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You searched for subject:(wing). Showing records 1 – 30 of 972 total matches.

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Texas A&M University

1. Cooper, Jacob. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 This dissertation investigates high angle of attack delta wing flow at multiple resolutions of turbulence closure. The work is divided into four studies. The objectives… (more)

Subjects/Keywords: delta wing; diamond wing; turbulence model; PANS

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APA (6th Edition):

Cooper, J. (2014). Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153426

Chicago Manual of Style (16th Edition):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Doctoral Dissertation, Texas A&M University. Accessed January 25, 2021. http://hdl.handle.net/1969.1/153426.

MLA Handbook (7th Edition):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Web. 25 Jan 2021.

Vancouver:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1969.1/153426.

Council of Science Editors:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153426


NSYSU

2. Pan, Chih-Hong. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism.

Degree: Master, Political Science, 2018, NSYSU

 With the theme of " why did Taiwan not yet have a strong left-wing party?", this paper analyzes the factors behind it and also analyzes… (more)

Subjects/Keywords: class consciousness; left-wing; left-wing party

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APA (6th Edition):

Pan, C. (2018). A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150

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):

Pan, Chih-Hong. “A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism.” 2018. Thesis, NSYSU. Accessed January 25, 2021. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150.

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

MLA Handbook (7th Edition):

Pan, Chih-Hong. “A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism.” 2018. Web. 25 Jan 2021.

Vancouver:

Pan C. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. [Internet] [Thesis]. NSYSU; 2018. [cited 2021 Jan 25]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150.

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

Council of Science Editors:

Pan C. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. [Thesis]. NSYSU; 2018. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0702118-104150

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


University of Manchester

3. 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 (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 January 25, 2021. 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. 25 Jan 2021.

Vancouver:

Abdul Hamid MF. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Jan 25]. 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 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 January 25, 2021. 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. 25 Jan 2021.

Vancouver:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Jan 25]. 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


University of Kansas

5. Brown, Matthew Alan. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.

Degree: MS, Aerospace Engineering, 2013, University of Kansas

 The methods presented in this work are intended to provided an easy to understand and easy to apply method for determining the distributed aerodynamic loads… (more)

Subjects/Keywords: Aerospace engineering; Aerodyanmic loads; Cranked wing; Wing aerodyanmics; Wing loads

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APA (6th Edition):

Brown, M. A. (2013). A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/14195

Chicago Manual of Style (16th Edition):

Brown, Matthew Alan. “A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.” 2013. Masters Thesis, University of Kansas. Accessed January 25, 2021. http://hdl.handle.net/1808/14195.

MLA Handbook (7th Edition):

Brown, Matthew Alan. “A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.” 2013. Web. 25 Jan 2021.

Vancouver:

Brown MA. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. [Internet] [Masters thesis]. University of Kansas; 2013. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1808/14195.

Council of Science Editors:

Brown MA. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. [Masters Thesis]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/14195


Linköping University

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

Degree: Machine Design, 2011, Linköping University

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

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

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APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

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

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

MLA Handbook (7th Edition):

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

Vancouver:

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

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

Council of Science Editors:

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

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


Carnegie Mellon University

7. Colmenares, David. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight.

Degree: 2017, Carnegie Mellon University

 Small scale unmanned aircraft, such as quadrotors, that are quickly emerging as versatile tools for a wide range of applications including search and rescue, hazardous… (more)

Subjects/Keywords: Micro Aerial Vehicle; Flapping wing; Resonant Actuator; DC motor; Thermal Model; Flexible Wing; Wing Twist

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APA (6th Edition):

Colmenares, D. (2017). Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. (Thesis). Carnegie Mellon University. Retrieved from http://repository.cmu.edu/dissertations/1032

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):

Colmenares, David. “Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight.” 2017. Thesis, Carnegie Mellon University. Accessed January 25, 2021. http://repository.cmu.edu/dissertations/1032.

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

MLA Handbook (7th Edition):

Colmenares, David. “Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight.” 2017. Web. 25 Jan 2021.

Vancouver:

Colmenares D. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. [Internet] [Thesis]. Carnegie Mellon University; 2017. [cited 2021 Jan 25]. Available from: http://repository.cmu.edu/dissertations/1032.

