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You searched for subject:(Aircraft design). Showing records 1 – 30 of 286 total matches.

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Delft University of Technology

1. Le, N.T.P. The design of a next generation Y class aircraft seat:.

Degree: 2015, Delft University of Technology

 Globalization has resulted in an increase in demand for air travel, whether for business or for leisure. And this demand is expected to rise a… (more)

Subjects/Keywords: aircraft seat; design

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APA (6th Edition):

Le, N. T. P. (2015). The design of a next generation Y class aircraft seat:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f

Chicago Manual of Style (16th Edition):

Le, N T P. “The design of a next generation Y class aircraft seat:.” 2015. Masters Thesis, Delft University of Technology. Accessed October 16, 2019. http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f.

MLA Handbook (7th Edition):

Le, N T P. “The design of a next generation Y class aircraft seat:.” 2015. Web. 16 Oct 2019.

Vancouver:

Le NTP. The design of a next generation Y class aircraft seat:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Oct 16]. Available from: http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f.

Council of Science Editors:

Le NTP. The design of a next generation Y class aircraft seat:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f4307eb4-f448-40d9-b65a-5a0a3356904f


University of Western Australia

2. Bryant, David. Design and prototyping of an aircraft to maximize the triaviation score.

Degree: M. Eng.Sci., 2008, University of Western Australia

This thesis describes some of the processes and results obtained during the design and prototyping of a single seat experimental aircraft. The major aim was… (more)

Subjects/Keywords: Airplanes; Research aircraft; Aircraft design; Triaviation score; Experimental aircraft

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APA (6th Edition):

Bryant, D. (2008). Design and prototyping of an aircraft to maximize the triaviation score. (Masters Thesis). University of Western Australia. Retrieved from http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01

Chicago Manual of Style (16th Edition):

Bryant, David. “Design and prototyping of an aircraft to maximize the triaviation score.” 2008. Masters Thesis, University of Western Australia. Accessed October 16, 2019. http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01.

MLA Handbook (7th Edition):

Bryant, David. “Design and prototyping of an aircraft to maximize the triaviation score.” 2008. Web. 16 Oct 2019.

Vancouver:

Bryant D. Design and prototyping of an aircraft to maximize the triaviation score. [Internet] [Masters thesis]. University of Western Australia; 2008. [cited 2019 Oct 16]. Available from: http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01.

Council of Science Editors:

Bryant D. Design and prototyping of an aircraft to maximize the triaviation score. [Masters Thesis]. University of Western Australia; 2008. Available from: http://repository.uwa.edu.au:80/R/?func=dbin-jump-full&object_id=6314&local_base=GEN01-INS01

3. Al-Shamma, Omran. Development of Interactive Aircraft Design Software for Use in Problem Based Learning .

Degree: 2013, University of Hertfordshire

 In the last ten years or so, many interactive aircraft design software packages have been released into the market. One drawback of these packages is… (more)

Subjects/Keywords: Aircraft Design; Problem-Based Learning; Preliminary Aircraft Design; Aircraft Design Software; Weight Estimation; Cost Estimation

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APA (6th Edition):

Al-Shamma, O. (2013). Development of Interactive Aircraft Design Software for Use in Problem Based Learning . (Thesis). University of Hertfordshire. Retrieved from http://hdl.handle.net/2299/12108

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):

Al-Shamma, Omran. “Development of Interactive Aircraft Design Software for Use in Problem Based Learning .” 2013. Thesis, University of Hertfordshire. Accessed October 16, 2019. http://hdl.handle.net/2299/12108.

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

MLA Handbook (7th Edition):

Al-Shamma, Omran. “Development of Interactive Aircraft Design Software for Use in Problem Based Learning .” 2013. Web. 16 Oct 2019.

Vancouver:

Al-Shamma O. Development of Interactive Aircraft Design Software for Use in Problem Based Learning . [Internet] [Thesis]. University of Hertfordshire; 2013. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/2299/12108.

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

Council of Science Editors:

Al-Shamma O. Development of Interactive Aircraft Design Software for Use in Problem Based Learning . [Thesis]. University of Hertfordshire; 2013. Available from: http://hdl.handle.net/2299/12108

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


Delft University of Technology

4. Miedema, J.J. MySeat: Development of a user focused aircraft seat:.

Degree: 2013, Delft University of Technology

 This master thesis shows the research and development of a user focused aircraft seat. The project is done in collaboration with Zodiac Seats US, an… (more)

Subjects/Keywords: aircraft interior; design for comfort; design; aircraft seat; user centered design

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APA (6th Edition):

Miedema, J. J. (2013). MySeat: Development of a user focused aircraft seat:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1a77e68d-54ab-4970-80f5-75fe5a51f408

Chicago Manual of Style (16th Edition):

Miedema, J J. “MySeat: Development of a user focused aircraft seat:.” 2013. Masters Thesis, Delft University of Technology. Accessed October 16, 2019. http://resolver.tudelft.nl/uuid:1a77e68d-54ab-4970-80f5-75fe5a51f408.

MLA Handbook (7th Edition):

Miedema, J J. “MySeat: Development of a user focused aircraft seat:.” 2013. Web. 16 Oct 2019.

