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You searched for subject:(wing structure). Showing records 1 – 29 of 29 total matches.

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Delft University of Technology

1. Riahi, G. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.

Degree: 2012, Delft University of Technology

 Joined Wing is a concept of nonplanar airplane wing structure. This is a new concept which is not yet used for commercial airplanes but has… (more)

Subjects/Keywords: nonlinear; finite; wing structure

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APA (6th Edition):

Riahi, G. (2012). Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164

Chicago Manual of Style (16th Edition):

Riahi, G. “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.” 2012. Masters Thesis, Delft University of Technology. Accessed April 01, 2020. http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

MLA Handbook (7th Edition):

Riahi, G. “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.” 2012. Web. 01 Apr 2020.

Vancouver:

Riahi G. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2020 Apr 01]. Available from: http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

Council of Science Editors:

Riahi G. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164


Cranfield University

2. Mohd Saleh, Siti Juita Mastura. Modelling and analysis of thin-walled structures for optimal design of composite wing.

Degree: PhD, 2017, Cranfield University

 At present, the option for composite usage in aircraft components and the associated manufacturing process is largely based on experience, knowledge, benchmarking, and partly market… (more)

Subjects/Keywords: Composite structure; aircraft wing structure; optimal wing design; knowledge-based; optimisation tool

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APA (6th Edition):

Mohd Saleh, S. J. M. (2017). Modelling and analysis of thin-walled structures for optimal design of composite wing. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/14308 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783253

Chicago Manual of Style (16th Edition):

Mohd Saleh, Siti Juita Mastura. “Modelling and analysis of thin-walled structures for optimal design of composite wing.” 2017. Doctoral Dissertation, Cranfield University. Accessed April 01, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/14308 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783253.

MLA Handbook (7th Edition):

Mohd Saleh, Siti Juita Mastura. “Modelling and analysis of thin-walled structures for optimal design of composite wing.” 2017. Web. 01 Apr 2020.

Vancouver:

Mohd Saleh SJM. Modelling and analysis of thin-walled structures for optimal design of composite wing. [Internet] [Doctoral dissertation]. Cranfield University; 2017. [cited 2020 Apr 01]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14308 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783253.

Council of Science Editors:

Mohd Saleh SJM. Modelling and analysis of thin-walled structures for optimal design of composite wing. [Doctoral Dissertation]. Cranfield University; 2017. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14308 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783253


Texas A&M University

3. Cha, Gene. Structural Locking in a Nastic Actuated Shaped-Changing Beam.

Degree: 2010, Texas A&M University

 This thesis endeavors to develop a new locking method for a twisted morphing wing spar. The conventional wing has to have hinges and a discontinuous… (more)

Subjects/Keywords: Nastic material; Shaped changing structure; Morphing wing; Structural locking

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APA (6th Edition):

Cha, G. (2010). Structural Locking in a Nastic Actuated Shaped-Changing Beam. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7926

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):

Cha, Gene. “Structural Locking in a Nastic Actuated Shaped-Changing Beam.” 2010. Thesis, Texas A&M University. Accessed April 01, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7926.

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

MLA Handbook (7th Edition):

Cha, Gene. “Structural Locking in a Nastic Actuated Shaped-Changing Beam.” 2010. Web. 01 Apr 2020.

Vancouver:

Cha G. Structural Locking in a Nastic Actuated Shaped-Changing Beam. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7926.

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

Council of Science Editors:

Cha G. Structural Locking in a Nastic Actuated Shaped-Changing Beam. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7926

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

4. Junchangpood, Aphaiwong. Study on Prediction of Thrust Force on Wing with Elastic Deformation Effects : 翅の弾性変形の影響による推進力の予測に関する研究.

Degree: 博士(情報工学), 2017, Kyushu Institute of Technology / 九州工業大学

 In this thesis, the simple predicting method of thrust-production on the wing’s elastic deformation effects has been proposed, which is named DRR’s principle. And then,… (more)

Subjects/Keywords: Flapping wing; Elastic deformation; Thrust force; Fluid Structure Interaction; DRR’s principle

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APA (6th Edition):

Junchangpood, A. (2017). Study on Prediction of Thrust Force on Wing with Elastic Deformation Effects : 翅の弾性変形の影響による推進力の予測に関する研究. (Thesis). Kyushu Institute of Technology / 九州工業大学. Retrieved from http://hdl.handle.net/10228/4950

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):

Junchangpood, Aphaiwong. “Study on Prediction of Thrust Force on Wing with Elastic Deformation Effects : 翅の弾性変形の影響による推進力の予測に関する研究.” 2017. Thesis, Kyushu Institute of Technology / 九州工業大学. Accessed April 01, 2020. http://hdl.handle.net/10228/4950.

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

MLA Handbook (7th Edition):

Junchangpood, Aphaiwong. “Study on Prediction of Thrust Force on Wing with Elastic Deformation Effects : 翅の弾性変形の影響による推進力の予測に関する研究.” 2017. Web. 01 Apr 2020.

Vancouver:

Junchangpood A. Study on Prediction of Thrust Force on Wing with Elastic Deformation Effects : 翅の弾性変形の影響による推進力の予測に関する研究. [Internet] [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/10228/4950.

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

Council of Science Editors:

Junchangpood A. Study on Prediction of Thrust Force on Wing with Elastic Deformation Effects : 翅の弾性変形の影響による推進力の予測に関する研究. [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. Available from: http://hdl.handle.net/10228/4950

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


Cranfield University

5. Cheng, Yun. Preliminary fuselage structural configuration of a flying-wing type airline.

Degree: MSc by Research, 2012, Cranfield University

 The flying-wing is a type of configuration which is a tailless airplane accommodating all of its parts within the outline of a single airfoil. Theoretically,… (more)

Subjects/Keywords: Preliminary design; Flying-wing; multi-bubble; structure initial design; AVIC program

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APA (6th Edition):

Cheng, Y. (2012). Preliminary fuselage structural configuration of a flying-wing type airline. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7419

Chicago Manual of Style (16th Edition):

Cheng, Yun. “Preliminary fuselage structural configuration of a flying-wing type airline.” 2012. Masters Thesis, Cranfield University. Accessed April 01, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/7419.