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

Council of Science Editors:

Colmenares D. Design and Control of a Resonant, Flapping Wing Micro Aerial Vehicle Capable of Controlled Flight. [Thesis]. Carnegie Mellon University; 2017. Available from: http://repository.cmu.edu/dissertations/1032

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


University of Manchester

8. El Ouardi, Othman. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.

Degree: 2014, University of Manchester

Wing morphing has the potential to significantly improve the performance of an aircraft. The aerospace industry currently relies on control surfaces for changing aircraft wing(more)

Subjects/Keywords: Morphing wing; Adaptive wing; SMA; Variable thickness wing; Shape morphing; Smart materials

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APA (6th Edition):

El Ouardi, O. (2014). Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682

Chicago Manual of Style (16th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Doctoral Dissertation, University of Manchester. Accessed January 25, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

MLA Handbook (7th Edition):

El Ouardi, Othman. “Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism.” 2014. Web. 25 Jan 2021.

Vancouver:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2021 Jan 25]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682.

Council of Science Editors:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:237682


Indian Institute of Science

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

Degree: PhD, Faculty of Engineering, 2013, 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. (2013). Structural Modeling And Analysis Of Insect Scale Flapping Wing. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2021

Chicago Manual of Style (16th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2013. Doctoral Dissertation, Indian Institute of Science. Accessed January 25, 2021. http://etd.iisc.ac.in/handle/2005/2021.

MLA Handbook (7th Edition):

Mukherjee, Sujoy. “Structural Modeling And Analysis Of Insect Scale Flapping Wing.” 2013. Web. 25 Jan 2021.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2013. [cited 2021 Jan 25]. Available from: http://etd.iisc.ac.in/handle/2005/2021.

Council of Science Editors:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Doctoral Dissertation]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ac.in/handle/2005/2021


University of Rochester

10. Loehlin, David Walker (1981 - ); Werren, John H. Genetics of size and shape evolution in Nasonia.

Degree: PhD, 2012, University of Rochester

 My research addresses a fundamental question in biology: What genes and genetic changes are responsible for size and shape differences between species? In Chapter 1,… (more)

Subjects/Keywords: Doublesex; Morphology; Unpaired; Wing

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APA (6th Edition):

Loehlin, David Walker (1981 - ); Werren, J. H. (2012). Genetics of size and shape evolution in Nasonia. (Doctoral Dissertation). University of Rochester. Retrieved from http://hdl.handle.net/1802/19345

Chicago Manual of Style (16th Edition):

Loehlin, David Walker (1981 - ); Werren, John H. “Genetics of size and shape evolution in Nasonia.” 2012. Doctoral Dissertation, University of Rochester. Accessed January 25, 2021. http://hdl.handle.net/1802/19345.

MLA Handbook (7th Edition):

Loehlin, David Walker (1981 - ); Werren, John H. “Genetics of size and shape evolution in Nasonia.” 2012. Web. 25 Jan 2021.

Vancouver:

Loehlin, David Walker (1981 - ); Werren JH. Genetics of size and shape evolution in Nasonia. [Internet] [Doctoral dissertation]. University of Rochester; 2012. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/1802/19345.

Council of Science Editors:

Loehlin, David Walker (1981 - ); Werren JH. Genetics of size and shape evolution in Nasonia. [Doctoral Dissertation]. University of Rochester; 2012. Available from: http://hdl.handle.net/1802/19345


Delft University of Technology

11. Riahi, G. (author). Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure.

Degree: 2012, Delft University of Technology

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

Subjects/Keywords: nonlinear; finite; wing structure

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Riahi, G (author). “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure.” 2012. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

MLA Handbook (7th Edition):

Riahi, G (author). “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure.” 2012. Web. 25 Jan 2021.