Vancouver:

Miedema JJ. MySeat: Development of a user focused aircraft seat:. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2019 Oct 16]. Available from: http://resolver.tudelft.nl/uuid:1a77e68d-54ab-4970-80f5-75fe5a51f408.

Council of Science Editors:

Miedema JJ. MySeat: Development of a user focused aircraft seat:. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:1a77e68d-54ab-4970-80f5-75fe5a51f408

5. [No author]. Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft.

Degree: PhD, Mechanical Engineering/G??nie m??canique, 2016, Royal Military College of Canada

A multidisciplinary study of an unconventional aircraft configuration was undertaken to determine if such a design could decrease the environmental impact of civil air transportation… (more)

Subjects/Keywords: Aircraft design; Optimization; Nonplanar wings

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APA (6th Edition):

author], [. (2016). Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft. (Doctoral Dissertation). Royal Military College of Canada. Retrieved from http://hdl.handle.net/11264/981

Chicago Manual of Style (16th Edition):

author], [No. “Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft.” 2016. Doctoral Dissertation, Royal Military College of Canada. Accessed October 16, 2019. http://hdl.handle.net/11264/981.

MLA Handbook (7th Edition):

author], [No. “Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft.” 2016. Web. 16 Oct 2019.

Vancouver:

author] [. Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft. [Internet] [Doctoral dissertation]. Royal Military College of Canada; 2016. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/11264/981.

Council of Science Editors:

author] [. Multidisciplinary Analysis of Closed, Nonplanar Wing Configurations for Transport Aircraft. [Doctoral Dissertation]. Royal Military College of Canada; 2016. Available from: http://hdl.handle.net/11264/981


Georgia Tech

6. Corman, Jason A. A methodology for structural technology performance characterization to enable reduction of structural uncertainty.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Government programs have been established to identify solutions that will significantly reduce the impact of aviation on the environment in the upcoming generations. Airframe structural… (more)

Subjects/Keywords: Aircraft design; Airframe structural technology

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APA (6th Edition):

Corman, J. A. (2017). A methodology for structural technology performance characterization to enable reduction of structural uncertainty. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59795

Chicago Manual of Style (16th Edition):

Corman, Jason A. “A methodology for structural technology performance characterization to enable reduction of structural uncertainty.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 16, 2019. http://hdl.handle.net/1853/59795.

MLA Handbook (7th Edition):

Corman, Jason A. “A methodology for structural technology performance characterization to enable reduction of structural uncertainty.” 2017. Web. 16 Oct 2019.

Vancouver:

Corman JA. A methodology for structural technology performance characterization to enable reduction of structural uncertainty. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/1853/59795.

Council of Science Editors:

Corman JA. A methodology for structural technology performance characterization to enable reduction of structural uncertainty. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59795


San Jose State University

7. Arnold, Deeptanshu. Study of Fly-by-Wire Flight Control System and its Benefits for Jet Transport.

Degree: MS, Mechanical and Aerospace Engineering, 2010, San Jose State University

  In a never-ending quest for reducing aircraft weight, an attempt is made to decrease the size of the horizontal stabilizer of a jet transport… (more)

Subjects/Keywords: Aircraft Design; Controls; Dynamics; Structures

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APA (6th Edition):

Arnold, D. (2010). Study of Fly-by-Wire Flight Control System and its Benefits for Jet Transport. (Masters Thesis). San Jose State University. Retrieved from https://doi.org/10.31979/etd.ac6t-bzvg ; https://scholarworks.sjsu.edu/etd_theses/3745

Chicago Manual of Style (16th Edition):

Arnold, Deeptanshu. “Study of Fly-by-Wire Flight Control System and its Benefits for Jet Transport.” 2010. Masters Thesis, San Jose State University. Accessed October 16, 2019. https://doi.org/10.31979/etd.ac6t-bzvg ; https://scholarworks.sjsu.edu/etd_theses/3745.

MLA Handbook (7th Edition):

Arnold, Deeptanshu. “Study of Fly-by-Wire Flight Control System and its Benefits for Jet Transport.” 2010. Web. 16 Oct 2019.

Vancouver:

Arnold D. Study of Fly-by-Wire Flight Control System and its Benefits for Jet Transport. [Internet] [Masters thesis]. San Jose State University; 2010. [cited 2019 Oct 16]. Available from: https://doi.org/10.31979/etd.ac6t-bzvg ; https://scholarworks.sjsu.edu/etd_theses/3745.

Council of Science Editors:

Arnold D. Study of Fly-by-Wire Flight Control System and its Benefits for Jet Transport. [Masters Thesis]. San Jose State University; 2010. Available from: https://doi.org/10.31979/etd.ac6t-bzvg ; https://scholarworks.sjsu.edu/etd_theses/3745


University of Sydney

8. Sharifzadeh, Shayan. Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles .

Degree: 2017, University of Sydney

 Aviation industry is continuously growing especially for very long distance flights due to the globalisation of local economies around the world and the explosive economic… (more)

Subjects/Keywords: Hypersonic; aircraft; design; cryogenic; hydrogen

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APA (6th Edition):

Sharifzadeh, S. (2017). Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/19127

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):

Sharifzadeh, Shayan. “Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles .” 2017. Thesis, University of Sydney. Accessed October 16, 2019. http://hdl.handle.net/2123/19127.