MLA Handbook (7th Edition):

Cheng, Yun. “Preliminary fuselage structural configuration of a flying-wing type airline.” 2012. Web. 01 Apr 2020.

Vancouver:

Cheng Y. Preliminary fuselage structural configuration of a flying-wing type airline. [Internet] [Masters thesis]. Cranfield University; 2012. [cited 2020 Apr 01]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7419.

Council of Science Editors:

Cheng Y. Preliminary fuselage structural configuration of a flying-wing type airline. [Masters Thesis]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7419


University of New South Wales

6. Tobing, Sheila. Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies.

Degree: Engineering & Information Technology, 2014, University of New South Wales

 A critical review of the progress of research on the effects of aerodynamics/kinematics and aeroelasticity on flapping-wing propulsion reveals the complexity of the subject. As… (more)

Subjects/Keywords: fluid structure interactions; flapping wing; insect flight; computational fluid dynamics; aerodynamics

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APA (6th Edition):

Tobing, S. (2014). Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/53832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12545/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Tobing, Sheila. “Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies.” 2014. Doctoral Dissertation, University of New South Wales. Accessed April 01, 2020. http://handle.unsw.edu.au/1959.4/53832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12545/SOURCE01?view=true.

MLA Handbook (7th Edition):

Tobing, Sheila. “Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies.” 2014. Web. 01 Apr 2020.

Vancouver:

Tobing S. Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies. [Internet] [Doctoral dissertation]. University of New South Wales; 2014. [cited 2020 Apr 01]. Available from: http://handle.unsw.edu.au/1959.4/53832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12545/SOURCE01?view=true.

Council of Science Editors:

Tobing S. Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies. [Doctoral Dissertation]. University of New South Wales; 2014. Available from: http://handle.unsw.edu.au/1959.4/53832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12545/SOURCE01?view=true


Brno University of Technology

7. Kaňák, Ondřej. Konstrukce křídla .

Degree: 2010, Brno University of Technology

 Tato bakalářská práce pojednává o konstrukci křídel malých letounů. Postupně se seznamujeme s rozličnými typy konstrukcí, jejich možností využití v leteckém průmyslu. Sledujeme charakteristické znaky… (more)

Subjects/Keywords: Křídlo; konstrukce; letoun; kompozit; Wing; structure; aeroplane; composite

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APA (6th Edition):

Kaňák, O. (2010). Konstrukce křídla . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1706

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):

Kaňák, Ondřej. “Konstrukce křídla .” 2010. Thesis, Brno University of Technology. Accessed April 01, 2020. http://hdl.handle.net/11012/1706.

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

MLA Handbook (7th Edition):

Kaňák, Ondřej. “Konstrukce křídla .” 2010. Web. 01 Apr 2020.

Vancouver:

Kaňák O. Konstrukce křídla . [Internet] [Thesis]. Brno University of Technology; 2010. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/11012/1706.

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

Council of Science Editors:

Kaňák O. Konstrukce křídla . [Thesis]. Brno University of Technology; 2010. Available from: http://hdl.handle.net/11012/1706

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


Delft University of Technology

8. Van Der Wurff, S. Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes:.

Degree: 2015, Delft University of Technology

 This work focuses on a multidisciplinary design optimization of an aircraft wing. Among others, a structural optimization of the wing stiffness is performed. For a… (more)

Subjects/Keywords: aircraft; optimization; flight dynamics; wing; stiffness; flexibility; loads; structure; loads envelope; load cases

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APA (6th Edition):

Van Der Wurff, S. (2015). Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:41e4de26-825c-493e-b89a-1e460969bd30

Chicago Manual of Style (16th Edition):

Van Der Wurff, S. “Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes:.” 2015. Masters Thesis, Delft University of Technology. Accessed April 01, 2020. http://resolver.tudelft.nl/uuid:41e4de26-825c-493e-b89a-1e460969bd30.

MLA Handbook (7th Edition):

Van Der Wurff, S. “Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes:.” 2015. Web. 01 Apr 2020.

Vancouver:

Van Der Wurff S. Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Apr 01]. Available from: http://resolver.tudelft.nl/uuid:41e4de26-825c-493e-b89a-1e460969bd30.

Council of Science Editors:

Van Der Wurff S. Changes of the Loads Envelope for Wing Stiffness Modifications, In the Frame of Multidisciplinary Design Optimization Purposes:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:41e4de26-825c-493e-b89a-1e460969bd30


Brno University of Technology

9. Mahdal, Vít. Konstrukční uspořádání křídla soutěžního letounu .

Degree: 2016, Brno University of Technology

 Tato bakalářská práce se zabývá konstrukčním uspořádáním křídla soutěžního letounu. Práce se skládá z pěti hlavních částí. První část popisuje soutěž Air Cargo Challenge, pro… (more)

Subjects/Keywords: Letoun; soutěž; křídlo; zatížení; nosník; konstrukce.; Aircraft; competition; wing; load; beam; structure.

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APA (6th Edition):

Mahdal, V. (2016). Konstrukční uspořádání křídla soutěžního letounu . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/61072

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):

Mahdal, Vít. “Konstrukční uspořádání křídla soutěžního letounu .” 2016. Thesis, Brno University of Technology. Accessed April 01, 2020. http://hdl.handle.net/11012/61072.

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

MLA Handbook (7th Edition):

Mahdal, Vít. “Konstrukční uspořádání křídla soutěžního letounu .” 2016. Web. 01 Apr 2020.

Vancouver:

Mahdal V. Konstrukční uspořádání křídla soutěžního letounu . [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/11012/61072.

