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

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Linköping University

1. Sohaib, Muhammad. Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis.

Degree: Machine Design, 2011, Linköping University

  This master thesis work presents the development of a parameterized automated generic model for the structural design of an aircraft wing. Furthermore, in order… (more)

Subjects/Keywords: aircraft design; aircraft wing; wing spars; wing ribs; FEM; structural mesh; generic wing model; parametric wing model; automation; design; TECHNOLOGY; TEKNIKVETENSKAP

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APA (6th Edition):

Sohaib, M. (2011). Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264

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):

Sohaib, Muhammad. “Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis.” 2011. Thesis, Linköping University. Accessed January 25, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264.

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

MLA Handbook (7th Edition):

Sohaib, Muhammad. “Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis.” 2011. Web. 25 Jan 2021.

Vancouver:

Sohaib M. Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis. [Internet] [Thesis]. Linköping University; 2011. [cited 2021 Jan 25]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264.

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

Council of Science Editors:

Sohaib M. Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis. [Thesis]. Linköping University; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264

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


University of Michigan

2. Bons, Nicolas. High-Fidelity Wing Design Exploration with Gradient-Based Optimization.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 Numerical optimization has been applied to wing design problems for over 40 years. Over the decades, the scope and detail of optimization problems have advanced… (more)

Subjects/Keywords: multidisciplinary design optimization; aerostructural optimization; wing design optimization; multimodality in wing design; practical wing design optimization; Aerospace Engineering; Engineering

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APA (6th Edition):

Bons, N. (2020). High-Fidelity Wing Design Exploration with Gradient-Based Optimization. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163242

Chicago Manual of Style (16th Edition):

Bons, Nicolas. “High-Fidelity Wing Design Exploration with Gradient-Based Optimization.” 2020. Doctoral Dissertation, University of Michigan. Accessed January 25, 2021. http://hdl.handle.net/2027.42/163242.

MLA Handbook (7th Edition):

Bons, Nicolas. “High-Fidelity Wing Design Exploration with Gradient-Based Optimization.” 2020. Web. 25 Jan 2021.

Vancouver:

Bons N. High-Fidelity Wing Design Exploration with Gradient-Based Optimization. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2027.42/163242.

Council of Science Editors:

Bons N. High-Fidelity Wing Design Exploration with Gradient-Based Optimization. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163242


Delft University of Technology

3. Sol, M.B. (author). Conceptual Design of Swept Wing Root Aerofoils.

Degree: 2015, Delft University of Technology

 For modern transonic transport aeroplanes, it is important to produce low drag at high cruise speeds. The root effect, caused by effects of symmetry on… (more)

Subjects/Keywords: conceptual; design; swept wing; wing root; aerofoil; straight isobars

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APA (6th Edition):

Sol, M. B. (. (2015). Conceptual Design of Swept Wing Root Aerofoils. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9

Chicago Manual of Style (16th Edition):

Sol, M B (author). “Conceptual Design of Swept Wing Root Aerofoils.” 2015. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9.

MLA Handbook (7th Edition):

Sol, M B (author). “Conceptual Design of Swept Wing Root Aerofoils.” 2015. Web. 25 Jan 2021.

Vancouver:

Sol MB(. Conceptual Design of Swept Wing Root Aerofoils. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9.

Council of Science Editors:

Sol MB(. Conceptual Design of Swept Wing Root Aerofoils. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9


University of Kansas

4. Schueler, Samantha Katelyn. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.

Degree: MS, Aerospace Engineering, 2014, University of Kansas

 In 2008, the commercial aerospace industry saw substantial reductions in aircraft operating hours because of the struggling economy and high operating costs. Recurring fuel costs… (more)

Subjects/Keywords: Aerospace engineering; Adaptive structures; Wing design

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APA (6th Edition):

Schueler, S. K. (2014). A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19593

Chicago Manual of Style (16th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Masters Thesis, University of Kansas. Accessed January 25, 2021. http://hdl.handle.net/1808/19593.

MLA Handbook (7th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Web. 25 Jan 2021.

Vancouver:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1808/19593.

Council of Science Editors:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Masters Thesis]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/19593


Cranfield University

5. 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 January 25, 2021. 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. 25 Jan 2021.

Vancouver:

Mohd Saleh SJM. Modelling and analysis of thin-walled structures for optimal design of composite wing. [Internet] [Doctoral dissertation]. Cranfield University; 2017. [cited 2021 Jan 25]. 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


Virginia Tech

6. Meadows, Nicholas Andrew. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 This study utilizes Multidisciplinary Design Optimization (MDO) techniques to explore the effectiveness of the truss-braced (TBW) and strut-braced (SBW) wing configurations in enhancing the performance… (more)

Subjects/Keywords: Transonic Transport Aircraft; Truss-Braced Wing; Multidisciplinary Design Optimization; Strut-Braced Wing

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APA (6th Edition):

Meadows, N. A. (2011). Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44022

Chicago Manual of Style (16th Edition):

Meadows, Nicholas Andrew. “Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft.” 2011. Masters Thesis, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/44022.

