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You searched for subject:(Flapping Flight). Showing records 1 – 30 of 58 total matches.

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Virginia Tech

1. Leonard, Benjamin Yoshi. Flapping Wing Flight Dynamic Modeling.

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

 Highly agile, hover capable flapping wing flight is a relatively new area of study in engineering. Researchers are looking to flapping flight as a potential… (more)

Subjects/Keywords: Flight Dynamics; Flapping Flight

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APA (6th Edition):

Leonard, B. Y. (2011). Flapping Wing Flight Dynamic Modeling. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34790

Chicago Manual of Style (16th Edition):

Leonard, Benjamin Yoshi. “Flapping Wing Flight Dynamic Modeling.” 2011. Masters Thesis, Virginia Tech. Accessed September 19, 2019. http://hdl.handle.net/10919/34790.

MLA Handbook (7th Edition):

Leonard, Benjamin Yoshi. “Flapping Wing Flight Dynamic Modeling.” 2011. Web. 19 Sep 2019.

Vancouver:

Leonard BY. Flapping Wing Flight Dynamic Modeling. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10919/34790.

Council of Science Editors:

Leonard BY. Flapping Wing Flight Dynamic Modeling. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/34790


Indian Institute of Science

2. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: 2012, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

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APA (6th Edition):

Mukherjee, S. (2012). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2021

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):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Thesis, Indian Institute of Science. Accessed September 19, 2019. http://hdl.handle.net/2005/2021.

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

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Web. 19 Sep 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/2005/2021.

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

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2021

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


Indian Institute of Science

3. Mukherjee, Sujoy. Structural Modeling And Analysis Of Insect Scale Flapping Wing.

Degree: 2012, Indian Institute of Science

 Micro Air Vehicles (MAVs) are defined as a class of vehicles with their larger dimension not exceeding 15 cm and weighing 100 gm. The three… (more)

Subjects/Keywords: Flapping Wing; Micro Air Vehicles (MAVs); Calliphora Wing; Flapping Wings; Twisting Wing; Flapping Flight; Aeronautics

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

APA (6th Edition):

Mukherjee, S. (2012). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf

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):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Thesis, Indian Institute of Science. Accessed September 19, 2019. http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf.

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

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2012. Web. 19 Sep 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Sep 19]. Available from: http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf.

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

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2021 ; http://etd.ncsi.iisc.ernet.in/abstracts/2616/G24985-Abs.pdf

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


University of Manchester

4. Abdul Hamid, Mohd Faisal Bin. Aerodynamic models for insect flight.

Degree: 2016, University of Manchester

 Numerical models of insect flapping flight have previously been developed and used to simulate the performance of insect flight. These models were commonly developed via… (more)

Subjects/Keywords: flapping wing; insect flight; tandem wing

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APA (6th Edition):

Abdul Hamid, M. F. B. (2016). Aerodynamic models for insect flight. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191

Chicago Manual of Style (16th Edition):

Abdul Hamid, Mohd Faisal Bin. “Aerodynamic models for insect flight.” 2016. Doctoral Dissertation, University of Manchester. Accessed September 19, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191.

MLA Handbook (7th Edition):

Abdul Hamid, Mohd Faisal Bin. “Aerodynamic models for insect flight.” 2016. Web. 19 Sep 2019.

Vancouver:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Sep 19]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191.

Council of Science Editors:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:303191


Cornell University

5. Richter, Charles. Flight And Symbolic Modeling Of A 3D Printed Ornithopter .

Degree: 2012, Cornell University

 The work described in this thesis represents a set of novel solutions to several challenges involved in the design and flight of hovering ornithopters as… (more)

Subjects/Keywords: Flapping Flight; 3D Printing; Symbolic Regression

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APA (6th Edition):

Richter, C. (2012). Flight And Symbolic Modeling Of A 3D Printed Ornithopter . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/29247

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):

Richter, Charles. “Flight And Symbolic Modeling Of A 3D Printed Ornithopter .” 2012. Thesis, Cornell University. Accessed September 19, 2019. http://hdl.handle.net/1813/29247.

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

MLA Handbook (7th Edition):

Richter, Charles. “Flight And Symbolic Modeling Of A 3D Printed Ornithopter .” 2012. Web. 19 Sep 2019.

Vancouver:

Richter C. Flight And Symbolic Modeling Of A 3D Printed Ornithopter . [Internet] [Thesis]. Cornell University; 2012. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1813/29247.

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

Council of Science Editors:

Richter C. Flight And Symbolic Modeling Of A 3D Printed Ornithopter . [Thesis]. Cornell University; 2012. Available from: http://hdl.handle.net/1813/29247

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


University of Manchester

6. Abdul Hamid, Mohd Faisal. Aerodynamic models for insect flight.

Degree: PhD, 2016, University of Manchester

 Numerical models of insect flapping flight have previously been developed and used to simulate the performance of insect flight. These models were commonly developed via… (more)

Subjects/Keywords: 629.13; flapping wing; insect flight; tandem wing

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

APA (6th Edition):

Abdul Hamid, M. F. (2016). Aerodynamic models for insect flight. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093

Chicago Manual of Style (16th Edition):

Abdul Hamid, Mohd Faisal. “Aerodynamic models for insect flight.” 2016. Doctoral Dissertation, University of Manchester. Accessed September 19, 2019. https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093.