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

Council of Science Editors:

Mahdal V. Konstrukční uspořádání křídla soutěžního letounu . [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/61072

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


Arizona State University

10. Miskin, Daniel L. Early Wing Structural Design for Stiffness and Frequency Response.

Degree: Aerospace Engineering, 2018, Arizona State University

 This paper describes an effort to bring wing structural stiffness and aeroelastic considerations early in the conceptual design process with an automated tool. Stiffness and… (more)

Subjects/Keywords: Aerospace engineering; Engineering; Mechanical engineering; Design; Frequency; Stiffness; Structure; Torque-Box; Wing

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APA (6th Edition):

Miskin, D. L. (2018). Early Wing Structural Design for Stiffness and Frequency Response. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/51702

Chicago Manual of Style (16th Edition):

Miskin, Daniel L. “Early Wing Structural Design for Stiffness and Frequency Response.” 2018. Masters Thesis, Arizona State University. Accessed April 01, 2020. http://repository.asu.edu/items/51702.

MLA Handbook (7th Edition):

Miskin, Daniel L. “Early Wing Structural Design for Stiffness and Frequency Response.” 2018. Web. 01 Apr 2020.

Vancouver:

Miskin DL. Early Wing Structural Design for Stiffness and Frequency Response. [Internet] [Masters thesis]. Arizona State University; 2018. [cited 2020 Apr 01]. Available from: http://repository.asu.edu/items/51702.

Council of Science Editors:

Miskin DL. Early Wing Structural Design for Stiffness and Frequency Response. [Masters Thesis]. Arizona State University; 2018. Available from: http://repository.asu.edu/items/51702


University of Dayton

11. Puttmann, John Paul. Spatially Targeted Activation of a SMP.

Degree: MS(M.S.), Aerospace Engineering, 2018, University of Dayton

 The purpose of the research is to identify the mechanical properties of a skin, an infilled honeycomb, for morphing aircraft and investigate ways to optimize… (more)

Subjects/Keywords: Aerospace Engineering; SMP; Morphing Skin; adaptive structure; honeycomb; morphing wing; morphing skin; composite skin; aerospace structures; monolithic skin

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APA (6th Edition):

Puttmann, J. P. (2018). Spatially Targeted Activation of a SMP. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011

Chicago Manual of Style (16th Edition):

Puttmann, John Paul. “Spatially Targeted Activation of a SMP.” 2018. Masters Thesis, University of Dayton. Accessed April 01, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011.

MLA Handbook (7th Edition):

Puttmann, John Paul. “Spatially Targeted Activation of a SMP.” 2018. Web. 01 Apr 2020.

Vancouver:

Puttmann JP. Spatially Targeted Activation of a SMP. [Internet] [Masters thesis]. University of Dayton; 2018. [cited 2020 Apr 01]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011.

Council of Science Editors:

Puttmann JP. Spatially Targeted Activation of a SMP. [Masters Thesis]. University of Dayton; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1525166147319011


Universidade do Rio Grande do Sul

12. Bordin, Franciele Stail. Análise do efeito da interação fluido-estrutura nas forças fluidodinâmicas em um elemento de pá flexível 3D.

Degree: 2014, Universidade do Rio Grande do Sul

Elementos de materiais flexíveis são empregados em diversas aplicações na engenharia, como por exemplo, em pás de turbinas eólicas. O comportamento do escoamento é afetado… (more)

Subjects/Keywords: Fluid-structure interaction (FSI); Turbinas eólicas; Simulação numérica; Flexible blade; Interação fluido-estrutura; Finite wing; Escoamento turbulento; Fluid-dynamic forces

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APA (6th Edition):

Bordin, F. S. (2014). Análise do efeito da interação fluido-estrutura nas forças fluidodinâmicas em um elemento de pá flexível 3D. (Thesis). Universidade do Rio Grande do Sul. Retrieved from http://hdl.handle.net/10183/108499

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):

Bordin, Franciele Stail. “Análise do efeito da interação fluido-estrutura nas forças fluidodinâmicas em um elemento de pá flexível 3D.” 2014. Thesis, Universidade do Rio Grande do Sul. Accessed April 01, 2020. http://hdl.handle.net/10183/108499.

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

MLA Handbook (7th Edition):

Bordin, Franciele Stail. “Análise do efeito da interação fluido-estrutura nas forças fluidodinâmicas em um elemento de pá flexível 3D.” 2014. Web. 01 Apr 2020.

Vancouver:

Bordin FS. Análise do efeito da interação fluido-estrutura nas forças fluidodinâmicas em um elemento de pá flexível 3D. [Internet] [Thesis]. Universidade do Rio Grande do Sul; 2014. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/10183/108499.

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

Council of Science Editors:

Bordin FS. Análise do efeito da interação fluido-estrutura nas forças fluidodinâmicas em um elemento de pá flexível 3D. [Thesis]. Universidade do Rio Grande do Sul; 2014. Available from: http://hdl.handle.net/10183/108499

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

13. Simsek, Mehmet R. A Hybrid Position Feedback Controller for Bistable Structures.

Degree: MS, Mechanical & Aerospace Engineering, 2016, Old Dominion University

  Bistability is the property of structures showing the ability to attain two statically stable states. Due to dynamic and static advantages such as no… (more)

Subjects/Keywords: Bistable structure; Hybrid feedback control; Morphing wing; Piezoletric actuation; Smart systems; Snap-through; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Simsek, M. R. (2016). A Hybrid Position Feedback Controller for Bistable Structures. (Thesis). Old Dominion University. Retrieved from 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5

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):

Simsek, Mehmet R. “A Hybrid Position Feedback Controller for Bistable Structures.” 2016. Thesis, Old Dominion University. Accessed April 01, 2020. 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5.

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

MLA Handbook (7th Edition):

Simsek, Mehmet R. “A Hybrid Position Feedback Controller for Bistable Structures.” 2016. Web. 01 Apr 2020.