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

MLA Handbook (7th Edition):

Sharifzadeh, Shayan. “Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles .” 2017. Web. 16 Oct 2019.

Vancouver:

Sharifzadeh S. Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles . [Internet] [Thesis]. University of Sydney; 2017. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/2123/19127.

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

Council of Science Editors:

Sharifzadeh S. Design Optimization and Analysis of Long-Range Hydrogen-Fuelled Hypersonic Cruise Vehicles . [Thesis]. University of Sydney; 2017. Available from: http://hdl.handle.net/2123/19127

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


Ryerson University

9. Simms, Devin. Lidar-based surface following control for unmanned aerial vehicles.

Degree: 2017, Ryerson University

 A simulation study is performed on a quadcopter which uses a LIDAR sensor to allow a quadcopter to navigate along and maintain a set distance… (more)

Subjects/Keywords: Drone aircraft  – Design and construction; Drone aircraft  – Control systems; Drone aircraft; Optical radar

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APA (6th Edition):

Simms, D. (2017). Lidar-based surface following control for unmanned aerial vehicles. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6636

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):

Simms, Devin. “Lidar-based surface following control for unmanned aerial vehicles.” 2017. Thesis, Ryerson University. Accessed October 16, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A6636.

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

MLA Handbook (7th Edition):

Simms, Devin. “Lidar-based surface following control for unmanned aerial vehicles.” 2017. Web. 16 Oct 2019.

Vancouver:

Simms D. Lidar-based surface following control for unmanned aerial vehicles. [Internet] [Thesis]. Ryerson University; 2017. [cited 2019 Oct 16]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6636.

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

Council of Science Editors:

Simms D. Lidar-based surface following control for unmanned aerial vehicles. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6636

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


Virginia Tech

10. Allison, Darcy L. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.

Degree: PhD, Aerospace Engineering, 2013, Virginia Tech

 This work seeks to develop multidisciplinary design optimization (MDO) methods to find the optimal design of a particular aircraft called an Efficient Supersonic Air Vehicle… (more)

Subjects/Keywords: aircraft design; multidisciplinary design optimization; supersonic military aircraft; design of computer experiments

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APA (6th Edition):

Allison, D. L. (2013). Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24187

Chicago Manual of Style (16th Edition):

Allison, Darcy L. “Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.” 2013. Doctoral Dissertation, Virginia Tech. Accessed October 16, 2019. http://hdl.handle.net/10919/24187.

MLA Handbook (7th Edition):

Allison, Darcy L. “Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.” 2013. Web. 16 Oct 2019.

Vancouver:

Allison DL. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/10919/24187.

Council of Science Editors:

Allison DL. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/24187


Georgia Tech

11. Patterson, Michael Dobson. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The maturation of electric propulsion technologies presents intriguing new degrees of freedom for aircraft designers including the ability to distribute many small propellers upstream of… (more)

Subjects/Keywords: distributed electric propulsion; high-lift propellers; aircraft design; aircraft performance; design method; propeller design

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APA (6th Edition):

Patterson, M. D. (2016). Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55569

Chicago Manual of Style (16th Edition):

Patterson, Michael Dobson. “Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 16, 2019. http://hdl.handle.net/1853/55569.

MLA Handbook (7th Edition):

Patterson, Michael Dobson. “Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.” 2016. Web. 16 Oct 2019.

Vancouver:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/1853/55569.

Council of Science Editors:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55569


RMIT University

12. Zhao, H. Development of a dynamic model of a ducted fan VTOL UAV.

Degree: 2009, RMIT University

 The technology of UAV (Unmanned Aerial Vehicle) has developed since its conception many years ago. UAVs have several features such as, computerised and autonomous control… (more)

Subjects/Keywords: Fields of Research; Drone aircraft  – Design and construction; Vertically rising aircraft

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APA (6th Edition):

Zhao, H. (2009). Development of a dynamic model of a ducted fan VTOL UAV. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:6872

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):

Zhao, H. “Development of a dynamic model of a ducted fan VTOL UAV.” 2009. Thesis, RMIT University. Accessed October 16, 2019. http://researchbank.rmit.edu.au/view/rmit:6872.

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

MLA Handbook (7th Edition):

Zhao, H. “Development of a dynamic model of a ducted fan VTOL UAV.” 2009. Web. 16 Oct 2019.

Vancouver:

Zhao H. Development of a dynamic model of a ducted fan VTOL UAV. [Internet] [Thesis]. RMIT University; 2009. [cited 2019 Oct 16]. Available from: http://researchbank.rmit.edu.au/view/rmit:6872.

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

Council of Science Editors:

Zhao H. Development of a dynamic model of a ducted fan VTOL UAV. [Thesis]. RMIT University; 2009. Available from: http://researchbank.rmit.edu.au/view/rmit:6872

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


Hong Kong University of Science and Technology

13. Wang, Ya. The design, prototyping, modeling and flight tests of a vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV).