MLA Handbook (7th Edition):

Abdul Hamid, Mohd Faisal. “Aerodynamic models for insect flight.” 2016. Web. 19 Sep 2019.

Vancouver:

Abdul Hamid MF. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Sep 19]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093.

Council of Science Editors:

Abdul Hamid MF. Aerodynamic models for insect flight. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/aerodynamic-models-for-insect-flight(057be27b-265a-45a0-b8d0-dc3c02a62a77).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728093


University of California – Irvine

7. Hassan, Ahmed. Differential-Geometric-Control Formulation of Unconventional Flight Dynamics.

Degree: Mechanical and Aerospace Engineering, 2018, University of California – Irvine

 Differential-geometric control theory exploits it{differential geometry} in the analysis of dynamical control systems. Differential geometry is a mathematical discipline that is concerned with studying calculus… (more)

Subjects/Keywords: Aerospace engineering; Flapping Flight; Flight Dynamics; Nonlinear Geometric Control

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APA (6th Edition):

Hassan, A. (2018). Differential-Geometric-Control Formulation of Unconventional Flight Dynamics. (Thesis). University of California – Irvine. Retrieved from http://www.escholarship.org/uc/item/6v38v60w

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):

Hassan, Ahmed. “Differential-Geometric-Control Formulation of Unconventional Flight Dynamics.” 2018. Thesis, University of California – Irvine. Accessed September 19, 2019. http://www.escholarship.org/uc/item/6v38v60w.

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

MLA Handbook (7th Edition):

Hassan, Ahmed. “Differential-Geometric-Control Formulation of Unconventional Flight Dynamics.” 2018. Web. 19 Sep 2019.

Vancouver:

Hassan A. Differential-Geometric-Control Formulation of Unconventional Flight Dynamics. [Internet] [Thesis]. University of California – Irvine; 2018. [cited 2019 Sep 19]. Available from: http://www.escholarship.org/uc/item/6v38v60w.

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

Council of Science Editors:

Hassan A. Differential-Geometric-Control Formulation of Unconventional Flight Dynamics. [Thesis]. University of California – Irvine; 2018. Available from: http://www.escholarship.org/uc/item/6v38v60w

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


Cornell University

8. Noest, Robert Matthijs. Insect Locomotion: Control, Stability, and Optimization .

Degree: 2017, Cornell University

 In complex dynamical systems consisting of many interacting degrees of freedom it can be impossible to predict how any single one will behave. Yet, usually,… (more)

Subjects/Keywords: Physics; evolution; Chasing prey; Flapping flight; Human controlled flight; Insect behavior

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APA (6th Edition):

Noest, R. M. (2017). Insect Locomotion: Control, Stability, and Optimization . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/57002

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):

Noest, Robert Matthijs. “Insect Locomotion: Control, Stability, and Optimization .” 2017. Thesis, Cornell University. Accessed September 19, 2019. http://hdl.handle.net/1813/57002.

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

MLA Handbook (7th Edition):

Noest, Robert Matthijs. “Insect Locomotion: Control, Stability, and Optimization .” 2017. Web. 19 Sep 2019.

Vancouver:

Noest RM. Insect Locomotion: Control, Stability, and Optimization . [Internet] [Thesis]. Cornell University; 2017. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1813/57002.

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

Council of Science Editors:

Noest RM. Insect Locomotion: Control, Stability, and Optimization . [Thesis]. Cornell University; 2017. Available from: http://hdl.handle.net/1813/57002

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


Missouri University of Science and Technology

9. Rolwes, Jessica. The effect of kinematics on flapping wing performance.

Degree: M.S. in Mechanical Engineering, Mechanical Engineering, Missouri University of Science and Technology

"The objective of this work was to investigate low Reynolds number (~6,000) aerodynamics of a three-dimensional elliptical acrylic wing (~150mm x 50mm) in cyclic flapping and pitching motion by experimentally testing the effects on performance of varying wing kinematics" – Abstract, leaf iii.

Subjects/Keywords: Flapping flight; Mechanical Engineering

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APA (6th Edition):

Rolwes, J. (n.d.). The effect of kinematics on flapping wing performance. (Masters Thesis). Missouri University of Science and Technology. Retrieved from http://scholarsmine.mst.edu/masters_theses/4097

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Chicago Manual of Style (16th Edition):

Rolwes, Jessica. “The effect of kinematics on flapping wing performance.” Masters Thesis, Missouri University of Science and Technology. Accessed September 19, 2019. http://scholarsmine.mst.edu/masters_theses/4097.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

MLA Handbook (7th Edition):

Rolwes, Jessica. “The effect of kinematics on flapping wing performance.” Web. 19 Sep 2019.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Rolwes J. The effect of kinematics on flapping wing performance. [Internet] [Masters thesis]. Missouri University of Science and Technology; [cited 2019 Sep 19]. Available from: http://scholarsmine.mst.edu/masters_theses/4097.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Council of Science Editors:

Rolwes J. The effect of kinematics on flapping wing performance. [Masters Thesis]. Missouri University of Science and Technology; Available from: http://scholarsmine.mst.edu/masters_theses/4097

Note: this citation may be lacking information needed for this citation format:
No year of publication.