Vancouver:

Simsek MR. A Hybrid Position Feedback Controller for Bistable Structures. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2020 Apr 01]. Available from: 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5.

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

Council of Science Editors:

Simsek MR. A Hybrid Position Feedback Controller for Bistable Structures. [Thesis]. Old Dominion University; 2016. Available from: 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5

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

14. ZHANG XIAOHU. AERODYNAMICS OF TWO-DIMENSIONAL FLAPPING WING(S).

Degree: 2013, National University of Singapore

Subjects/Keywords: flapping wing; unsteady aerodynamics; flow structure; PIV

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APA (6th Edition):

XIAOHU, Z. (2013). AERODYNAMICS OF TWO-DIMENSIONAL FLAPPING WING(S). (Thesis). National University of Singapore. Retrieved from http://scholarbank.nus.edu.sg/handle/10635/49391

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):

XIAOHU, ZHANG. “AERODYNAMICS OF TWO-DIMENSIONAL FLAPPING WING(S).” 2013. Thesis, National University of Singapore. Accessed April 01, 2020. http://scholarbank.nus.edu.sg/handle/10635/49391.

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

MLA Handbook (7th Edition):

XIAOHU, ZHANG. “AERODYNAMICS OF TWO-DIMENSIONAL FLAPPING WING(S).” 2013. Web. 01 Apr 2020.

Vancouver:

XIAOHU Z. AERODYNAMICS OF TWO-DIMENSIONAL FLAPPING WING(S). [Internet] [Thesis]. National University of Singapore; 2013. [cited 2020 Apr 01]. Available from: http://scholarbank.nus.edu.sg/handle/10635/49391.

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

Council of Science Editors:

XIAOHU Z. AERODYNAMICS OF TWO-DIMENSIONAL FLAPPING WING(S). [Thesis]. National University of Singapore; 2013. Available from: http://scholarbank.nus.edu.sg/handle/10635/49391

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


Brno University of Technology

15. Rybka, Slavomír. Návrh konstrukce křídla čtyřmístného jednomotorového letounu .

Degree: 2014, Brno University of Technology

 Obsahom diplomovej práce je oboznámenie sa s lietadlom TL4000 a technickými parametrami krídla. Práca zahŕňa výpočet letových obálok podľa predpisu CS 23 v troch hmotnostných… (more)

Subjects/Keywords: Krídlo; zaťaženie; statická skúška; maximálny ohyb; maximálny krut; kompozitová konštrukcia; Wing; loading; static test; the maximum bending; maximum torque; composite structure

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APA (6th Edition):

Rybka, S. (2014). Návrh konstrukce křídla čtyřmístného jednomotorového letounu . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/34035

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):

Rybka, Slavomír. “Návrh konstrukce křídla čtyřmístného jednomotorového letounu .” 2014. Thesis, Brno University of Technology. Accessed April 01, 2020. http://hdl.handle.net/11012/34035.

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

MLA Handbook (7th Edition):

Rybka, Slavomír. “Návrh konstrukce křídla čtyřmístného jednomotorového letounu .” 2014. Web. 01 Apr 2020.

Vancouver:

Rybka S. Návrh konstrukce křídla čtyřmístného jednomotorového letounu . [Internet] [Thesis]. Brno University of Technology; 2014. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/11012/34035.

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

Council of Science Editors:

Rybka S. Návrh konstrukce křídla čtyřmístného jednomotorového letounu . [Thesis]. Brno University of Technology; 2014. Available from: http://hdl.handle.net/11012/34035

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


Virginia Tech

16. Papadales, Basil S. An experimental investigation of oblique wing static aeroelastic phenomena.

Degree: MS, Aerospace and Ocean Engineering, 1975, Virginia Tech

 A series of wind tunnel tests were conducted to determine the aerodynamic forces and moments produced by several clamped oblique wings. The wing sweep and… (more)

Subjects/Keywords: aileron deflection; wing structure; LD5655.V855 1975.P36

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APA (6th Edition):

Papadales, B. S. (1975). An experimental investigation of oblique wing static aeroelastic phenomena. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/42938

Chicago Manual of Style (16th Edition):

Papadales, Basil S. “An experimental investigation of oblique wing static aeroelastic phenomena.” 1975. Masters Thesis, Virginia Tech. Accessed April 01, 2020. http://hdl.handle.net/10919/42938.

MLA Handbook (7th Edition):

Papadales, Basil S. “An experimental investigation of oblique wing static aeroelastic phenomena.” 1975. Web. 01 Apr 2020.

Vancouver:

Papadales BS. An experimental investigation of oblique wing static aeroelastic phenomena. [Internet] [Masters thesis]. Virginia Tech; 1975. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/10919/42938.

Council of Science Editors:

Papadales BS. An experimental investigation of oblique wing static aeroelastic phenomena. [Masters Thesis]. Virginia Tech; 1975. Available from: http://hdl.handle.net/10919/42938

17. Mohd Saleh, Siti Juita Mastura. Modelling and analysis of thin-walled structures for optimal design of composite wing.

Degree: 2017, Cranfield University

 At present, the option for composite usage in aircraft components and the associated manufacturing process is largely based on experience, knowledge, benchmarking, and partly market… (more)

Subjects/Keywords: Composite structure; aircraft wing structure; optimal wing design; knowledge-based; optimisation tool

…laminate layup is extended to a box structure. 2 5. To create the FE model of a composite wing… …application of a composite wing box in structure design is much more widespread now, compared to… …design of composite wing structure, subject to multi constraint. The tool is called a Knowledge… …6.1 FE model of baseline wing… …Figure 6.3 Composite wing skin thickness distributions (min t=1.46mm, max t=9.15mm)… 

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APA (6th Edition):

Mohd Saleh, S. J. M. (2017). Modelling and analysis of thin-walled structures for optimal design of composite wing. (Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/14308

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):

Mohd Saleh, Siti Juita Mastura. “Modelling and analysis of thin-walled structures for optimal design of composite wing.” 2017. Thesis, Cranfield University. Accessed April 01, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/14308.