Vancouver:

Riahi G(. Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

Council of Science Editors:

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


Delft University of Technology

12. Rousseau, Rob (author). Semi-Analytical Closed-Wing Weight Estimation during Conceptual Design.

Degree: 2017, Delft University of Technology

 One of the novel configurations that could revolutionize the aviation industry is the PrandtlPlane. The closed-wing design features a low front wing and a high… (more)

Subjects/Keywords: Weight-Estimation; Closed-Wing; PrandtlPlane

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APA (6th Edition):

Rousseau, R. (. (2017). Semi-Analytical Closed-Wing Weight Estimation during Conceptual Design. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:948ab573-cea8-43a7-af94-40a38994016b

Chicago Manual of Style (16th Edition):

Rousseau, Rob (author). “Semi-Analytical Closed-Wing Weight Estimation during Conceptual Design.” 2017. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:948ab573-cea8-43a7-af94-40a38994016b.

MLA Handbook (7th Edition):

Rousseau, Rob (author). “Semi-Analytical Closed-Wing Weight Estimation during Conceptual Design.” 2017. Web. 25 Jan 2021.

Vancouver:

Rousseau R(. Semi-Analytical Closed-Wing Weight Estimation during Conceptual Design. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:948ab573-cea8-43a7-af94-40a38994016b.

Council of Science Editors:

Rousseau R(. Semi-Analytical Closed-Wing Weight Estimation during Conceptual Design. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:948ab573-cea8-43a7-af94-40a38994016b


University of Melbourne

13. Brett, James Daniel. Numerical study of the flow over delta wings.

Degree: 2016, University of Melbourne

 Delta wing aircraft are becoming more commonplace due to the increasing numbers of unmanned aerial vehicles (UAV) which favour designs capable of producing large amounts… (more)

Subjects/Keywords: CFD; delta wing; UAV

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APA (6th Edition):

Brett, J. D. (2016). Numerical study of the flow over delta wings. (Doctoral Dissertation). University of Melbourne. Retrieved from http://hdl.handle.net/11343/92383

Chicago Manual of Style (16th Edition):

Brett, James Daniel. “Numerical study of the flow over delta wings.” 2016. Doctoral Dissertation, University of Melbourne. Accessed January 25, 2021. http://hdl.handle.net/11343/92383.

MLA Handbook (7th Edition):

Brett, James Daniel. “Numerical study of the flow over delta wings.” 2016. Web. 25 Jan 2021.

Vancouver:

Brett JD. Numerical study of the flow over delta wings. [Internet] [Doctoral dissertation]. University of Melbourne; 2016. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11343/92383.

Council of Science Editors:

Brett JD. Numerical study of the flow over delta wings. [Doctoral Dissertation]. University of Melbourne; 2016. Available from: http://hdl.handle.net/11343/92383


Virginia Tech

14. Eger, Charles Alfred Gaitan. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.

Degree: MS, Aerospace Engineering, 2013, Virginia Tech

 A procedure for the design of a scaled aircraft using linear aeroelastic scaling is developed and demonstrated. Previous work has shown the viability in matching… (more)

Subjects/Keywords: Aeroelasticity; Scaling; Joined-wing

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APA (6th Edition):

Eger, C. A. G. (2013). Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23088

Chicago Manual of Style (16th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Masters Thesis, Virginia Tech. Accessed January 25, 2021. http://hdl.handle.net/10919/23088.

MLA Handbook (7th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Web. 25 Jan 2021.

Vancouver:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10919/23088.

Council of Science Editors:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23088


University of New South Wales

15. Liu, Zhengliang. Numerical analysis of the performance of flapping foil power generators.

Degree: Aerospace, Civil & Mechanical Engineering, 2018, University of New South Wales

 An innovative concept of wind turbines, the flapping foil power generator that exploits dynamic stall, is numerically studied at Reynolds number of 1100. The combination… (more)

Subjects/Keywords: Flapping wing; Power generator

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APA (6th Edition):

Liu, Z. (2018). Numerical analysis of the performance of flapping foil power generators. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/60105 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51387/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Liu, Zhengliang. “Numerical analysis of the performance of flapping foil power generators.” 2018. Doctoral Dissertation, University of New South Wales. Accessed January 25, 2021. http://handle.unsw.edu.au/1959.4/60105 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51387/SOURCE02?view=true.

MLA Handbook (7th Edition):

Liu, Zhengliang. “Numerical analysis of the performance of flapping foil power generators.” 2018. Web. 25 Jan 2021.