MLA Handbook (7th Edition):

Meadows, Nicholas Andrew. “Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft.” 2011. Web. 25 Jan 2021.

Vancouver:

Meadows NA. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/44022.

Council of Science Editors:

Meadows NA. Multidisciplinary Design Optimization of a Medium Range Transonic Truss-Braced Wing Transport Aircraft. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/44022


University of KwaZulu-Natal

7. Moore, Neall Neville. Lightweight structural design of a UAV wing through the use of coreless composite materials employing novel construction techniques.

Degree: 2017, University of KwaZulu-Natal

 A new structural layout was designed for an existing UAV wing with the aims of lightening the wing by eliminating the use of cored composite… (more)

Subjects/Keywords: Structural design.; Coreless composite materials.; Construction techniques.; Wing design.

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APA (6th Edition):

Moore, N. N. (2017). Lightweight structural design of a UAV wing through the use of coreless composite materials employing novel construction techniques. (Thesis). University of KwaZulu-Natal. Retrieved from https://researchspace.ukzn.ac.za/handle/10413/17298

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):

Moore, Neall Neville. “Lightweight structural design of a UAV wing through the use of coreless composite materials employing novel construction techniques.” 2017. Thesis, University of KwaZulu-Natal. Accessed January 25, 2021. https://researchspace.ukzn.ac.za/handle/10413/17298.

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

MLA Handbook (7th Edition):

Moore, Neall Neville. “Lightweight structural design of a UAV wing through the use of coreless composite materials employing novel construction techniques.” 2017. Web. 25 Jan 2021.

Vancouver:

Moore NN. Lightweight structural design of a UAV wing through the use of coreless composite materials employing novel construction techniques. [Internet] [Thesis]. University of KwaZulu-Natal; 2017. [cited 2021 Jan 25]. Available from: https://researchspace.ukzn.ac.za/handle/10413/17298.

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

Council of Science Editors:

Moore NN. Lightweight structural design of a UAV wing through the use of coreless composite materials employing novel construction techniques. [Thesis]. University of KwaZulu-Natal; 2017. Available from: https://researchspace.ukzn.ac.za/handle/10413/17298

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


Cranfield University

8. 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 January 25, 2021. 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. 25 Jan 2021.

Vancouver:

Cheng Y. Preliminary fuselage structural configuration of a flying-wing type airline. [Internet] [Masters thesis]. Cranfield University; 2012. [cited 2021 Jan 25]. 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


Brno University of Technology

9. Křížová, Barbora. Design plachetnice: Design of Sailing Boat.

Degree: 2019, Brno University of Technology

 The topic of this master‘s thesis is design and analysis of a sailing boat in accordance with ergonomic and technological requirements. The goal is to… (more)

Subjects/Keywords: Plachetnice; loď; plavidlo; jachta; design; křídlo; Sailing boat; sailing ship; vessel; sailing yacht; sail; design; wing; wing-sail

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APA (6th Edition):

Křížová, B. (2019). Design plachetnice: Design of Sailing Boat. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/24730

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):

Křížová, Barbora. “Design plachetnice: Design of Sailing Boat.” 2019. Thesis, Brno University of Technology. Accessed January 25, 2021. http://hdl.handle.net/11012/24730.

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

MLA Handbook (7th Edition):

Křížová, Barbora. “Design plachetnice: Design of Sailing Boat.” 2019. Web. 25 Jan 2021.

Vancouver:

Křížová B. Design plachetnice: Design of Sailing Boat. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11012/24730.

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

Council of Science Editors:

Křížová B. Design plachetnice: Design of Sailing Boat. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/24730

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


Delft University of Technology

10. Elham, A. Weight Indexing for Multidisciplinary Design Optimization of Lifting Surfaces.

Degree: 2013, Delft University of Technology

Subjects/Keywords: wing design; multidisciplinary design optimization; wing weight estimation

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APA (6th Edition):

Elham, A. (2013). Weight Indexing for Multidisciplinary Design Optimization of Lifting Surfaces. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79

Chicago Manual of Style (16th Edition):

Elham, A. “Weight Indexing for Multidisciplinary Design Optimization of Lifting Surfaces.” 2013. Doctoral Dissertation, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79.

MLA Handbook (7th Edition):

Elham, A. “Weight Indexing for Multidisciplinary Design Optimization of Lifting Surfaces.” 2013. Web. 25 Jan 2021.

Vancouver:

Elham A. Weight Indexing for Multidisciplinary Design Optimization of Lifting Surfaces. [Internet] [Doctoral dissertation]. Delft University of Technology; 2013. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79.