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

MLA Handbook (7th Edition):

Mohd Saleh, Siti Juita Mastura. “Modelling and analysis of thin-walled structures for optimal design of composite wing.” 2017. Web. 01 Apr 2020.

Vancouver:

Mohd Saleh SJM. Modelling and analysis of thin-walled structures for optimal design of composite wing. [Internet] [Thesis]. Cranfield University; 2017. [cited 2020 Apr 01]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14308.

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

Council of Science Editors:

Mohd Saleh SJM. Modelling and analysis of thin-walled structures for optimal design of composite wing. [Thesis]. Cranfield University; 2017. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14308

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


University of Florida

18. Timpe, Amory W. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 The inherent challenges associated with low Reynolds number flight have stemmed biologically inspired wing designs incorporating highly flexible membranes. Natural membrane wing flyers demonstrate advantages… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Modeling; Momentum; Near wakes; Pixels; Shear layers; Velocity; Vibration; Vorticity; compliant  – dic  – flexible  – fluid-structure  – fsi  – mav  – membrane  – piv  – reynolds  – wing

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APA (6th Edition):

Timpe, A. W. (2012). Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0044220

Chicago Manual of Style (16th Edition):

Timpe, Amory W. “Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.” 2012. Masters Thesis, University of Florida. Accessed April 01, 2020. http://ufdc.ufl.edu/UFE0044220.

MLA Handbook (7th Edition):

Timpe, Amory W. “Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.” 2012. Web. 01 Apr 2020.

Vancouver:

Timpe AW. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2020 Apr 01]. Available from: http://ufdc.ufl.edu/UFE0044220.

Council of Science Editors:

Timpe AW. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. [Masters Thesis]. University of Florida; 2012. Available from: http://ufdc.ufl.edu/UFE0044220


Virginia Tech

19. Bilgen, Onur. Macro Fiber Composite Actuated Unmanned Air Vehicles: Design, Development, and Testing.

Degree: MS, Mechanical Engineering, 2007, Virginia Tech

 The design and implementation of a morphing unmanned aircraft using smart materials is presented. Articulated lifting surfaces and articulated wing sections actuated by servos are… (more)

Subjects/Keywords: composite materials; unimorph structure; morphing wing; Macro Fiber Composite; micro air vehicles

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APA (6th Edition):

Bilgen, O. (2007). Macro Fiber Composite Actuated Unmanned Air Vehicles: Design, Development, and Testing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33117

Chicago Manual of Style (16th Edition):

Bilgen, Onur. “Macro Fiber Composite Actuated Unmanned Air Vehicles: Design, Development, and Testing.” 2007. Masters Thesis, Virginia Tech. Accessed April 01, 2020. http://hdl.handle.net/10919/33117.

MLA Handbook (7th Edition):

Bilgen, Onur. “Macro Fiber Composite Actuated Unmanned Air Vehicles: Design, Development, and Testing.” 2007. Web. 01 Apr 2020.

Vancouver:

Bilgen O. Macro Fiber Composite Actuated Unmanned Air Vehicles: Design, Development, and Testing. [Internet] [Masters thesis]. Virginia Tech; 2007. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/10919/33117.

Council of Science Editors:

Bilgen O. Macro Fiber Composite Actuated Unmanned Air Vehicles: Design, Development, and Testing. [Masters Thesis]. Virginia Tech; 2007. Available from: http://hdl.handle.net/10919/33117


Brno University of Technology

20. Navrátil, Jan. New Approaches in Numerical Aeroelasticity Applied in Aerodynamic Optimization of Elastic Wing .

Degree: 2016, Brno University of Technology

 Aeroelasticita je nezbytná vědní disciplína zahrnuta do návrhu letounů. Zaměřuje se na předpovídání jevů, které vznikají vlivem interakce aerodynamických, elastických a setrvačných sil. Tyto jevy… (more)

Subjects/Keywords: aeroelasticita; výpočetní; statický; podobná konstrukce; aerodynamika; optimalizace; elastický; křídlo; třepetní; flutter; transonický; aeroelasticity; computational; static; equivalent structure; aerodynamics; optimization; elastic; wing; flutter; transonic

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APA (6th Edition):

Navrátil, J. (2016). New Approaches in Numerical Aeroelasticity Applied in Aerodynamic Optimization of Elastic Wing . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/63311

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):

Navrátil, Jan. “New Approaches in Numerical Aeroelasticity Applied in Aerodynamic Optimization of Elastic Wing .” 2016. Thesis, Brno University of Technology. Accessed April 01, 2020. http://hdl.handle.net/11012/63311.

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

MLA Handbook (7th Edition):

Navrátil, Jan. “New Approaches in Numerical Aeroelasticity Applied in Aerodynamic Optimization of Elastic Wing .” 2016. Web. 01 Apr 2020.

Vancouver:

Navrátil J. New Approaches in Numerical Aeroelasticity Applied in Aerodynamic Optimization of Elastic Wing . [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/11012/63311.

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

Council of Science Editors:

Navrátil J. New Approaches in Numerical Aeroelasticity Applied in Aerodynamic Optimization of Elastic Wing . [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/63311

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

21. Eisenbeis, Brian Joseph. Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings.

Degree: 2011, Texas A&M University

 Morphing air vehicles enable more efficient and capable multi-role aircraft by adapting their shape to reach an ideal configuration in an ever-changing environment. Morphing capability… (more)

Subjects/Keywords: morphing; morphing wing; reconfigurable wing; wing; structure; structures; structural; finite element; space frame; Euler-Bernoulli; beam; aerodynamic; aerodynamics; aeroelastic; aeroelasticity; code

…Structural Components . . . . . . . . . . . 72 V Manureva Wing Structure Geometry Parameters… …structure. The model used two wings sections with the extendable wing section constrained to the… …of a morphing wing. Equivalent plate continuum models for the structure were utilized… …structure of the same spanwise bending wing. This reference also discusses the need for a… …structure. By using nonlinear beam analysis in Abaqus, a more accurate representation of the wing… 

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APA (6th Edition):

Eisenbeis, B. J. (2011). Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8373

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):

Eisenbeis, Brian Joseph. “Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings.” 2011. Thesis, Texas A&M University. Accessed April 01, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8373.