University of Manchester

10. Parslew, Ben. Simulating avian wingbeats and wakes.

Degree: PhD, 2012, University of Manchester

 Analytical models of avian flight have previously been used to predict mechanical and metabolic power consumption during cruise. These models are limited, in that they… (more)

Subjects/Keywords: 598; Avian; Predictive simulation; Flapping; Wake; Bird flight; Inverse dynamics

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

APA (6th Edition):

Parslew, B. (2012). Simulating avian wingbeats and wakes. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489

Chicago Manual of Style (16th Edition):

Parslew, Ben. “Simulating avian wingbeats and wakes.” 2012. Doctoral Dissertation, University of Manchester. Accessed September 19, 2019. https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489.

MLA Handbook (7th Edition):

Parslew, Ben. “Simulating avian wingbeats and wakes.” 2012. Web. 19 Sep 2019.

Vancouver:

Parslew B. Simulating avian wingbeats and wakes. [Internet] [Doctoral dissertation]. University of Manchester; 2012. [cited 2019 Sep 19]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489.

Council of Science Editors:

Parslew B. Simulating avian wingbeats and wakes. [Doctoral Dissertation]. University of Manchester; 2012. Available from: https://www.research.manchester.ac.uk/portal/en/theses/simulating-avian-wingbeats-and-wakes(038035c2-fe9e-4104-92dc-544579c7011b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553489


UCLA

11. Medina, Albert. The Aerodynamics of Deforming Wings at Low Reynolds Number.

Degree: Mechanical Engineering, 2013, UCLA

Flapping flight has gained much attention in the past decade driven by the desire to understand capabilities observed in nature and the desire to develop… (more)

Subjects/Keywords: Mechanical engineering; Flapping flight; Flexible wings; Unsteady aerodynamics

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

APA (6th Edition):

Medina, A. (2013). The Aerodynamics of Deforming Wings at Low Reynolds Number. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/0s824546

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):

Medina, Albert. “The Aerodynamics of Deforming Wings at Low Reynolds Number.” 2013. Thesis, UCLA. Accessed September 19, 2019. http://www.escholarship.org/uc/item/0s824546.

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

MLA Handbook (7th Edition):

Medina, Albert. “The Aerodynamics of Deforming Wings at Low Reynolds Number.” 2013. Web. 19 Sep 2019.

Vancouver:

Medina A. The Aerodynamics of Deforming Wings at Low Reynolds Number. [Internet] [Thesis]. UCLA; 2013. [cited 2019 Sep 19]. Available from: http://www.escholarship.org/uc/item/0s824546.

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

Council of Science Editors:

Medina A. The Aerodynamics of Deforming Wings at Low Reynolds Number. [Thesis]. UCLA; 2013. Available from: http://www.escholarship.org/uc/item/0s824546

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

12. 井村, 忠継. 無尾翼・小型羽ばたき飛翔体の開発と飛翔に及ぼす翅挙動の影響に関する研究 : The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight.

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

九州工業大学博士学位論文 学位記番号:情工博甲第268号 学位授与年月日:平成24年9月30日

第1章 序論|第2章 無尾翼・羽ばたき飛翔体の開発|第3章 開発した飛翔体の翅の挙動と飛翔|第4章 無尾翼・小型羽ばたき飛翔体の持つ諸パラメータとその飛翔特性|第5章 飛翔モデルの構築とその妥当性の検討および飛翔に必要な条件|第6章 結言

平成24年度

Advisors/Committee Members: 田中, 和博.

Subjects/Keywords: Flapping robot; Small robot; Tailless; Body angle; Flight characteristics

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

APA (6th Edition):

井村, . (2017). 無尾翼・小型羽ばたき飛翔体の開発と飛翔に及ぼす翅挙動の影響に関する研究 : The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight. (Thesis). Kyushu Institute of Technology / 九州工業大学. Retrieved from http://hdl.handle.net/10228/4948

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):

井村, 忠継. “無尾翼・小型羽ばたき飛翔体の開発と飛翔に及ぼす翅挙動の影響に関する研究 : The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight.” 2017. Thesis, Kyushu Institute of Technology / 九州工業大学. Accessed September 19, 2019. http://hdl.handle.net/10228/4948.

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

MLA Handbook (7th Edition):

井村, 忠継. “無尾翼・小型羽ばたき飛翔体の開発と飛翔に及ぼす翅挙動の影響に関する研究 : The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight.” 2017. Web. 19 Sep 2019.

Vancouver:

井村 . 無尾翼・小型羽ばたき飛翔体の開発と飛翔に及ぼす翅挙動の影響に関する研究 : The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight. [Internet] [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10228/4948.