Degree: 2017, Hong Kong University of Science and Technology

 This paper presents the design and implementation of a cost-effective, lightweight, yet power efficient tail-sitter Vertical Take-off and Landing (VTOL) unmanned aerial vehicle (UAV). The… (more)

Subjects/Keywords: Drone aircraft; Design and construction; Vertically rising aircraft

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APA (6th Edition):

Wang, Y. (2017). The design, prototyping, modeling and flight tests of a vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV). (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-991012535962203412 ; http://repository.ust.hk/ir/bitstream/1783.1-88458/1/th_redirect.html

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):

Wang, Ya. “The design, prototyping, modeling and flight tests of a vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV).” 2017. Thesis, Hong Kong University of Science and Technology. Accessed October 16, 2019. https://doi.org/10.14711/thesis-991012535962203412 ; http://repository.ust.hk/ir/bitstream/1783.1-88458/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Wang, Ya. “The design, prototyping, modeling and flight tests of a vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV).” 2017. Web. 16 Oct 2019.

Vancouver:

Wang Y. The design, prototyping, modeling and flight tests of a vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV). [Internet] [Thesis]. Hong Kong University of Science and Technology; 2017. [cited 2019 Oct 16]. Available from: https://doi.org/10.14711/thesis-991012535962203412 ; http://repository.ust.hk/ir/bitstream/1783.1-88458/1/th_redirect.html.

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

Council of Science Editors:

Wang Y. The design, prototyping, modeling and flight tests of a vertical take-off and landing (VTOL) unmanned aerial vehicle (UAV). [Thesis]. Hong Kong University of Science and Technology; 2017. Available from: https://doi.org/10.14711/thesis-991012535962203412 ; http://repository.ust.hk/ir/bitstream/1783.1-88458/1/th_redirect.html

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


University of Dayton

14. Landolfo, Giuseppe. Aerodynamic and Structural Design of a Small Nonplanar Wing UAV.

Degree: MS(M.S.), Aerospace Engineering, 2008, University of Dayton

 The overall air vehicle performance of a multiple lifting surface configuration has been studied with respect to both structural and aerodynamic considerations for a candidate… (more)

Subjects/Keywords: Engineering; Aerospace; aircraft design; aerodynamics; structural analysis; UAV; unmanned aircraft; biplane

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APA (6th Edition):

Landolfo, G. (2008). Aerodynamic and Structural Design of a Small Nonplanar Wing UAV. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704

Chicago Manual of Style (16th Edition):

Landolfo, Giuseppe. “Aerodynamic and Structural Design of a Small Nonplanar Wing UAV.” 2008. Masters Thesis, University of Dayton. Accessed October 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704.

MLA Handbook (7th Edition):

Landolfo, Giuseppe. “Aerodynamic and Structural Design of a Small Nonplanar Wing UAV.” 2008. Web. 16 Oct 2019.

Vancouver:

Landolfo G. Aerodynamic and Structural Design of a Small Nonplanar Wing UAV. [Internet] [Masters thesis]. University of Dayton; 2008. [cited 2019 Oct 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704.

Council of Science Editors:

Landolfo G. Aerodynamic and Structural Design of a Small Nonplanar Wing UAV. [Masters Thesis]. University of Dayton; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1262089704


Ryerson University

15. Kwon, Ohyun. Development of UAV derivative MDO methodology for flight simulation.

Degree: 2016, Ryerson University

 An integrated methodology for the design of an Unmanned Aerial Vehicle (UAV) derivative has been developed. The proposed methodology utilized the Multidisciplinary Design Optimization (MDO)… (more)

Subjects/Keywords: Drone aircraft  – Mathematical models; Drone aircraft  – Design and construction

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APA (6th Edition):

Kwon, O. (2016). Development of UAV derivative MDO methodology for flight simulation. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A5004

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):

Kwon, Ohyun. “Development of UAV derivative MDO methodology for flight simulation.” 2016. Thesis, Ryerson University. Accessed October 16, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A5004.

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

MLA Handbook (7th Edition):

Kwon, Ohyun. “Development of UAV derivative MDO methodology for flight simulation.” 2016. Web. 16 Oct 2019.

Vancouver:

Kwon O. Development of UAV derivative MDO methodology for flight simulation. [Internet] [Thesis]. Ryerson University; 2016. [cited 2019 Oct 16]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A5004.

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

Council of Science Editors:

Kwon O. Development of UAV derivative MDO methodology for flight simulation. [Thesis]. Ryerson University; 2016. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A5004

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


University of Johannesburg

16. Wilkins, Grant. Design and implementation of a power system for a solar unmanned aerial vehicle.

Degree: 2012, University of Johannesburg

M. Ing.

Solar powered UAV's have gained world wide attention with aircraft such as Solar Impulse and Quinetiq's Zephyr. UAV's in general are becomming increasingly… (more)

Subjects/Keywords: Solar aircraft; Drone aircraft; Unmanned aerial vehicle; Solar power system design

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

APA (6th Edition):

Wilkins, G. (2012). Design and implementation of a power system for a solar unmanned aerial vehicle. (Thesis). University of Johannesburg. Retrieved from http://hdl.handle.net/10210/4835

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):

Wilkins, Grant. “Design and implementation of a power system for a solar unmanned aerial vehicle.” 2012. Thesis, University of Johannesburg. Accessed October 16, 2019. http://hdl.handle.net/10210/4835.