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

MLA Handbook (7th Edition):

Eisenbeis, Brian Joseph. “Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings.” 2011. Web. 01 Apr 2020.

Vancouver:

Eisenbeis BJ. Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8373.

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

Council of Science Editors:

Eisenbeis BJ. Structural and Aerodynamic Interaction Computational Tool for Highly Reconfigurable Wings. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8373

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

22. Mistry, Mihir. Quasi-static rotor morphing concepts for rotorcraft performance improvements.

Degree: PhD, Aerospace Engineering, 2012, Penn State University

 The current research is focused on two separate quasi-static rotor morphing concepts: Variable span and variable camber. Both concepts were analyzed from the perspective of… (more)

Subjects/Keywords: rotorcraft; rotor; morphing; smart structure; blade; span; camber; RPM; rotor speed; variation; rotating wing; warping; twist

structure . . . . . . . . . . . . . . . . . . . B.2.1 Region I… …the current model . . . . . . . . . . . . . . B.8.1 Wake structure comparison… …B.9.1.2 Tip vortex helix structure . . . . . . . B.9.1.3 Number of extended near wake… …174 Exploded view of the actuation frame structure . . . . . . . . . . . 174 Detail view of… …View of the completed actuation structure assembly . . . . . . . . . 177 Schematic showing… 

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APA (6th Edition):

Mistry, M. (2012). Quasi-static rotor morphing concepts for rotorcraft performance improvements. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/16272

Chicago Manual of Style (16th Edition):

Mistry, Mihir. “Quasi-static rotor morphing concepts for rotorcraft performance improvements.” 2012. Doctoral Dissertation, Penn State University. Accessed April 01, 2020. https://etda.libraries.psu.edu/catalog/16272.

MLA Handbook (7th Edition):

Mistry, Mihir. “Quasi-static rotor morphing concepts for rotorcraft performance improvements.” 2012. Web. 01 Apr 2020.

Vancouver:

Mistry M. Quasi-static rotor morphing concepts for rotorcraft performance improvements. [Internet] [Doctoral dissertation]. Penn State University; 2012. [cited 2020 Apr 01]. Available from: https://etda.libraries.psu.edu/catalog/16272.

Council of Science Editors:

Mistry M. Quasi-static rotor morphing concepts for rotorcraft performance improvements. [Doctoral Dissertation]. Penn State University; 2012. Available from: https://etda.libraries.psu.edu/catalog/16272


Brno University of Technology

23. Dvouletý, Martin. Muzeum vojenské techniky .

Degree: 2016, Brno University of Technology

 Předmětem bakalářské práce je návrh a posouzení ocelové nosné konstrukce budoucího muzea vojenské techniky. Konstrukce je určena pro muzejní výstavu středně těžké a těžké techniky… (more)

Subjects/Keywords: ocelová nosná konstrukce; sloup; vazník; rám; loď; ocel; muzeum; vojenská technika; náběh; pultová střecha; steel (load bearing) structure; column; girder; frame; wing; steel; museum; military equipment; haunched beam; mono-pitched roof

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APA (6th Edition):

Dvouletý, M. (2016). Muzeum vojenské techniky . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/62634

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):

Dvouletý, Martin. “Muzeum vojenské techniky .” 2016. Thesis, Brno University of Technology. Accessed April 01, 2020. http://hdl.handle.net/11012/62634.

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

MLA Handbook (7th Edition):

Dvouletý, Martin. “Muzeum vojenské techniky .” 2016. Web. 01 Apr 2020.

Vancouver:

Dvouletý M. Muzeum vojenské techniky . [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/11012/62634.

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

Council of Science Editors:

Dvouletý M. Muzeum vojenské techniky . [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/62634

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


Brno University of Technology

24. Pluhař, Tomáš. Návrh repliky letounu L-40 "Meta Sokol" - křídlo .

Degree: 2008, Brno University of Technology

 Tato diplomová práce se zabývá návrhem křídla, křidélka, vztlakové klapky a hlavního podvozku ultralehké repliky letounu L-40 Meta Sokol. Vznikala ve spolupráci s dalšími dvěma… (more)

Subjects/Keywords: Křídlo; křidélko; vztlaková klapka; hlavní podvozek; zatížení; konstrukce.; Wing; aileron; flap; main undercarriage; load; structure.

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APA (6th Edition):

Pluhař, T. (2008). Návrh repliky letounu L-40 "Meta Sokol" - křídlo . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1213

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):

Pluhař, Tomáš. “Návrh repliky letounu L-40 "Meta Sokol" - křídlo .” 2008. Thesis, Brno University of Technology. Accessed April 01, 2020. http://hdl.handle.net/11012/1213.

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

MLA Handbook (7th Edition):

Pluhař, Tomáš. “Návrh repliky letounu L-40 "Meta Sokol" - křídlo .” 2008. Web. 01 Apr 2020.

Vancouver:

Pluhař T. Návrh repliky letounu L-40 "Meta Sokol" - křídlo . [Internet] [Thesis]. Brno University of Technology; 2008. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/11012/1213.