Council of Science Editors:

Elham A. Weight Indexing for Multidisciplinary Design Optimization of Lifting Surfaces. [Doctoral Dissertation]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; urn:NBN:nl:ui:24-uuid:253459bb-e20b-4165-b093-81b1a8cf3a79 ; http://resolver.tudelft.nl/uuid:253459bb-e20b-4165-b093-81b1a8cf3a79


Indian Institute of Science

11. Pushpangathan, Jinraj V. Design and Development of 75 mm Fixed-Wing Nano Air Vehicle.

Degree: PhD, Faculty of Engineering, 2018, Indian Institute of Science

 This thesis deals with the design and development of a 75 mm fixed-wing nano-air vehicle (NAV). The NAV is designed to fit inside a cube… (more)

Subjects/Keywords: Nano Air Vehicle (NAV); Flight Control System Design; Fixed Wing Nano Air Vehicle; 75 mm Fixed-Wing Nano Air Vehicle Design; Fixed-Wing Air Vehicle; Aerospace Engineering

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APA (6th Edition):

Pushpangathan, J. V. (2018). Design and Development of 75 mm Fixed-Wing Nano Air Vehicle. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3689

Chicago Manual of Style (16th Edition):

Pushpangathan, Jinraj V. “Design and Development of 75 mm Fixed-Wing Nano Air Vehicle.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed January 25, 2021. http://etd.iisc.ac.in/handle/2005/3689.

MLA Handbook (7th Edition):

Pushpangathan, Jinraj V. “Design and Development of 75 mm Fixed-Wing Nano Air Vehicle.” 2018. Web. 25 Jan 2021.

Vancouver:

Pushpangathan JV. Design and Development of 75 mm Fixed-Wing Nano Air Vehicle. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2021 Jan 25]. Available from: http://etd.iisc.ac.in/handle/2005/3689.

Council of Science Editors:

Pushpangathan JV. Design and Development of 75 mm Fixed-Wing Nano Air Vehicle. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3689


IUPUI

12. Gandhi, Viraj D. Parametric Designs and Weight Optimization using Direct and Indirect Aero-structure Load Transfer Methods.

Degree: 2019, IUPUI

Indiana University-Purdue University Indianapolis (IUPUI)

Within the aerospace design, analysis and optimization community, there is an increasing demand to finalize the preliminary design phase of… (more)

Subjects/Keywords: Multifidelity optimization; Parametric design; Weight optimization of wing

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APA (6th Edition):

Gandhi, V. D. (2019). Parametric Designs and Weight Optimization using Direct and Indirect Aero-structure Load Transfer Methods. (Thesis). IUPUI. Retrieved from http://hdl.handle.net/1805/19941

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):

Gandhi, Viraj D. “Parametric Designs and Weight Optimization using Direct and Indirect Aero-structure Load Transfer Methods.” 2019. Thesis, IUPUI. Accessed January 25, 2021. http://hdl.handle.net/1805/19941.

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

MLA Handbook (7th Edition):

Gandhi, Viraj D. “Parametric Designs and Weight Optimization using Direct and Indirect Aero-structure Load Transfer Methods.” 2019. Web. 25 Jan 2021.

Vancouver:

Gandhi VD. Parametric Designs and Weight Optimization using Direct and Indirect Aero-structure Load Transfer Methods. [Internet] [Thesis]. IUPUI; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1805/19941.

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

Council of Science Editors:

Gandhi VD. Parametric Designs and Weight Optimization using Direct and Indirect Aero-structure Load Transfer Methods. [Thesis]. IUPUI; 2019. Available from: http://hdl.handle.net/1805/19941

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


Penn State University

13. Kambampati, Sandilya. Optimization of Composite Tiltrotor Wings with Extensions and Winglets.

Degree: 2016, Penn State University

 Tiltrotors suffer from an aeroelastic instability during forward flight called whirl flutter. Whirl flutter is caused by the whirling motion of the rotor, characterized by… (more)

Subjects/Keywords: optimization; tiltrotor; winglet; whirl flutter; composite material; wing extensions; aircraft design

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APA (6th Edition):

Kambampati, S. (2016). Optimization of Composite Tiltrotor Wings with Extensions and Winglets. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/ns0646000

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):

Kambampati, Sandilya. “Optimization of Composite Tiltrotor Wings with Extensions and Winglets.” 2016. Thesis, Penn State University. Accessed January 25, 2021. https://submit-etda.libraries.psu.edu/catalog/ns0646000.

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

MLA Handbook (7th Edition):

Kambampati, Sandilya. “Optimization of Composite Tiltrotor Wings with Extensions and Winglets.” 2016. Web. 25 Jan 2021.

Vancouver:

Kambampati S. Optimization of Composite Tiltrotor Wings with Extensions and Winglets. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Jan 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/ns0646000.