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

MLA Handbook (7th Edition):

Wilkins, Grant. “Design and implementation of a power system for a solar unmanned aerial vehicle.” 2012. Web. 16 Oct 2019.

Vancouver:

Wilkins G. Design and implementation of a power system for a solar unmanned aerial vehicle. [Internet] [Thesis]. University of Johannesburg; 2012. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/10210/4835.

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

Council of Science Editors:

Wilkins G. Design and implementation of a power system for a solar unmanned aerial vehicle. [Thesis]. University of Johannesburg; 2012. Available from: http://hdl.handle.net/10210/4835

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


University of Florida

17. Schneider, Alexander Wolfgang. Wing Spar Optimization of Radio Controlled Size Aircraft.

Degree: 2016, University of Florida

 This honors thesis shall provide a comprehensive optimization of wing spars for use in radio controlled aircraft. The model aircraft chosen for the experimentation is… (more)

Subjects/Keywords: Aircraft; Aircraft design; Aircraft wings; Carbon fibers; Cost functions; Design analysis; Design engineering; Design optimization; Moduli of elasticity; Structural deflection; Aircraft; Design; Optimization; Spar; Wing

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APA (6th Edition):

Schneider, A. W. (2016). Wing Spar Optimization of Radio Controlled Size Aircraft. (Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/AA00046860

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):

Schneider, Alexander Wolfgang. “Wing Spar Optimization of Radio Controlled Size Aircraft.” 2016. Thesis, University of Florida. Accessed October 16, 2019. http://ufdc.ufl.edu/AA00046860.

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

MLA Handbook (7th Edition):

Schneider, Alexander Wolfgang. “Wing Spar Optimization of Radio Controlled Size Aircraft.” 2016. Web. 16 Oct 2019.

Vancouver:

Schneider AW. Wing Spar Optimization of Radio Controlled Size Aircraft. [Internet] [Thesis]. University of Florida; 2016. [cited 2019 Oct 16]. Available from: http://ufdc.ufl.edu/AA00046860.

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

Council of Science Editors:

Schneider AW. Wing Spar Optimization of Radio Controlled Size Aircraft. [Thesis]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/AA00046860

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


Ryerson University

18. George, Issi-Rae Emanuelle. A multirotor vehicle performance prediction method.

Degree: 2017, Ryerson University

 A method has been developed to predict the performance of small multirotor vehicles. Using the vehicle geometry, rotor geometry and flight conditions as inputs, the… (more)

Subjects/Keywords: Drone aircraft  – Design and construction; Drone aircraft  – Flight testing; Drone aircraft  – Testing; Drone aircraft  – Aerodynamics; Rotors  – Aerodynamics  – Mathematical models; Rotors  – Testing

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APA (6th Edition):

George, I. E. (2017). A multirotor vehicle performance prediction method. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6879

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):

George, Issi-Rae Emanuelle. “A multirotor vehicle performance prediction method.” 2017. Thesis, Ryerson University. Accessed October 16, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A6879.

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

MLA Handbook (7th Edition):

George, Issi-Rae Emanuelle. “A multirotor vehicle performance prediction method.” 2017. Web. 16 Oct 2019.

Vancouver:

George IE. A multirotor vehicle performance prediction method. [Internet] [Thesis]. Ryerson University; 2017. [cited 2019 Oct 16]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6879.

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

Council of Science Editors:

George IE. A multirotor vehicle performance prediction method. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6879

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


University of Limerick

19. Gray, Patrick Joseph. Highly efficient numerical analysis of load distribution in composite bolted joints.

Degree: 2011, University of Limerick

peer-reviewed

In the design of composite aircraft structures, joint efficiency is a key area for realising the weight-saving potential of advanced composite materials. Cost-effective, efficient… (more)

Subjects/Keywords: composite aircraft structure; design; bolted joints

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APA (6th Edition):

Gray, P. J. (2011). Highly efficient numerical analysis of load distribution in composite bolted joints. (Thesis). University of Limerick. Retrieved from http://hdl.handle.net/10344/5957

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):

Gray, Patrick Joseph. “Highly efficient numerical analysis of load distribution in composite bolted joints.” 2011. Thesis, University of Limerick. Accessed October 16, 2019. http://hdl.handle.net/10344/5957.

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

MLA Handbook (7th Edition):

Gray, Patrick Joseph. “Highly efficient numerical analysis of load distribution in composite bolted joints.” 2011. Web. 16 Oct 2019.

Vancouver:

Gray PJ. Highly efficient numerical analysis of load distribution in composite bolted joints. [Internet] [Thesis]. University of Limerick; 2011. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/10344/5957.