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

Council of Science Editors:

Pluhař T. Návrh repliky letounu L-40 "Meta Sokol" - křídlo . [Thesis]. Brno University of Technology; 2008. Available from: http://hdl.handle.net/11012/1213

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

25. NGUYEN TAN TRONG. COMPUTATIONAL STUDY OF FLEXIBLE FLAPPING WINGS.

Degree: 2014, National University of Singapore

Subjects/Keywords: deformable; insect flight; flapping wing; aerodynamics; flexibility; CFD; computational fluid dynamics; FSI; fluid structure interaction

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APA (6th Edition):

TRONG, N. T. (2014). COMPUTATIONAL STUDY OF FLEXIBLE FLAPPING WINGS. (Thesis). National University of Singapore. Retrieved from http://scholarbank.nus.edu.sg/handle/10635/53800

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):

TRONG, NGUYEN TAN. “COMPUTATIONAL STUDY OF FLEXIBLE FLAPPING WINGS.” 2014. Thesis, National University of Singapore. Accessed April 01, 2020. http://scholarbank.nus.edu.sg/handle/10635/53800.

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

MLA Handbook (7th Edition):

TRONG, NGUYEN TAN. “COMPUTATIONAL STUDY OF FLEXIBLE FLAPPING WINGS.” 2014. Web. 01 Apr 2020.

Vancouver:

TRONG NT. COMPUTATIONAL STUDY OF FLEXIBLE FLAPPING WINGS. [Internet] [Thesis]. National University of Singapore; 2014. [cited 2020 Apr 01]. Available from: http://scholarbank.nus.edu.sg/handle/10635/53800.

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

Council of Science Editors:

TRONG NT. COMPUTATIONAL STUDY OF FLEXIBLE FLAPPING WINGS. [Thesis]. National University of Singapore; 2014. Available from: http://scholarbank.nus.edu.sg/handle/10635/53800

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

26. Francuski Ljubinka. Molekularni i fenotipski diverzitet vrste Eristalis tenax (Diptera, Syrphidae).

Degree: 2012, University of Novi Sad

Sagledavanje ukupnog genetičkog i fenotipskog diverziteta i evolucionog potencijala vrste E. tenax izvršeno je analizom jedinki poreklom sa 42 područja Evrope, Australije, Severne i… (more)

Subjects/Keywords: Eristalis tenax, molekularni diverzitet, fenotipska varijabilnost, inbriding, temporalna varijabilnost, populaciona struktuiranost, polni dimorfizam, alozimska varijabilnost, COI mtDNK, veličina i oblik krila; Eristalis tenax, molecular diversity, phenotypic variability, inbreeding, temporal variability, population structure, sexual dimophism, allozyme, COI mtDNA, wing geometric morphometrics

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APA (6th Edition):

Ljubinka, F. (2012). Molekularni i fenotipski diverzitet vrste Eristalis tenax (Diptera, Syrphidae). (Thesis). University of Novi Sad. Retrieved from https://www.cris.uns.ac.rs/DownloadFileServlet/DisertacijadisertacijaFrancuskiLjubinka.pdf?controlNumber=(BISIS)77084&fileName=disertacijaFrancuskiLjubinka.pdf&id=673&source=OATD&language=en ; https://www.cris.uns.ac.rs/record.jsf?recordId=77084&source=OATD&language=en ; http://dx.doi.org/10.2298/NS20120314FRANCUSKI ; http://vbs.rs/scripts/cobiss?command=SEARCH&base=99999&select=ID=free viagra coupon 2016 interview-questions.sumedh.in pfizer viagra coupons

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):

Ljubinka, Francuski. “Molekularni i fenotipski diverzitet vrste Eristalis tenax (Diptera, Syrphidae).” 2012. Thesis, University of Novi Sad. Accessed April 01, 2020. https://www.cris.uns.ac.rs/DownloadFileServlet/DisertacijadisertacijaFrancuskiLjubinka.pdf?controlNumber=(BISIS)77084&fileName=disertacijaFrancuskiLjubinka.pdf&id=673&source=OATD&language=en ; https://www.cris.uns.ac.rs/record.jsf?recordId=77084&source=OATD&language=en ; http://dx.doi.org/10.2298/NS20120314FRANCUSKI ; http://vbs.rs/scripts/cobiss?command=SEARCH&base=99999&select=ID=free viagra coupon 2016 interview-questions.sumedh.in pfizer viagra coupons.

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

MLA Handbook (7th Edition):

Ljubinka, Francuski. “Molekularni i fenotipski diverzitet vrste Eristalis tenax (Diptera, Syrphidae).” 2012. Web. 01 Apr 2020.

Vancouver:

Ljubinka F. Molekularni i fenotipski diverzitet vrste Eristalis tenax (Diptera, Syrphidae). [Internet] [Thesis]. University of Novi Sad; 2012. [cited 2020 Apr 01]. Available from: https://www.cris.uns.ac.rs/DownloadFileServlet/DisertacijadisertacijaFrancuskiLjubinka.pdf?controlNumber=(BISIS)77084&fileName=disertacijaFrancuskiLjubinka.pdf&id=673&source=OATD&language=en ; https://www.cris.uns.ac.rs/record.jsf?recordId=77084&source=OATD&language=en ; http://dx.doi.org/10.2298/NS20120314FRANCUSKI ; http://vbs.rs/scripts/cobiss?command=SEARCH&base=99999&select=ID=free viagra coupon 2016 interview-questions.sumedh.in pfizer viagra coupons.

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

Council of Science Editors:

Ljubinka F. Molekularni i fenotipski diverzitet vrste Eristalis tenax (Diptera, Syrphidae). [Thesis]. University of Novi Sad; 2012. Available from: https://www.cris.uns.ac.rs/DownloadFileServlet/DisertacijadisertacijaFrancuskiLjubinka.pdf?controlNumber=(BISIS)77084&fileName=disertacijaFrancuskiLjubinka.pdf&id=673&source=OATD&language=en ; https://www.cris.uns.ac.rs/record.jsf?recordId=77084&source=OATD&language=en ; http://dx.doi.org/10.2298/NS20120314FRANCUSKI ; http://vbs.rs/scripts/cobiss?command=SEARCH&base=99999&select=ID=free viagra coupon 2016 interview-questions.sumedh.in pfizer viagra coupons

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


University of Illinois – Urbana-Champaign

27. Koev, Danail. The determinants of ethnic minority party formation and success in Europe.

Degree: PhD, 0343, 2014, University of Illinois – Urbana-Champaign

 Why do some ethnic minority groups in Europe form political parties of their own in order to obtain political representation, whereas others choose to work… (more)

Subjects/Keywords: ethnic politics; ethnic parties; European politics; parties and elections; ethnicity; nationalism; Bulgaria; Eastern Europe; Western Europe; social identity theory; history; European Union; kin state; right-wing populism; political opportunity structure; party organization; clientelism; migrants; minorities

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

APA (6th Edition):

Koev, D. (2014). The determinants of ethnic minority party formation and success in Europe. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/50361

Chicago Manual of Style (16th Edition):

Koev, Danail. “The determinants of ethnic minority party formation and success in Europe.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed April 01, 2020. http://hdl.handle.net/2142/50361.