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

Council of Science Editors:

Kambampati S. Optimization of Composite Tiltrotor Wings with Extensions and Winglets. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/ns0646000

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


Washington University in St. Louis

14. Hainline, Kevin. Vehicle Design Study of a Straight Flying-Wing with Bell-Shaped Spanload.

Degree: MS, Mechanical Engineering & Materials Science, 2020, Washington University in St. Louis

 Straight flying-wing configurations, that is flying wings with zero quarter-chord sweep, are key to understanding bird flight, have potential performance improvements, and are suitable for… (more)

Subjects/Keywords: Aircraft Design Bell-Shaped Birds Flying Wing; Engineering

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APA (6th Edition):

Hainline, K. (2020). Vehicle Design Study of a Straight Flying-Wing with Bell-Shaped Spanload. (Thesis). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/eng_etds/512

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):

Hainline, Kevin. “Vehicle Design Study of a Straight Flying-Wing with Bell-Shaped Spanload.” 2020. Thesis, Washington University in St. Louis. Accessed January 25, 2021. https://openscholarship.wustl.edu/eng_etds/512.

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

MLA Handbook (7th Edition):

Hainline, Kevin. “Vehicle Design Study of a Straight Flying-Wing with Bell-Shaped Spanload.” 2020. Web. 25 Jan 2021.

Vancouver:

Hainline K. Vehicle Design Study of a Straight Flying-Wing with Bell-Shaped Spanload. [Internet] [Thesis]. Washington University in St. Louis; 2020. [cited 2021 Jan 25]. Available from: https://openscholarship.wustl.edu/eng_etds/512.

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

Council of Science Editors:

Hainline K. Vehicle Design Study of a Straight Flying-Wing with Bell-Shaped Spanload. [Thesis]. Washington University in St. Louis; 2020. Available from: https://openscholarship.wustl.edu/eng_etds/512

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


Delft University of Technology

15. Hendrich, T.J.M. (author). Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy.

Degree: 2011, Delft University of Technology

 Traditionally, the aircraft design process is divided into three phases: conceptual, preliminary and detailed design. In each subsequent phase, the fidelity of the analysis tools… (more)

Subjects/Keywords: MDO; multidisciplinary; BLISS; Blended Wing Body; design; optimization

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APA (6th Edition):

Hendrich, T. J. M. (. (2011). Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d586ee6e-4815-4561-87d9-6ae00bdb739e

Chicago Manual of Style (16th Edition):

Hendrich, T J M (author). “Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy.” 2011. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:d586ee6e-4815-4561-87d9-6ae00bdb739e.

MLA Handbook (7th Edition):

Hendrich, T J M (author). “Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy.” 2011. Web. 25 Jan 2021.

Vancouver:

Hendrich TJM(. Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:d586ee6e-4815-4561-87d9-6ae00bdb739e.

Council of Science Editors:

Hendrich TJM(. Multidisciplinary Design Optimization in the Conceptual Design Phase: Creating a Conceptual Design of the Blended Wing-Body with the BLISS Optimization Strategy. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:d586ee6e-4815-4561-87d9-6ae00bdb739e


Delft University of Technology

16. Zohlandt, C.N. (author). Conceptual Design of High Subsonic Prandtl Planes.

Degree: 2016, Delft University of Technology

The increasing airtraffic demands on aircraft capacity, sustainability and profitability, require the investigation of unconventional aircraft configurations with high aerodynamic efficiency, as the commonly applied… (more)

Subjects/Keywords: Prandtl Plane; box wing; initiator; conceptual aircraft design

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APA (6th Edition):

Zohlandt, C. N. (. (2016). Conceptual Design of High Subsonic Prandtl Planes. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e1f01743-e2eb-4d8b-8b2c-131f50f41a2c

Chicago Manual of Style (16th Edition):

Zohlandt, C N (author). “Conceptual Design of High Subsonic Prandtl Planes.” 2016. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:e1f01743-e2eb-4d8b-8b2c-131f50f41a2c.

MLA Handbook (7th Edition):

Zohlandt, C N (author). “Conceptual Design of High Subsonic Prandtl Planes.” 2016. Web. 25 Jan 2021.

Vancouver:

Zohlandt CN(. Conceptual Design of High Subsonic Prandtl Planes. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:e1f01743-e2eb-4d8b-8b2c-131f50f41a2c.

Council of Science Editors:

Zohlandt CN(. Conceptual Design of High Subsonic Prandtl Planes. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:e1f01743-e2eb-4d8b-8b2c-131f50f41a2c

17. Vanneste, Thomas. Développement d'un outil de modélisation aéroélastique du vol battu de l'insecte appliqué à la conception d'un nano-drone résonant : Aeroelastic framework of insect-like flapping-wing applied to the design of a resonant nano air vehicle.