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

Council of Science Editors:

井村 . 無尾翼・小型羽ばたき飛翔体の開発と飛翔に及ぼす翅挙動の影響に関する研究 : The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight. [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. Available from: http://hdl.handle.net/10228/4948

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


Harvard University

13. Chirarattananon, Pakpong. Flight Control of a Millimeter-Scale Flapping-Wing Robot.

Degree: PhD, Engineering and Applied Sciences, 2014, Harvard University

Flying insects display remarkable maneuverability. Unlike typical airplanes, these insects are able to execute an evasive action, rapidly change their flight speed and direction, or… (more)

Subjects/Keywords: Engineering; Electrical engineering; Control; Flapping-wing; Flight; Robot

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APA (6th Edition):

Chirarattananon, P. (2014). Flight Control of a Millimeter-Scale Flapping-Wing Robot. (Doctoral Dissertation). Harvard University. Retrieved from http://nrs.harvard.edu/urn-3:HUL.InstRepos:13070057

Chicago Manual of Style (16th Edition):

Chirarattananon, Pakpong. “Flight Control of a Millimeter-Scale Flapping-Wing Robot.” 2014. Doctoral Dissertation, Harvard University. Accessed September 19, 2019. http://nrs.harvard.edu/urn-3:HUL.InstRepos:13070057.

MLA Handbook (7th Edition):

Chirarattananon, Pakpong. “Flight Control of a Millimeter-Scale Flapping-Wing Robot.” 2014. Web. 19 Sep 2019.

Vancouver:

Chirarattananon P. Flight Control of a Millimeter-Scale Flapping-Wing Robot. [Internet] [Doctoral dissertation]. Harvard University; 2014. [cited 2019 Sep 19]. Available from: http://nrs.harvard.edu/urn-3:HUL.InstRepos:13070057.

Council of Science Editors:

Chirarattananon P. Flight Control of a Millimeter-Scale Flapping-Wing Robot. [Doctoral Dissertation]. Harvard University; 2014. Available from: http://nrs.harvard.edu/urn-3:HUL.InstRepos:13070057


Washington University in St. Louis

14. Li, Hang. Aerodynamics and Vortex Structures of a Flapping Airfoil in Forward Flight in Proximity of Ground.

Degree: MS, Mechanical Engineering & Materials Science, 2017, Washington University in St. Louis

  The traditional flapping wing high lift mechanism research mainly focuses on the wing in unbounded flow. However, the real insect flight includes not only… (more)

Subjects/Keywords: Flapping forward flight vortex ground effect; Aerodynamics and Fluid Mechanics; Engineering

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APA (6th Edition):

Li, H. (2017). Aerodynamics and Vortex Structures of a Flapping Airfoil in Forward Flight in Proximity of Ground. (Thesis). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/eng_etds/266

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):

Li, Hang. “Aerodynamics and Vortex Structures of a Flapping Airfoil in Forward Flight in Proximity of Ground.” 2017. Thesis, Washington University in St. Louis. Accessed September 19, 2019. https://openscholarship.wustl.edu/eng_etds/266.

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

MLA Handbook (7th Edition):

Li, Hang. “Aerodynamics and Vortex Structures of a Flapping Airfoil in Forward Flight in Proximity of Ground.” 2017. Web. 19 Sep 2019.

Vancouver:

Li H. Aerodynamics and Vortex Structures of a Flapping Airfoil in Forward Flight in Proximity of Ground. [Internet] [Thesis]. Washington University in St. Louis; 2017. [cited 2019 Sep 19]. Available from: https://openscholarship.wustl.edu/eng_etds/266.

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

Council of Science Editors:

Li H. Aerodynamics and Vortex Structures of a Flapping Airfoil in Forward Flight in Proximity of Ground. [Thesis]. Washington University in St. Louis; 2017. Available from: https://openscholarship.wustl.edu/eng_etds/266

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


Virginia Tech

15. Murphy, Ian Patrick. Modeling and Control of Flapping Wing Robots.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 The study of fixed wing aeronautical engineering has matured to the point where years of research result in small performance improvements.  In the past decade,… (more)

Subjects/Keywords: Flapping Flight; Robotic Modeling; Nonlinear Control; Adaptive Control

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APA (6th Edition):

Murphy, I. P. (2013). Modeling and Control of Flapping Wing Robots. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/19275

Chicago Manual of Style (16th Edition):

Murphy, Ian Patrick. “Modeling and Control of Flapping Wing Robots.” 2013. Masters Thesis, Virginia Tech. Accessed September 19, 2019. http://hdl.handle.net/10919/19275.

MLA Handbook (7th Edition):

Murphy, Ian Patrick. “Modeling and Control of Flapping Wing Robots.” 2013. Web. 19 Sep 2019.

Vancouver:

Murphy IP. Modeling and Control of Flapping Wing Robots. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10919/19275.

Council of Science Editors:

Murphy IP. Modeling and Control of Flapping Wing Robots. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/19275


Cornell University

16. Chang, Song. Stability And Control Of Flapping Flight: Modeling, Simulation, And Analysis .

Degree: 2013, Cornell University

 We study the stability and control of flapping flight of insects. To quantify the stability and to assess the control, we build a 3D dynamic… (more)

Subjects/Keywords: flapping flight; pitching instability; dynamic stability and neural control

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APA (6th Edition):

Chang, S. (2013). Stability And Control Of Flapping Flight: Modeling, Simulation, And Analysis . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/34350

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):

Chang, Song. “Stability And Control Of Flapping Flight: Modeling, Simulation, And Analysis .” 2013. Thesis, Cornell University. Accessed September 19, 2019. http://hdl.handle.net/1813/34350.