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

Council of Science Editors:

Gray PJ. Highly efficient numerical analysis of load distribution in composite bolted joints. [Thesis]. University of Limerick; 2011. Available from: http://hdl.handle.net/10344/5957

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


Georgia Tech

20. Miller, Michael Z. A decision support framework for aircraft conceptual design in the presence of competition.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Most conceptual design techniques for aircraft implicitly assume that the aircraft manufacturer operates in a monopoly. This is because these techniques do not directly account… (more)

Subjects/Keywords: Aircraft; Conceptual design; Uncertainty; Competition; Probabilistic

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APA (6th Edition):

Miller, M. Z. (2016). A decision support framework for aircraft conceptual design in the presence of competition. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55585

Chicago Manual of Style (16th Edition):

Miller, Michael Z. “A decision support framework for aircraft conceptual design in the presence of competition.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 16, 2019. http://hdl.handle.net/1853/55585.

MLA Handbook (7th Edition):

Miller, Michael Z. “A decision support framework for aircraft conceptual design in the presence of competition.” 2016. Web. 16 Oct 2019.

Vancouver:

Miller MZ. A decision support framework for aircraft conceptual design in the presence of competition. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/1853/55585.

Council of Science Editors:

Miller MZ. A decision support framework for aircraft conceptual design in the presence of competition. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55585


University of Plymouth

21. Bonham, Christopher Richard. Evolutionary decomposition of complex design spaces.

Degree: PhD, 2000, University of Plymouth

 This dissertation investigates the support of conceptual engineering design through the decomposition of multi-dimensional search spaces into regions of high performance. Such decomposition helps the… (more)

Subjects/Keywords: 620.0042029; Aircraft design

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APA (6th Edition):

Bonham, C. R. (2000). Evolutionary decomposition of complex design spaces. (Doctoral Dissertation). University of Plymouth. Retrieved from http://hdl.handle.net/10026.1/2274

Chicago Manual of Style (16th Edition):

Bonham, Christopher Richard. “Evolutionary decomposition of complex design spaces.” 2000. Doctoral Dissertation, University of Plymouth. Accessed October 16, 2019. http://hdl.handle.net/10026.1/2274.

MLA Handbook (7th Edition):

Bonham, Christopher Richard. “Evolutionary decomposition of complex design spaces.” 2000. Web. 16 Oct 2019.

Vancouver:

Bonham CR. Evolutionary decomposition of complex design spaces. [Internet] [Doctoral dissertation]. University of Plymouth; 2000. [cited 2019 Oct 16]. Available from: http://hdl.handle.net/10026.1/2274.

Council of Science Editors:

Bonham CR. Evolutionary decomposition of complex design spaces. [Doctoral Dissertation]. University of Plymouth; 2000. Available from: http://hdl.handle.net/10026.1/2274


Hong Kong University of Science and Technology

22. Wang, Mingxi. The design and development of a base station for small unmanned aerial vehicle.

Degree: 2016, Hong Kong University of Science and Technology

 Unmanned aerial vehicle (UAV) is being used in various applications, such as consumer electronics, aerial filming and infrastructure inspection. Certain UAV applications require a fully… (more)

Subjects/Keywords: Drone aircraft; Control systems; Design and construction

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

APA (6th Edition):

Wang, M. (2016). The design and development of a base station for small unmanned aerial vehicle. (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-b1627134 ; http://repository.ust.hk/ir/bitstream/1783.1-88559/1/th_redirect.html

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):

Wang, Mingxi. “The design and development of a base station for small unmanned aerial vehicle.” 2016. Thesis, Hong Kong University of Science and Technology. Accessed October 16, 2019. https://doi.org/10.14711/thesis-b1627134 ; http://repository.ust.hk/ir/bitstream/1783.1-88559/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Wang, Mingxi. “The design and development of a base station for small unmanned aerial vehicle.” 2016. Web. 16 Oct 2019.

Vancouver:

Wang M. The design and development of a base station for small unmanned aerial vehicle. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2016. [cited 2019 Oct 16]. Available from: https://doi.org/10.14711/thesis-b1627134 ; http://repository.ust.hk/ir/bitstream/1783.1-88559/1/th_redirect.html.

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

Council of Science Editors:

Wang M. The design and development of a base station for small unmanned aerial vehicle. [Thesis]. Hong Kong University of Science and Technology; 2016. Available from: https://doi.org/10.14711/thesis-b1627134 ; http://repository.ust.hk/ir/bitstream/1783.1-88559/1/th_redirect.html

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


Louisiana State University

23. King, Sean Lauderdale. Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System.

Degree: MSME, Aerodynamics and Fluid Mechanics, 2018, Louisiana State University

  The purpose of this thesis is to conceptually design a fixed-wing unmanned aircraft systems (UAS) with a higher flight-time and top stable speed than… (more)

Subjects/Keywords: Design; Aerodynamics; Control; Unmanned Aircraft System

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

APA (6th Edition):

King, S. L. (2018). Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System. (Masters Thesis). Louisiana State University. Retrieved from https://digitalcommons.lsu.edu/gradschool_theses/4773

Chicago Manual of Style (16th Edition):

King, Sean Lauderdale. “Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System.” 2018. Masters Thesis, Louisiana State University. Accessed October 16, 2019. https://digitalcommons.lsu.edu/gradschool_theses/4773.

MLA Handbook (7th Edition):

King, Sean Lauderdale. “Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System.” 2018. Web. 16 Oct 2019.