Degree: Docteur es, Mécanique, 2013, Valenciennes

Développer, à partir de zéro, un drone imitant le vol battu de l'insecte est une tâche ambitieuse et ardue pour un designer en raison du… (more)

Subjects/Keywords: Aile battante; Modèle aéroélastique; Aile souple; Optimisation; Outil de dimensionnement; Flapping-wing; Aeroelastic framework; Flexible wing; Optimization; Design tool

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APA (6th Edition):

Vanneste, T. (2013). Développement d'un outil de modélisation aéroélastique du vol battu de l'insecte appliqué à la conception d'un nano-drone résonant : Aeroelastic framework of insect-like flapping-wing applied to the design of a resonant nano air vehicle. (Doctoral Dissertation). Valenciennes. Retrieved from http://www.theses.fr/2013VALE0021

Chicago Manual of Style (16th Edition):

Vanneste, Thomas. “Développement d'un outil de modélisation aéroélastique du vol battu de l'insecte appliqué à la conception d'un nano-drone résonant : Aeroelastic framework of insect-like flapping-wing applied to the design of a resonant nano air vehicle.” 2013. Doctoral Dissertation, Valenciennes. Accessed January 25, 2021. http://www.theses.fr/2013VALE0021.

MLA Handbook (7th Edition):

Vanneste, Thomas. “Développement d'un outil de modélisation aéroélastique du vol battu de l'insecte appliqué à la conception d'un nano-drone résonant : Aeroelastic framework of insect-like flapping-wing applied to the design of a resonant nano air vehicle.” 2013. Web. 25 Jan 2021.

Vancouver:

Vanneste T. Développement d'un outil de modélisation aéroélastique du vol battu de l'insecte appliqué à la conception d'un nano-drone résonant : Aeroelastic framework of insect-like flapping-wing applied to the design of a resonant nano air vehicle. [Internet] [Doctoral dissertation]. Valenciennes; 2013. [cited 2021 Jan 25]. Available from: http://www.theses.fr/2013VALE0021.

Council of Science Editors:

Vanneste T. Développement d'un outil de modélisation aéroélastique du vol battu de l'insecte appliqué à la conception d'un nano-drone résonant : Aeroelastic framework of insect-like flapping-wing applied to the design of a resonant nano air vehicle. [Doctoral Dissertation]. Valenciennes; 2013. Available from: http://www.theses.fr/2013VALE0021


Delft University of Technology

18. Brown, M.T.H. (author). Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework.

Degree: 2017, Delft University of Technology

 Blended wing body aircraft represent a paradigm shift in jet transport aircraft design. Stepping away from the conventional tube-and-wing philosophy, they promise benefits over existing… (more)

Subjects/Keywords: Blended Wing Body; BWB; Hybrid Wing Body; HWB; conceptual; design; MDO; KBE; unconventional; passenger; aircraft; oval fuselage

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APA (6th Edition):

Brown, M. T. H. (. (2017). Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:6f66cd83-673c-4a20-ae5f-c3ea1b7ce3c3

Chicago Manual of Style (16th Edition):

Brown, M T H (author). “Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework.” 2017. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:6f66cd83-673c-4a20-ae5f-c3ea1b7ce3c3.

MLA Handbook (7th Edition):

Brown, M T H (author). “Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework.” 2017. Web. 25 Jan 2021.

Vancouver:

Brown MTH(. Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:6f66cd83-673c-4a20-ae5f-c3ea1b7ce3c3.

Council of Science Editors:

Brown MTH(. Conceptual Design of Blended Wing Body Airliners Within a Semi-automated Design Framework. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:6f66cd83-673c-4a20-ae5f-c3ea1b7ce3c3


Brno University of Technology

19. Jurda, Martin. Návrh křídla soutěžního letounu: Wing design of competition aircraft.

Degree: 2020, Brno University of Technology

 This bachelor thesis deals with wing design of the new competition aircraft for the SAE Aero Design East 2020 competition. Introduction of the thesis is… (more)

Subjects/Keywords: Návrh krídla; SAE Aero Design East; bodová analýza; koncepčný návrh; letová obálka; zaťaženie krídla; Wing design; SAE Aero Design East; point analysis; conceptual design; flight envelope; wing load

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APA (6th Edition):

Jurda, M. (2020). Návrh křídla soutěžního letounu: Wing design of competition aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/192570

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):

Jurda, Martin. “Návrh křídla soutěžního letounu: Wing design of competition aircraft.” 2020. Thesis, Brno University of Technology. Accessed January 25, 2021. http://hdl.handle.net/11012/192570.

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

MLA Handbook (7th Edition):

Jurda, Martin. “Návrh křídla soutěžního letounu: Wing design of competition aircraft.” 2020. Web. 25 Jan 2021.