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

MLA Handbook (7th Edition):

Chang, Song. “Stability And Control Of Flapping Flight: Modeling, Simulation, And Analysis .” 2013. Web. 19 Sep 2019.

Vancouver:

Chang S. Stability And Control Of Flapping Flight: Modeling, Simulation, And Analysis . [Internet] [Thesis]. Cornell University; 2013. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1813/34350.

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

Council of Science Editors:

Chang S. Stability And Control Of Flapping Flight: Modeling, Simulation, And Analysis . [Thesis]. Cornell University; 2013. Available from: http://hdl.handle.net/1813/34350

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


Cornell University

17. Melfi Jr., James. Flight Mechanics Of The Dragonfly .

Degree: 2016, Cornell University

Subjects/Keywords: Biomechanics; Dynamics; Flapping Flight

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APA (6th Edition):

Melfi Jr., J. (2016). Flight Mechanics Of The Dragonfly . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/45221

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):

Melfi Jr., James. “Flight Mechanics Of The Dragonfly .” 2016. Thesis, Cornell University. Accessed September 19, 2019. http://hdl.handle.net/1813/45221.

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

MLA Handbook (7th Edition):

Melfi Jr., James. “Flight Mechanics Of The Dragonfly .” 2016. Web. 19 Sep 2019.

Vancouver:

Melfi Jr. J. Flight Mechanics Of The Dragonfly . [Internet] [Thesis]. Cornell University; 2016. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1813/45221.

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

Council of Science Editors:

Melfi Jr. J. Flight Mechanics Of The Dragonfly . [Thesis]. Cornell University; 2016. Available from: http://hdl.handle.net/1813/45221

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


University of New South Wales

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Tobing, Sheila. “Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies.” 2014. Doctoral Dissertation, University of New South Wales. Accessed September 19, 2019. http://handle.unsw.edu.au/1959.4/53832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12545/SOURCE01?view=true.

MLA Handbook (7th Edition):

Tobing, Sheila. “Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies.” 2014. Web. 19 Sep 2019.

Vancouver:

Tobing S. Numerical Analysis of Effects of Aeroelasticity on Flapping-wing Propulsion: Case Study of Bumblebees and Hoverflies. [Internet] [Doctoral dissertation]. University of New South Wales; 2014. [cited 2019 Sep 19]. Available from: http://handle.unsw.edu.au/1959.4/53832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12545/SOURCE01?view=true.

Council of Science Editors:

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


Brigham Young University

19. George, Ryan Brandon. Design and Analysis of a Flapping Wing Mechanism for Optimization.

Degree: MS, 2011, Brigham Young University

 Furthering our understanding of the physics of flapping flight has the potential to benefit the field of micro air vehicles. Advancements in micro air vehicles… (more)

Subjects/Keywords: flapping flight; flapping mechanism; ladybug; direct linear transformation; Box-Behnken; response surface optimization; flight; micro-air vehicle; biologically-inspired flight; Mechanical Engineering

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APA (6th Edition):

George, R. B. (2011). Design and Analysis of a Flapping Wing Mechanism for Optimization. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3736&context=etd

Chicago Manual of Style (16th Edition):

George, Ryan Brandon. “Design and Analysis of a Flapping Wing Mechanism for Optimization.” 2011. Masters Thesis, Brigham Young University. Accessed September 19, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3736&context=etd.

MLA Handbook (7th Edition):

George, Ryan Brandon. “Design and Analysis of a Flapping Wing Mechanism for Optimization.” 2011. Web. 19 Sep 2019.

Vancouver:

George RB. Design and Analysis of a Flapping Wing Mechanism for Optimization. [Internet] [Masters thesis]. Brigham Young University; 2011. [cited 2019 Sep 19]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3736&context=etd.

Council of Science Editors:

George RB. Design and Analysis of a Flapping Wing Mechanism for Optimization. [Masters Thesis]. Brigham Young University; 2011. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3736&context=etd


Brigham Young University

20. Naegle, Nathaniel Stephen. Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism.

Degree: MS, 2012, Brigham Young University

Flapping flight shows promise for micro air vehicle design because flapping wings provide superior aerodynamic performance than that of fixed wings and rotors at… (more)

Subjects/Keywords: flapping flight; flapping mechanism; water tunnel; hawkmoth; Box-Behnken; particle image velocimetry; PIV; flow characterization; micro-air vehicles; MAV; Mechanical Engineering

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APA (6th Edition):

Naegle, N. S. (2012). Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd

Chicago Manual of Style (16th Edition):

Naegle, Nathaniel Stephen. “Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism.” 2012. Masters Thesis, Brigham Young University. Accessed September 19, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd.

MLA Handbook (7th Edition):

Naegle, Nathaniel Stephen. “Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism.” 2012. Web. 19 Sep 2019.