Vancouver:

King SL. Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System. [Internet] [Masters thesis]. Louisiana State University; 2018. [cited 2019 Oct 16]. Available from: https://digitalcommons.lsu.edu/gradschool_theses/4773.

Council of Science Editors:

King SL. Design and Performance Estimation of a Low-Reynolds Number Unmanned Aircraft System. [Masters Thesis]. Louisiana State University; 2018. Available from: https://digitalcommons.lsu.edu/gradschool_theses/4773


Delft University of Technology

24. De Gelder, V. Concepts for a large commercial aircraft rudder:.

Degree: 2015, Delft University of Technology

 Fokker Aerostructures is a world leading specialist in the application thermoplastic carbon fiber reinforced plastics (CFRP) material on control surfaces of business jets. They want… (more)

Subjects/Keywords: Rudder; Aircraft Design; Market analysis; Concept development

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APA (6th Edition):

De Gelder, V. (2015). Concepts for a large commercial aircraft rudder:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:824e12d9-72c7-48f4-b333-c9ae380531b5

Chicago Manual of Style (16th Edition):

De Gelder, V. “Concepts for a large commercial aircraft rudder:.” 2015. Masters Thesis, Delft University of Technology. Accessed October 16, 2019. http://resolver.tudelft.nl/uuid:824e12d9-72c7-48f4-b333-c9ae380531b5.

MLA Handbook (7th Edition):

De Gelder, V. “Concepts for a large commercial aircraft rudder:.” 2015. Web. 16 Oct 2019.

Vancouver:

De Gelder V. Concepts for a large commercial aircraft rudder:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Oct 16]. Available from: http://resolver.tudelft.nl/uuid:824e12d9-72c7-48f4-b333-c9ae380531b5.

Council of Science Editors:

De Gelder V. Concepts for a large commercial aircraft rudder:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:824e12d9-72c7-48f4-b333-c9ae380531b5


Delft University of Technology

25. Mulder, A. A methodological approach for optimisation of product development processes by application of design automation:.

Degree: 2015, Delft University of Technology

 In the past decades a clear transition can be seen from fully human-based production techniques towards more automated systems. With the Product Development Process (PDP)… (more)

Subjects/Keywords: optimisation; product development process; aircraft design; methodology

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APA (6th Edition):

Mulder, A. (2015). A methodological approach for optimisation of product development processes by application of design automation:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5a7520f7-373d-44a5-9961-931ba9fdca15

Chicago Manual of Style (16th Edition):

Mulder, A. “A methodological approach for optimisation of product development processes by application of design automation:.” 2015. Masters Thesis, Delft University of Technology. Accessed October 16, 2019. http://resolver.tudelft.nl/uuid:5a7520f7-373d-44a5-9961-931ba9fdca15.

MLA Handbook (7th Edition):

Mulder, A. “A methodological approach for optimisation of product development processes by application of design automation:.” 2015. Web. 16 Oct 2019.

Vancouver:

Mulder A. A methodological approach for optimisation of product development processes by application of design automation:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Oct 16]. Available from: http://resolver.tudelft.nl/uuid:5a7520f7-373d-44a5-9961-931ba9fdca15.

Council of Science Editors:

Mulder A. A methodological approach for optimisation of product development processes by application of design automation:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:5a7520f7-373d-44a5-9961-931ba9fdca15


Delft University of Technology

26. Ramakers, M.A.Y. Accelerating aircraft design using automated process generation: An experimental architecture for aircraft design software:.

Degree: 2015, Delft University of Technology

 The aircraft industry has seen many evolutionary changes in the past decades. Since the Boeing 707 however, the general shape and configuration of transport aircraft(more)

Subjects/Keywords: aircraft design; process modelling; automated; software

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APA (6th Edition):

Ramakers, M. A. Y. (2015). Accelerating aircraft design using automated process generation: An experimental architecture for aircraft design software:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1cdca7a1-a440-4dce-9fce-859fd9701839

Chicago Manual of Style (16th Edition):

Ramakers, M A Y. “Accelerating aircraft design using automated process generation: An experimental architecture for aircraft design software:.” 2015. Masters Thesis, Delft University of Technology. Accessed October 16, 2019. http://resolver.tudelft.nl/uuid:1cdca7a1-a440-4dce-9fce-859fd9701839.

MLA Handbook (7th Edition):

Ramakers, M A Y. “Accelerating aircraft design using automated process generation: An experimental architecture for aircraft design software:.” 2015. Web. 16 Oct 2019.

Vancouver:

Ramakers MAY. Accelerating aircraft design using automated process generation: An experimental architecture for aircraft design software:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Oct 16]. Available from: http://resolver.tudelft.nl/uuid:1cdca7a1-a440-4dce-9fce-859fd9701839.

Council of Science Editors:

Ramakers MAY. Accelerating aircraft design using automated process generation: An experimental architecture for aircraft design software:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:1cdca7a1-a440-4dce-9fce-859fd9701839


Virginia Tech

27. 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 October 16, 2019. http://hdl.handle.net/10919/26345.

MLA Handbook (7th Edition):

Locatelli, Davide. “Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs.” 2012. Web. 16 Oct 2019.