Vancouver:

Liu Z. Numerical analysis of the performance of flapping foil power generators. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2021 Jan 25]. Available from: http://handle.unsw.edu.au/1959.4/60105 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51387/SOURCE02?view=true.

Council of Science Editors:

Liu Z. Numerical analysis of the performance of flapping foil power generators. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/60105 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51387/SOURCE02?view=true


Utah State University

16. Goates, Joshua Taylor. Development of an Improved Low-Order Model for Propeller-Wing Interactions.

Degree: MS, Mechanical and Aerospace Engineering, 2018, Utah State University

  For aircraft that have propellers mounted in front of the wings or tail, the prop wash produced by the propellers can have a strong… (more)

Subjects/Keywords: Propeller; Wing; Aerodynamics; Mechanical Engineering

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

APA (6th Edition):

Goates, J. T. (2018). Development of an Improved Low-Order Model for Propeller-Wing Interactions. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7394

Chicago Manual of Style (16th Edition):

Goates, Joshua Taylor. “Development of an Improved Low-Order Model for Propeller-Wing Interactions.” 2018. Masters Thesis, Utah State University. Accessed January 25, 2021. https://digitalcommons.usu.edu/etd/7394.

MLA Handbook (7th Edition):

Goates, Joshua Taylor. “Development of an Improved Low-Order Model for Propeller-Wing Interactions.” 2018. Web. 25 Jan 2021.

Vancouver:

Goates JT. Development of an Improved Low-Order Model for Propeller-Wing Interactions. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2021 Jan 25]. Available from: https://digitalcommons.usu.edu/etd/7394.

Council of Science Editors:

Goates JT. Development of an Improved Low-Order Model for Propeller-Wing Interactions. [Masters Thesis]. Utah State University; 2018. Available from: https://digitalcommons.usu.edu/etd/7394


University of Vermont

17. Fitz, William Peter. Reactionary Postmodernism? Neoliberalism, Multiculturalism, the Internet, and the Ideology of the New Far Right in Germany.

Degree: European Studies, 2018, University of Vermont

  This thesis aims to map the material, discursive, and ideological foundations of the new far right in Germany within the context of neoliberalism and… (more)

Subjects/Keywords: Right wing extremism; right wing radicalism; Identity Politics; Memes; Postmodernity; Fascism

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APA (6th Edition):

Fitz, W. P. (2018). Reactionary Postmodernism? Neoliberalism, Multiculturalism, the Internet, and the Ideology of the New Far Right in Germany. (Thesis). University of Vermont. Retrieved from https://scholarworks.uvm.edu/hcoltheses/275

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):

Fitz, William Peter. “Reactionary Postmodernism? Neoliberalism, Multiculturalism, the Internet, and the Ideology of the New Far Right in Germany.” 2018. Thesis, University of Vermont. Accessed January 25, 2021. https://scholarworks.uvm.edu/hcoltheses/275.

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

MLA Handbook (7th Edition):

Fitz, William Peter. “Reactionary Postmodernism? Neoliberalism, Multiculturalism, the Internet, and the Ideology of the New Far Right in Germany.” 2018. Web. 25 Jan 2021.

Vancouver:

Fitz WP. Reactionary Postmodernism? Neoliberalism, Multiculturalism, the Internet, and the Ideology of the New Far Right in Germany. [Internet] [Thesis]. University of Vermont; 2018. [cited 2021 Jan 25]. Available from: https://scholarworks.uvm.edu/hcoltheses/275.

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

Council of Science Editors:

Fitz WP. Reactionary Postmodernism? Neoliberalism, Multiculturalism, the Internet, and the Ideology of the New Far Right in Germany. [Thesis]. University of Vermont; 2018. Available from: https://scholarworks.uvm.edu/hcoltheses/275

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


Universidade Nova

18. Ponte, Susana Isabel Pereira da. The role of Grainy head in epithelial tissue growth.

Degree: 2014, Universidade Nova

Part of the results of this thesis was presented in the following meetings: Susana Ponte, Lara Carvalho, Inês Cristo and António Jacinto. The role of… (more)

Subjects/Keywords: Grainy head; Epithelia; Growth; Drosophila; Wing; Wing imaginal disc

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APA (6th Edition):

Ponte, S. I. P. d. (2014). The role of Grainy head in epithelial tissue growth. (Thesis). Universidade Nova. Retrieved from http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/13839

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):

Ponte, Susana Isabel Pereira da. “The role of Grainy head in epithelial tissue growth.” 2014. Thesis, Universidade Nova. Accessed January 25, 2021. http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/13839.