Vancouver:

Naegle NS. Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism. [Internet] [Masters thesis]. Brigham Young University; 2012. [cited 2019 Sep 19]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd.

Council of Science Editors:

Naegle NS. Force Optimization and Flow Field Characterization from a Flapping Wing Mechanism. [Masters Thesis]. Brigham Young University; 2012. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4277&context=etd

21. TAY WEE BENG. Dynamics and control of a flapping wing aircraft.

Degree: 2004, National University of Singapore

Subjects/Keywords: flapping wing ornithopter membrane bird flight

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APA (6th Edition):

BENG, T. W. (2004). Dynamics and control of a flapping wing aircraft. (Thesis). National University of Singapore. Retrieved from http://scholarbank.nus.edu.sg/handle/10635/14174

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):

BENG, TAY WEE. “Dynamics and control of a flapping wing aircraft.” 2004. Thesis, National University of Singapore. Accessed September 19, 2019. http://scholarbank.nus.edu.sg/handle/10635/14174.

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

MLA Handbook (7th Edition):

BENG, TAY WEE. “Dynamics and control of a flapping wing aircraft.” 2004. Web. 19 Sep 2019.

Vancouver:

BENG TW. Dynamics and control of a flapping wing aircraft. [Internet] [Thesis]. National University of Singapore; 2004. [cited 2019 Sep 19]. Available from: http://scholarbank.nus.edu.sg/handle/10635/14174.

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

Council of Science Editors:

BENG TW. Dynamics and control of a flapping wing aircraft. [Thesis]. National University of Singapore; 2004. Available from: http://scholarbank.nus.edu.sg/handle/10635/14174

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


Brigham Young University

22. Duffield, Michael Luke. Variable Fidelity Optimization with Hardware-in-the-Loop for Flapping Flight.

Degree: MS, 2013, Brigham Young University

 Hardware-in-the-loop (HIL) modeling is a powerful way of modeling complicated systems. However, some hardware is expensive to use in terms of time or mechanical wear.… (more)

Subjects/Keywords: variable fidelity optimization; hardware-in-the-loop modeling; flapping flight; Mechanical Engineering

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APA (6th Edition):

Duffield, M. L. (2013). Variable Fidelity Optimization with Hardware-in-the-Loop for Flapping Flight. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4730&context=etd

Chicago Manual of Style (16th Edition):

Duffield, Michael Luke. “Variable Fidelity Optimization with Hardware-in-the-Loop for Flapping Flight.” 2013. Masters Thesis, Brigham Young University. Accessed September 19, 2019. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4730&context=etd.

MLA Handbook (7th Edition):

Duffield, Michael Luke. “Variable Fidelity Optimization with Hardware-in-the-Loop for Flapping Flight.” 2013. Web. 19 Sep 2019.

Vancouver:

Duffield ML. Variable Fidelity Optimization with Hardware-in-the-Loop for Flapping Flight. [Internet] [Masters thesis]. Brigham Young University; 2013. [cited 2019 Sep 19]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4730&context=etd.

Council of Science Editors:

Duffield ML. Variable Fidelity Optimization with Hardware-in-the-Loop for Flapping Flight. [Masters Thesis]. Brigham Young University; 2013. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=4730&context=etd


Virginia Tech

23. Viswanath, Kamal. Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat.

Degree: PhD, Mechanical Engineering, 2013, Virginia Tech

 This dissertation broadly seeks to understand the effect different kinematic parameters, external forces, and dynamic wing conformation have on the fluid dynamics of flapping flight.… (more)

Subjects/Keywords: Computational fluid dynamics (CFD); Flapping Flight; Micro Air Vehicles; Flexible Wings; Bat Flight; Wind Gusts; Stroke Deviation

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APA (6th Edition):

Viswanath, K. (2013). Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50825

Chicago Manual of Style (16th Edition):

Viswanath, Kamal. “Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat.” 2013. Doctoral Dissertation, Virginia Tech. Accessed September 19, 2019. http://hdl.handle.net/10919/50825.

MLA Handbook (7th Edition):

Viswanath, Kamal. “Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat.” 2013. Web. 19 Sep 2019.

Vancouver:

Viswanath K. Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10919/50825.

Council of Science Editors:

Viswanath K. Effect of frontal gusts and stroke deviation in forward flapping flight and deconstructing the aerodynamics of a fruit bat. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/50825


Purdue University

24. Musick, Stephen J. Design and Analysis of a Cable-Driven Test Apparatus for Flapping-Flight Research.

Degree: MS, Mechanical Engineering, 2014, Purdue University

  The biology, physiology, kinematics, and aerodynamics of insect flight have been a longstanding fascination for biologists and engineers. The former three are easily obtained… (more)

Subjects/Keywords: Communication and the arts; Applied sciences; Bio-robotics; Cable-driven design; Flapping-flight; Mechanical Engineering; Robotics

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APA (6th Edition):

Musick, S. J. (2014). Design and Analysis of a Cable-Driven Test Apparatus for Flapping-Flight Research. (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/357

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):

Musick, Stephen J. “Design and Analysis of a Cable-Driven Test Apparatus for Flapping-Flight Research.” 2014. Thesis, Purdue University. Accessed September 19, 2019. http://docs.lib.purdue.edu/open_access_theses/357.