Vancouver:

Jurda M. Návrh křídla soutěžního letounu: Wing design of competition aircraft. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11012/192570.

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

Council of Science Editors:

Jurda M. Návrh křídla soutěžního letounu: Wing design of competition aircraft. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/192570

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


Delft University of Technology

20. Schouten, Tom (author). Assessment of Conceptual High-Capacity Regional Turbopropeller Aircraft.

Degree: 2018, Delft University of Technology

Designers are motivated to create more a efficient aircraft design following the growth of the market and environmental restrictions. As a result new interest in… (more)

Subjects/Keywords: aircraft design; Initiator; slipstream; longitudinal stability; longitudinal control; propeller wing interaction; conceptual design; feasibility study

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APA (6th Edition):

Schouten, T. (. (2018). Assessment of Conceptual High-Capacity Regional Turbopropeller Aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:236ad212-eb0b-443d-a40d-602ec6fe64f9

Chicago Manual of Style (16th Edition):

Schouten, Tom (author). “Assessment of Conceptual High-Capacity Regional Turbopropeller Aircraft.” 2018. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:236ad212-eb0b-443d-a40d-602ec6fe64f9.

MLA Handbook (7th Edition):

Schouten, Tom (author). “Assessment of Conceptual High-Capacity Regional Turbopropeller Aircraft.” 2018. Web. 25 Jan 2021.

Vancouver:

Schouten T(. Assessment of Conceptual High-Capacity Regional Turbopropeller Aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:236ad212-eb0b-443d-a40d-602ec6fe64f9.

Council of Science Editors:

Schouten T(. Assessment of Conceptual High-Capacity Regional Turbopropeller Aircraft. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:236ad212-eb0b-443d-a40d-602ec6fe64f9


Virginia Tech

21. Blaesser, Nathaniel James. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft.

Degree: PhD, Aerospace Engineering, 2020, Virginia Tech

 Engine placement on an aircraft is dependent on multiple disciplines. Engine placement affects the noise of the aircraft because the wing can shield or reflect… (more)

Subjects/Keywords: Propulsion-Airframe Integration; Interference Drag; Computational Fluid Dynamics; Transonic Aerodynamics; Wing Design; Aircraft Design

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APA (6th Edition):

Blaesser, N. J. (2020). Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/96446

Chicago Manual of Style (16th Edition):

Blaesser, Nathaniel James. “Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft.” 2020. Doctoral Dissertation, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/96446.

MLA Handbook (7th Edition):

Blaesser, Nathaniel James. “Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft.” 2020. Web. 25 Jan 2021.

Vancouver:

Blaesser NJ. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/96446.

Council of Science Editors:

Blaesser NJ. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/96446


Virginia Tech

22. Locatelli, Davide. Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs.

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

 This dissertation investigates the advantages of using curvilinear spars and ribs, termed SpaRibs, to design supersonic aircraft wing-box in comparison to the use of classic… (more)

Subjects/Keywords: Structural Optimization; Wing Optimization; SpaRibs; Aircraft Design; Particle Swarm Optimization; Supersonic Aircraft Design

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APA (6th Edition):

Locatelli, D. (2012). Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26345

Chicago Manual of Style (16th Edition):

Locatelli, Davide. “Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs.” 2012. Doctoral Dissertation, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/26345.

MLA Handbook (7th Edition):

Locatelli, Davide. “Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs.” 2012. Web. 25 Jan 2021.

Vancouver:

Locatelli D. Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/26345.

Council of Science Editors:

Locatelli D. Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/26345


Virginia Tech

23. Naghshineh-Pour, Amir H. Structural Optimization and Design of a Strut-Braced Wing Aircraft.

Degree: MS, Aerospace and Ocean Engineering, 1998, Virginia Tech

 A significant improvement can be achieved in the performance of transonic transport aircraft using Multidisciplinary Design Optimization (MDO) by implementing truss-braced wing concepts in combination… (more)

Subjects/Keywords: Strut-Braced Wing; Wing Box; Structural Optimization; Multidisciplinary Design Optimization; Aircraft Design

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APA (6th Edition):

Naghshineh-Pour, A. H. (1998). Structural Optimization and Design of a Strut-Braced Wing Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36142

Chicago Manual of Style (16th Edition):

Naghshineh-Pour, Amir H. “Structural Optimization and Design of a Strut-Braced Wing Aircraft.” 1998. Masters Thesis, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/36142.

MLA Handbook (7th Edition):

Naghshineh-Pour, Amir H. “Structural Optimization and Design of a Strut-Braced Wing Aircraft.” 1998. Web. 25 Jan 2021.

Vancouver:

Naghshineh-Pour AH. Structural Optimization and Design of a Strut-Braced Wing Aircraft. [Internet] [Masters thesis]. Virginia Tech; 1998. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/36142.

