats; Stiffened panels; Paneles rigidizados; Materials compòsits; Composite materials; Materiales compuestos; Metamodelatge; Metamodeling; Metamodelado; Mètode dels elements finits; Finite element method; Método de los elementos finitos; Assaig virtual; Virtual test; Ensayo virtual; Aircraft industry; Industria aeronautica; Indústries aeroespacials; Aerospace industries; Indústrias aeroespaciales; 620; 629

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APA (6th Edition):

Badalló i Cañellas, P. (2015). Analysis and optimization of composite stringers. (Thesis). Universitat de Girona. Retrieved from http://hdl.handle.net/10803/323087

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):

Badalló i Cañellas, Pere. “Analysis and optimization of composite stringers.” 2015. Thesis, Universitat de Girona. Accessed April 11, 2021. http://hdl.handle.net/10803/323087.

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

MLA Handbook (7th Edition):

Badalló i Cañellas, Pere. “Analysis and optimization of composite stringers.” 2015. Web. 11 Apr 2021.

Vancouver:

Badalló i Cañellas P. Analysis and optimization of composite stringers. [Internet] [Thesis]. Universitat de Girona; 2015. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10803/323087.

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

Council of Science Editors:

Badalló i Cañellas P. Analysis and optimization of composite stringers. [Thesis]. Universitat de Girona; 2015. Available from: http://hdl.handle.net/10803/323087

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


Virginia Tech

15. Islam, Mohammad Majharul. Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints.

Degree: PhD, Engineering Science and Mechanics, 2012, Virginia Tech

 Global-local finite element analyses were used to study the damage tolerance of curvilinearly stiffened panels; fabricated using the modern additive manufacturing process, the so-called unitized… (more)

Subjects/Keywords: buckling analysis; curvilinearly stiffened panels; stress intensity factors; adhesive lap joints; J-integral; VCCT; fracture mechanics; compression-shear test-fixture; nonlinear finite element analysis; global-local finite element analysis; cohesive zone finite element analysis; asymmetric double cantilever beam; three-point bending test

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

APA (6th Edition):

Islam, M. M. (2012). Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/38687

Chicago Manual of Style (16th Edition):

Islam, Mohammad Majharul. “Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints.” 2012. Doctoral Dissertation, Virginia Tech. Accessed April 11, 2021. http://hdl.handle.net/10919/38687.

MLA Handbook (7th Edition):

Islam, Mohammad Majharul. “Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints.” 2012. Web. 11 Apr 2021.

Vancouver:

Islam MM. Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10919/38687.

Council of Science Editors:

Islam MM. Global-local Finite Element Fracture Analysis of Curvilinearly Stiffened Panels and Adhesive Joints. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/38687

16. Σταματέλος, Δημήτριος. Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών.

Degree: 2010, University of Patras; Πανεπιστήμιο Πατρών

 The design and development of a modern aerospace structure consists of many design stages. The most important stages are the conceptual and the preliminary where… (more)

Subjects/Keywords: Πτέρυγα από σύνθετα υλικά; Πολυάριθμες κύριες δοκούς; Ανάλυση τάσεων; Λυγισμός πλακών με ενισχυτικές δοκούς; Πεπερασμένα στοιχεία; Προκαταρκτικός σχεδιασμός; Μεθοδολογία διαστασιολόγησης; Composite wing; Multispar wing; Stress analysis; Buckling of stiffened panels; Conceptual design; Sizing methodology

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Σταματέλος, . . (2010). Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών. (Thesis). University of Patras; Πανεπιστήμιο Πατρών. Retrieved from http://hdl.handle.net/10442/hedi/28015

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):

Σταματέλος, Δημήτριος. “Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών.” 2010. Thesis, University of Patras; Πανεπιστήμιο Πατρών. Accessed April 11, 2021. http://hdl.handle.net/10442/hedi/28015.

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

MLA Handbook (7th Edition):

Σταματέλος, Δημήτριος. “Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών.” 2010. Web. 11 Apr 2021.

Vancouver:

Σταματέλος . Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών. [Internet] [Thesis]. University of Patras; Πανεπιστήμιο Πατρών; 2010. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/10442/hedi/28015.

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

Council of Science Editors:

Σταματέλος . Μεθοδολογία ανάλυσης και προκαταρκτικού σχεδιασμού μη-συμβατικών αεροναυπηγικών δομών. [Thesis]. University of Patras; Πανεπιστήμιο Πατρών; 2010. Available from: http://hdl.handle.net/10442/hedi/28015

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

.