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

MLA Handbook (7th Edition):

Musick, Stephen J. “Design and Analysis of a Cable-Driven Test Apparatus for Flapping-Flight Research.” 2014. Web. 19 Sep 2019.

Vancouver:

Musick SJ. Design and Analysis of a Cable-Driven Test Apparatus for Flapping-Flight Research. [Internet] [Thesis]. Purdue University; 2014. [cited 2019 Sep 19]. Available from: http://docs.lib.purdue.edu/open_access_theses/357.

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

Council of Science Editors:

Musick SJ. Design and Analysis of a Cable-Driven Test Apparatus for Flapping-Flight Research. [Thesis]. Purdue University; 2014. Available from: http://docs.lib.purdue.edu/open_access_theses/357

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


University of Washington

25. Jankauski, Mark Andrew. Dynamic Modeling of Insect Flight Mechanisms.

Degree: PhD, 2017, University of Washington

 A dynamic model of an insect wing is developed treating the wing as a deformable body subject to three-dimensional finite rotation about a fixed point… (more)

Subjects/Keywords: Flapping wings; Hawkmoth; Inertial steering; Insect flight; Micro Air Vehicles; Rotational dynamics; Mechanical engineering; Mechanical engineering

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APA (6th Edition):

Jankauski, M. A. (2017). Dynamic Modeling of Insect Flight Mechanisms. (Doctoral Dissertation). University of Washington. Retrieved from http://hdl.handle.net/1773/38660

Chicago Manual of Style (16th Edition):

Jankauski, Mark Andrew. “Dynamic Modeling of Insect Flight Mechanisms.” 2017. Doctoral Dissertation, University of Washington. Accessed September 19, 2019. http://hdl.handle.net/1773/38660.

MLA Handbook (7th Edition):

Jankauski, Mark Andrew. “Dynamic Modeling of Insect Flight Mechanisms.” 2017. Web. 19 Sep 2019.

Vancouver:

Jankauski MA. Dynamic Modeling of Insect Flight Mechanisms. [Internet] [Doctoral dissertation]. University of Washington; 2017. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/1773/38660.

Council of Science Editors:

Jankauski MA. Dynamic Modeling of Insect Flight Mechanisms. [Doctoral Dissertation]. University of Washington; 2017. Available from: http://hdl.handle.net/1773/38660

26. Mikkelsen, Markus. Development, Modelling and Control of a Multirotor Vehicle.

Degree: Applied Physics and Electronics, 2015, Umeå University

  The interest of drones in all forms has exploded in the recent years. The development of multirotor vehicles such as quadcopters and octocopters, has… (more)

Subjects/Keywords: Multirotor; Octocopter; Blade flapping; Induced drag; Gyroscopic torque; Drone; Modelling; Control; Code generation; Raspberry Pi; Matlab; Simulink; Simulations; Flight tests

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APA (6th Edition):

Mikkelsen, M. (2015). Development, Modelling and Control of a Multirotor Vehicle. (Thesis). Umeå University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889

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):

Mikkelsen, Markus. “Development, Modelling and Control of a Multirotor Vehicle.” 2015. Thesis, Umeå University. Accessed September 19, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889.

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

MLA Handbook (7th Edition):

Mikkelsen, Markus. “Development, Modelling and Control of a Multirotor Vehicle.” 2015. Web. 19 Sep 2019.

Vancouver:

Mikkelsen M. Development, Modelling and Control of a Multirotor Vehicle. [Internet] [Thesis]. Umeå University; 2015. [cited 2019 Sep 19]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889.

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

Council of Science Editors:

Mikkelsen M. Development, Modelling and Control of a Multirotor Vehicle. [Thesis]. Umeå University; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-110889

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


University of California – Irvine

27. Kiani, Mohammadali. Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight.

Degree: Mechanical and Aerospace Engineering, 2018, University of California – Irvine

Flapping wing micro-air-vehicles (FWMAV) are micro-air-vehicles that use biomimetic actuation (oscillatory flapping wing) for lift, propulsion, and control. The dynamic behavior of these bio-inspired systems… (more)

Subjects/Keywords: Mechanical engineering; Aerial Systems: Mechanics and Control; Bio-inspired flight; Biomimetics; Dynamics; Flapping wing micro air vehicle; Vibrational stability

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APA (6th Edition):

Kiani, M. (2018). Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight. (Thesis). University of California – Irvine. Retrieved from http://www.escholarship.org/uc/item/8vg5j1kk

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):

Kiani, Mohammadali. “Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight.” 2018. Thesis, University of California – Irvine. Accessed September 19, 2019. http://www.escholarship.org/uc/item/8vg5j1kk.

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

MLA Handbook (7th Edition):

Kiani, Mohammadali. “Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight.” 2018. Web. 19 Sep 2019.

Vancouver:

Kiani M. Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight. [Internet] [Thesis]. University of California – Irvine; 2018. [cited 2019 Sep 19]. Available from: http://www.escholarship.org/uc/item/8vg5j1kk.