Council of Science Editors:

Naghshineh-Pour AH. Structural Optimization and Design of a Strut-Braced Wing Aircraft. [Masters Thesis]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/36142


Virginia Tech

24. McDonald, Melea E. The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft.

Degree: MS, Aerospace and Ocean Engineering, 2010, Virginia Tech

 In recent years, research has been conducted for alternative commercial transonic aircraft design configurations, such as the strut- braced wing and the truss-braced wing aircraft… (more)

Subjects/Keywords: Multidisciplinary Design Optimization; Aircraft Design; Strut-Braced Wing; Truss-Braced Wing; Transonic Transport

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APA (6th Edition):

McDonald, M. E. (2010). The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34124

Chicago Manual of Style (16th Edition):

McDonald, Melea E. “The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft.” 2010. Masters Thesis, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/34124.

MLA Handbook (7th Edition):

McDonald, Melea E. “The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft.” 2010. Web. 25 Jan 2021.

Vancouver:

McDonald ME. The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/34124.

Council of Science Editors:

McDonald ME. The Effect of Reducing Cruise Altitude on the Topology and Emissions of a Commercial Transport Aircraft. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/34124


Ryerson University

25. Kalaji, Ahmad T. Design And Experimental Studies Of Flexible Trailing Edge For Variable Camber Morphing Wing.

Degree: 2017, Ryerson University

 This thesis presents a flexible trailing edge mechanism capable of undergoing a change in camber for a wing section. The mechanism takes advantage of a… (more)

Subjects/Keywords: Wing-warping (Aerodynamics); Airplanes  – Wings  – Design and construction; Drag (Aerodynamics); Aeronautics  – Research

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APA (6th Edition):

Kalaji, A. T. (2017). Design And Experimental Studies Of Flexible Trailing Edge For Variable Camber Morphing Wing. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6844

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):

Kalaji, Ahmad T. “Design And Experimental Studies Of Flexible Trailing Edge For Variable Camber Morphing Wing.” 2017. Thesis, Ryerson University. Accessed January 25, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A6844.

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

MLA Handbook (7th Edition):

Kalaji, Ahmad T. “Design And Experimental Studies Of Flexible Trailing Edge For Variable Camber Morphing Wing.” 2017. Web. 25 Jan 2021.

Vancouver:

Kalaji AT. Design And Experimental Studies Of Flexible Trailing Edge For Variable Camber Morphing Wing. [Internet] [Thesis]. Ryerson University; 2017. [cited 2021 Jan 25]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6844.

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

Council of Science Editors:

Kalaji AT. Design And Experimental Studies Of Flexible Trailing Edge For Variable Camber Morphing Wing. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6844

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


University of Toronto

26. Galantai, Vlad Paul. Design and Analysis of Morphing Wing for Unmanned Aerial Vehicles.

Degree: 2012, University of Toronto

This study is concerned with the design and development of a novel wing for UAVs that morphs seamlessly without the use of complex hydraulics, servo… (more)

Subjects/Keywords: Morphing Wing; UAV; Shape Adaptation; Smart Materials; Shape Memory Alloy; Conceptual Design; RPV; Biomimetics; 0538

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APA (6th Edition):

Galantai, V. P. (2012). Design and Analysis of Morphing Wing for Unmanned Aerial Vehicles. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/33722

Chicago Manual of Style (16th Edition):

Galantai, Vlad Paul. “Design and Analysis of Morphing Wing for Unmanned Aerial Vehicles.” 2012. Masters Thesis, University of Toronto. Accessed January 25, 2021. http://hdl.handle.net/1807/33722.

MLA Handbook (7th Edition):

Galantai, Vlad Paul. “Design and Analysis of Morphing Wing for Unmanned Aerial Vehicles.” 2012. Web. 25 Jan 2021.

Vancouver:

Galantai VP. Design and Analysis of Morphing Wing for Unmanned Aerial Vehicles. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1807/33722.

Council of Science Editors:

Galantai VP. Design and Analysis of Morphing Wing for Unmanned Aerial Vehicles. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/33722


Delft University of Technology

27. Lambers, A.C. (author). Development of surrogate-based multidisciplinary optimization methodology with flutter constraints for aircraft conceptual design.

Degree: 2016, Delft University of Technology

Aircraft concepts with high aspect ratio wings have been investigated more extensively in the recent past, as such configurations would reduce the induced drag significantly.… (more)

Subjects/Keywords: Mutlidisciplinary Design Optimization; MDO; surrogate modelling; SBO; surrogate-based optimization; strut-braced wing; flutter

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APA (6th Edition):

Lambers, A. C. (. (2016). Development of surrogate-based multidisciplinary optimization methodology with flutter constraints for aircraft conceptual design. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a8f151f0-1c47-4a8a-9cef-b9784a1662cd

Chicago Manual of Style (16th Edition):

Lambers, A C (author). “Development of surrogate-based multidisciplinary optimization methodology with flutter constraints for aircraft conceptual design.” 2016. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:a8f151f0-1c47-4a8a-9cef-b9784a1662cd.