Vancouver:

Locatelli D. Optimization of Supersonic Aircraft Wing-Box using Curvilinear SpaRibs. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2019 Oct 16]. 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


RMIT University

28. Roy Salam, I. Multidisciplinary analysis and parametric optimisation of box-wing aircraft for reduced fuel burn.

Degree: 2015, RMIT University

 A conceptual design analysis methodology and toolchain was developed for multidisciplinary analysis of box-wing aircraft. This methodology was applied to investigate the effect of wing… (more)

Subjects/Keywords: Fields of Research; aerospace engineering; aircraft design; multidisciplinary optimisation; box-wing; aerodynamics; aircraft structures; conceptual design; unconventional aircraft configurations

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APA (6th Edition):

Roy Salam, I. (2015). Multidisciplinary analysis and parametric optimisation of box-wing aircraft for reduced fuel burn. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161346

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):

Roy Salam, I. “Multidisciplinary analysis and parametric optimisation of box-wing aircraft for reduced fuel burn.” 2015. Thesis, RMIT University. Accessed October 16, 2019. http://researchbank.rmit.edu.au/view/rmit:161346.

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

MLA Handbook (7th Edition):

Roy Salam, I. “Multidisciplinary analysis and parametric optimisation of box-wing aircraft for reduced fuel burn.” 2015. Web. 16 Oct 2019.

Vancouver:

Roy Salam I. Multidisciplinary analysis and parametric optimisation of box-wing aircraft for reduced fuel burn. [Internet] [Thesis]. RMIT University; 2015. [cited 2019 Oct 16]. Available from: http://researchbank.rmit.edu.au/view/rmit:161346.

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

Council of Science Editors:

Roy Salam I. Multidisciplinary analysis and parametric optimisation of box-wing aircraft for reduced fuel burn. [Thesis]. RMIT University; 2015. Available from: http://researchbank.rmit.edu.au/view/rmit:161346

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


University of Florida

29. Troner, David B. Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle.

Degree: 2015, University of Florida

 With increasing growth of micro air vehicles and flexible aircraft structures, new ways to control aircraft are needed where conventional trailing edge control surfaces are… (more)

Subjects/Keywords: Aerodynamic lift; Aeroelasticity; Ailerons; Aircraft; Aircraft design; Aircraft roll; Aircraft wings; Stiffness; Structural deflection; Velocity; Aeroelasticity; aerodynamics; aircraft structures; micro air vehicle; wing twist

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APA (6th Edition):

Troner, D. B. (2015). Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle. (Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/AA00038571

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):

Troner, David B. “Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle.” 2015. Thesis, University of Florida. Accessed October 16, 2019. http://ufdc.ufl.edu/AA00038571.

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

MLA Handbook (7th Edition):

Troner, David B. “Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle.” 2015. Web. 16 Oct 2019.

Vancouver:

Troner DB. Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle. [Internet] [Thesis]. University of Florida; 2015. [cited 2019 Oct 16]. Available from: http://ufdc.ufl.edu/AA00038571.

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

Council of Science Editors:

Troner DB. Aeroelastic Analysis of Wing Twist for Roll Control of a Micro Air Vehicle. [Thesis]. University of Florida; 2015. Available from: http://ufdc.ufl.edu/AA00038571

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


Purdue University

30. Choi, Jung Hoon. Platform Design For Fleet-Level Efficiency Under Uncertain Demand: Application For Military Cargo Aircraft And Fleet.

Degree: Aeronautics and Astronautics, 2013, Purdue University

  The aircraft system's role in the United Stated Air Force is crucial. For the U.S. Air Force to maintain its air superiority in the… (more)

Subjects/Keywords: Aircraft Design; Decomposition; Fleet Level Efficiency; Military Aircraft; Resource Allocation; Aerospace Engineering

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APA (6th Edition):

Choi, J. H. (2013). Platform Design For Fleet-Level Efficiency Under Uncertain Demand: Application For Military Cargo Aircraft And Fleet. (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/28

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):

Choi, Jung Hoon. “Platform Design For Fleet-Level Efficiency Under Uncertain Demand: Application For Military Cargo Aircraft And Fleet.” 2013. Thesis, Purdue University. Accessed October 16, 2019. http://docs.lib.purdue.edu/open_access_theses/28.

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

MLA Handbook (7th Edition):

Choi, Jung Hoon. “Platform Design For Fleet-Level Efficiency Under Uncertain Demand: Application For Military Cargo Aircraft And Fleet.” 2013. Web. 16 Oct 2019.

Vancouver:

Choi JH. Platform Design For Fleet-Level Efficiency Under Uncertain Demand: Application For Military Cargo Aircraft And Fleet. [Internet] [Thesis]. Purdue University; 2013. [cited 2019 Oct 16]. Available from: http://docs.lib.purdue.edu/open_access_theses/28.

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

Council of Science Editors:

Choi JH. Platform Design For Fleet-Level Efficiency Under Uncertain Demand: Application For Military Cargo Aircraft And Fleet. [Thesis]. Purdue University; 2013. Available from: http://docs.lib.purdue.edu/open_access_theses/28

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

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