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

Council of Science Editors:

Kiani M. Experimental Demonstration of the Vibrational Stability Phenomenon in Bio-inspired Flight. [Thesis]. University of California – Irvine; 2018. Available from: http://www.escholarship.org/uc/item/8vg5j1kk

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

28. Song, Jialei. Computational modeling of unsteady aerodynamics in hummingbird flight.

Degree: PhD, Mechanical Engineering, 2016, Vanderbilt University

 The flapping wings of flyers in nature such as birds, insects, and bats have recently attracted engineers' interest because of their applications in biomimetic and… (more)

Subjects/Keywords: hummingbird; animal flight; unsteady aerodynamics; flapping wing

…40 3.11 Comparison of the wing tip velocity between the flapping wing of the revolving wing… …x28;a) downstroke; (b) upstroke. Note that for the flapping wing, the wing… …function. 43 3.12 The revolving wing versus the flapping wing in the production of lift. (… …flapping motion of the entire wing. (b) The corresponding power for flapping motion of… …113 6.17 Force production of upstroke during forward flight. (a) Backward-flick by… 

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

APA (6th Edition):

Song, J. (2016). Computational modeling of unsteady aerodynamics in hummingbird flight. (Doctoral Dissertation). Vanderbilt University. Retrieved from http://etd.library.vanderbilt.edu/available/etd-01192016-100906/ ;

Chicago Manual of Style (16th Edition):

Song, Jialei. “Computational modeling of unsteady aerodynamics in hummingbird flight.” 2016. Doctoral Dissertation, Vanderbilt University. Accessed September 19, 2019. http://etd.library.vanderbilt.edu/available/etd-01192016-100906/ ;.

MLA Handbook (7th Edition):

Song, Jialei. “Computational modeling of unsteady aerodynamics in hummingbird flight.” 2016. Web. 19 Sep 2019.

Vancouver:

Song J. Computational modeling of unsteady aerodynamics in hummingbird flight. [Internet] [Doctoral dissertation]. Vanderbilt University; 2016. [cited 2019 Sep 19]. Available from: http://etd.library.vanderbilt.edu/available/etd-01192016-100906/ ;.

Council of Science Editors:

Song J. Computational modeling of unsteady aerodynamics in hummingbird flight. [Doctoral Dissertation]. Vanderbilt University; 2016. Available from: http://etd.library.vanderbilt.edu/available/etd-01192016-100906/ ;


North Carolina State University

29. McGowan, Gregory Zar. Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers.

Degree: PhD, Aerospace Engineering, 2008, North Carolina State University

 Current interests in Micro Air Vehicle (MAV)technologies call for the development of aerodynamic-design tools that will aid in the design of more efficient platforms that… (more)

Subjects/Keywords: unsteady aerodynamics; airfoil; CFD; flapping flight; low Reynolds number

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APA (6th Edition):

McGowan, G. Z. (2008). Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/5678

Chicago Manual of Style (16th Edition):

McGowan, Gregory Zar. “Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers.” 2008. Doctoral Dissertation, North Carolina State University. Accessed September 19, 2019. http://www.lib.ncsu.edu/resolver/1840.16/5678.

MLA Handbook (7th Edition):

McGowan, Gregory Zar. “Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers.” 2008. Web. 19 Sep 2019.

Vancouver:

McGowan GZ. Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers. [Internet] [Doctoral dissertation]. North Carolina State University; 2008. [cited 2019 Sep 19]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5678.

Council of Science Editors:

McGowan GZ. Analytical and Computational Investigations of Airfoils Undergoing High-Frequency Sinusoidal Pitch and Plunge Motions at Low Reynolds Numbers. [Doctoral Dissertation]. North Carolina State University; 2008. Available from: http://www.lib.ncsu.edu/resolver/1840.16/5678


Virginia Tech

30. Taha, Haithem Ezzat Mohammed. Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics and Control.

Degree: PhD, Engineering Science and Mechanics, 2013, Virginia Tech

 A flapping-wing micro-air-vehicle (FWMAV) represents a complex multi-disciplinary system whose analysis invokes the frontiers of the aerospace engineering disciplines. From the aerodynamic point of view,… (more)

Subjects/Keywords: Flapping Flight; Finite-State Unsteady Aerodynamics; Calculus of Variations and Optimal Control; Flight Dynamics; Nonlinear Time-Periodic Systems; Averaging Theorem; Geometric Control; Nonlinear Dynamics and Saturation

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

APA (6th Edition):

Taha, H. E. M. (2013). Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics and Control. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24428

Chicago Manual of Style (16th Edition):

Taha, Haithem Ezzat Mohammed. “Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics and Control.” 2013. Doctoral Dissertation, Virginia Tech. Accessed September 19, 2019. http://hdl.handle.net/10919/24428.

MLA Handbook (7th Edition):

Taha, Haithem Ezzat Mohammed. “Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics and Control.” 2013. Web. 19 Sep 2019.

Vancouver:

Taha HEM. Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics and Control. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2019 Sep 19]. Available from: http://hdl.handle.net/10919/24428.

Council of Science Editors:

Taha HEM. Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics and Control. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/24428

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