MLA Handbook (7th Edition):

Koev, Danail. “The determinants of ethnic minority party formation and success in Europe.” 2014. Web. 01 Apr 2020.

Vancouver:

Koev D. The determinants of ethnic minority party formation and success in Europe. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/2142/50361.

Council of Science Editors:

Koev D. The determinants of ethnic minority party formation and success in Europe. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/50361

28. Altememe, Abduljaleel. CM Scale Flapping Wing Of Unmanned Aerial Vehicle At Very Low Reynolds Numbers Regime.

Degree: PhD, Mechanical Engineering, 2019, Clemson University

  This dissertation investigates the CM-SCALE Flapping Wing of Unmanned Aerial Vehicle (FWUAV) that can accommodate nacelles of the scale of current Unmanned Air vehicle… (more)

Subjects/Keywords: Flapping Wing; Fluid Structure Interaction; Laminar Flow; Low Reynolds numbers regimes; RANS Turbulent Flow; Unmanned Air Vehicle

…speed. This structure is later named ornithopter by da Vinci [17]. Within the wing… …1.2 Flapping Wing in History . . . . . . . . . . . . . . . 1.3 Birds Tail… …Modeling and wing generations . . . . . . . . . . . . . . . . . . . . . . . . 2.7 Wing Gear… …Computational Fluid Dynamic Analysis for 2D Flapping Wing of cm-Scale Unmanned Aerial Vehicle at Low… …4.2 FLUID-STRUCTURE INTERACTION . . . . . . . . . . . . . . . . . . . . . . . . . 4.3… 

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

APA (6th Edition):

Altememe, A. (2019). CM Scale Flapping Wing Of Unmanned Aerial Vehicle At Very Low Reynolds Numbers Regime. (Doctoral Dissertation). Clemson University. Retrieved from https://tigerprints.clemson.edu/all_dissertations/2358

Chicago Manual of Style (16th Edition):

Altememe, Abduljaleel. “CM Scale Flapping Wing Of Unmanned Aerial Vehicle At Very Low Reynolds Numbers Regime.” 2019. Doctoral Dissertation, Clemson University. Accessed April 01, 2020. https://tigerprints.clemson.edu/all_dissertations/2358.

MLA Handbook (7th Edition):

Altememe, Abduljaleel. “CM Scale Flapping Wing Of Unmanned Aerial Vehicle At Very Low Reynolds Numbers Regime.” 2019. Web. 01 Apr 2020.

Vancouver:

Altememe A. CM Scale Flapping Wing Of Unmanned Aerial Vehicle At Very Low Reynolds Numbers Regime. [Internet] [Doctoral dissertation]. Clemson University; 2019. [cited 2020 Apr 01]. Available from: https://tigerprints.clemson.edu/all_dissertations/2358.

Council of Science Editors:

Altememe A. CM Scale Flapping Wing Of Unmanned Aerial Vehicle At Very Low Reynolds Numbers Regime. [Doctoral Dissertation]. Clemson University; 2019. Available from: https://tigerprints.clemson.edu/all_dissertations/2358

29. Pontbriand-Paré, Olivier. Influence de la structure du paysage sur les communautés de parasitoïdes de la tordeuse des bourgeons de l’épinette .

Degree: 2017, Université de Montréal

Subjects/Keywords: Aménagement forestier; Échelle spatiale; Épidémies; Forêt boréale; Hétérogénéité; Parasitoïdes; Structure du paysage; Taux de parasitisme; Tordeuse des bourgeons de l’épinette; Boreal forest; Dispersal ability; Forest management; Heterogeneity; Landscape heterogeneity; Landscape structure; Parasitism rates; Parasitoids; Pest outbreaks; Spatial scale; Spruce budworm; Wing load

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

APA (6th Edition):

Pontbriand-Paré, O. (2017). Influence de la structure du paysage sur les communautés de parasitoïdes de la tordeuse des bourgeons de l’épinette . (Thesis). Université de Montréal. Retrieved from http://hdl.handle.net/1866/19556

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):

Pontbriand-Paré, Olivier. “Influence de la structure du paysage sur les communautés de parasitoïdes de la tordeuse des bourgeons de l’épinette .” 2017. Thesis, Université de Montréal. Accessed April 01, 2020. http://hdl.handle.net/1866/19556.

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

MLA Handbook (7th Edition):

Pontbriand-Paré, Olivier. “Influence de la structure du paysage sur les communautés de parasitoïdes de la tordeuse des bourgeons de l’épinette .” 2017. Web. 01 Apr 2020.

Vancouver:

Pontbriand-Paré O. Influence de la structure du paysage sur les communautés de parasitoïdes de la tordeuse des bourgeons de l’épinette . [Internet] [Thesis]. Université de Montréal; 2017. [cited 2020 Apr 01]. Available from: http://hdl.handle.net/1866/19556.

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

Council of Science Editors:

Pontbriand-Paré O. Influence de la structure du paysage sur les communautés de parasitoïdes de la tordeuse des bourgeons de l’épinette . [Thesis]. Université de Montréal; 2017. Available from: http://hdl.handle.net/1866/19556

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

.