MLA Handbook (7th Edition):

Lambers, A C (author). “Development of surrogate-based multidisciplinary optimization methodology with flutter constraints for aircraft conceptual design.” 2016. Web. 25 Jan 2021.

Vancouver:

Lambers AC(. Development of surrogate-based multidisciplinary optimization methodology with flutter constraints for aircraft conceptual design. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:a8f151f0-1c47-4a8a-9cef-b9784a1662cd.

Council of Science Editors:

Lambers AC(. Development of surrogate-based multidisciplinary optimization methodology with flutter constraints for aircraft conceptual design. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:a8f151f0-1c47-4a8a-9cef-b9784a1662cd


Delft University of Technology

28. Rubio Pascual, Berta (author). Engine-Airframe Integration for the Flying-V.

Degree: 2018, Delft University of Technology

 The Flying-V is a novel flying wing concept where the main lifting surface has been fully integrated with the passenger cabin. Previous studies have focused… (more)

Subjects/Keywords: Flying V; Engine; Integration; flying wing; Interference; Aerodynamic; Aircraft design; positioning study

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APA (6th Edition):

Rubio Pascual, B. (. (2018). Engine-Airframe Integration for the Flying-V. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:75be27a7-6fd4-4112-a600-45df2999758f

Chicago Manual of Style (16th Edition):

Rubio Pascual, Berta (author). “Engine-Airframe Integration for the Flying-V.” 2018. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:75be27a7-6fd4-4112-a600-45df2999758f.

MLA Handbook (7th Edition):

Rubio Pascual, Berta (author). “Engine-Airframe Integration for the Flying-V.” 2018. Web. 25 Jan 2021.

Vancouver:

Rubio Pascual B(. Engine-Airframe Integration for the Flying-V. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:75be27a7-6fd4-4112-a600-45df2999758f.

Council of Science Editors:

Rubio Pascual B(. Engine-Airframe Integration for the Flying-V. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:75be27a7-6fd4-4112-a600-45df2999758f


Delft University of Technology

29. Mangano, Marco (author). Multi-point aerodynamic shape optimization for airfoils and wings at supersonic and subsonic regimes.

Degree: 2019, Delft University of Technology

 The second-generation of supersonic civil transport has to match ambitious targets in terms of noise reduction and efficiency to become economically and environmentally viable. High-fidelity… (more)

Subjects/Keywords: Optimization; Aerodynamics; MDO; CFD; Supersonic; wing design; Airfoil; morphing; Gradient-based Optimization

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

APA (6th Edition):

Mangano, M. (. (2019). Multi-point aerodynamic shape optimization for airfoils and wings at supersonic and subsonic regimes. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4a40e302-bdf1-4319-81de-a6aad9376d65

Chicago Manual of Style (16th Edition):

Mangano, Marco (author). “Multi-point aerodynamic shape optimization for airfoils and wings at supersonic and subsonic regimes.” 2019. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:4a40e302-bdf1-4319-81de-a6aad9376d65.

MLA Handbook (7th Edition):

Mangano, Marco (author). “Multi-point aerodynamic shape optimization for airfoils and wings at supersonic and subsonic regimes.” 2019. Web. 25 Jan 2021.

Vancouver:

Mangano M(. Multi-point aerodynamic shape optimization for airfoils and wings at supersonic and subsonic regimes. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:4a40e302-bdf1-4319-81de-a6aad9376d65.

Council of Science Editors:

Mangano M(. Multi-point aerodynamic shape optimization for airfoils and wings at supersonic and subsonic regimes. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:4a40e302-bdf1-4319-81de-a6aad9376d65


Virginia Tech

30. Mallik, Wrik. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.

Degree: PhD, Aerospace Engineering, 2016, Virginia Tech

 This study highlights the aeroelastic behavior of very flexible truss-braced wing (TBW) aircraft designs obtained through a multidisciplinary design optimization (MDO) framework. Several improvements to… (more)

Subjects/Keywords: Aeroelasticity; Multidisciplinary Design Optimization; Truss-Braced Wing Aircraft; Variable Geometry Raked Wingtip; State-space Aerodynamics

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

APA (6th Edition):

Mallik, W. (2016). Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71650

Chicago Manual of Style (16th Edition):

Mallik, Wrik. “Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.” 2016. Doctoral Dissertation, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/71650.

MLA Handbook (7th Edition):

Mallik, Wrik. “Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.” 2016. Web. 25 Jan 2021.

Vancouver:

Mallik W. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/71650.

Council of Science Editors:

Mallik W. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71650

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