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

MLA Handbook (7th Edition):

Ponte, Susana Isabel Pereira da. “The role of Grainy head in epithelial tissue growth.” 2014. Web. 25 Jan 2021.

Vancouver:

Ponte SIPd. The role of Grainy head in epithelial tissue growth. [Internet] [Thesis]. Universidade Nova; 2014. [cited 2021 Jan 25]. Available from: http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/13839.

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

Council of Science Editors:

Ponte SIPd. The role of Grainy head in epithelial tissue growth. [Thesis]. Universidade Nova; 2014. Available from: http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/13839

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


University of Vienna

19. Eder, Alexander. Motive im Wing Chun.

Degree: 2017, University of Vienna

Wing Chun ist eine Kampfkunst, die sich in die Sparte des chinesischen Kung Fu einreiht. Ihre Entstehungsgeschichte ist verworren und von Uneinigkeiten geprägt. Es handelt… (more)

Subjects/Keywords: 76.11 Sportsoziologie, Sportpsychologie; Wing Chun / Motive; Wing Chun / motives

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APA (6th Edition):

Eder, A. (2017). Motive im Wing Chun. (Thesis). University of Vienna. Retrieved from http://othes.univie.ac.at/46752/

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):

Eder, Alexander. “Motive im Wing Chun.” 2017. Thesis, University of Vienna. Accessed January 25, 2021. http://othes.univie.ac.at/46752/.

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

MLA Handbook (7th Edition):

Eder, Alexander. “Motive im Wing Chun.” 2017. Web. 25 Jan 2021.

Vancouver:

Eder A. Motive im Wing Chun. [Internet] [Thesis]. University of Vienna; 2017. [cited 2021 Jan 25]. Available from: http://othes.univie.ac.at/46752/.

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

Council of Science Editors:

Eder A. Motive im Wing Chun. [Thesis]. University of Vienna; 2017. Available from: http://othes.univie.ac.at/46752/

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


Univerzitet u Beogradu

20. Đorić, Marija R., 1981-. Идеолошки мотивисан екстремизам као генератор политичкиг насиља.

Degree: Fakultet političkih nauka, 2015, Univerzitet u Beogradu

Политичке науке / Political sciences

У раду се истражује које све то облике политичког насиља може генерисати идеолошки мотивисан екстремизам и под којим условима. Како… (more)

Subjects/Keywords: extremism; ideology; left wing; right wing; terrorism; political violence

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APA (6th Edition):

Đorić, Marija R., 1. (2015). Идеолошки мотивисан екстремизам као генератор политичкиг насиља. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:7253/bdef:Content/get

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):

Đorić, Marija R., 1981-. “Идеолошки мотивисан екстремизам као генератор политичкиг насиља.” 2015. Thesis, Univerzitet u Beogradu. Accessed January 25, 2021. https://fedorabg.bg.ac.rs/fedora/get/o:7253/bdef:Content/get.

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

MLA Handbook (7th Edition):

Đorić, Marija R., 1981-. “Идеолошки мотивисан екстремизам као генератор политичкиг насиља.” 2015. Web. 25 Jan 2021.

Vancouver:

Đorić, Marija R. 1. Идеолошки мотивисан екстремизам као генератор политичкиг насиља. [Internet] [Thesis]. Univerzitet u Beogradu; 2015. [cited 2021 Jan 25]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:7253/bdef:Content/get.

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

Council of Science Editors:

Đorić, Marija R. 1. Идеолошки мотивисан екстремизам као генератор политичкиг насиља. [Thesis]. Univerzitet u Beogradu; 2015. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:7253/bdef:Content/get

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


Delft University of Technology

21. Epema, Kitso (author). Wing Optimisation for Tractor Propeller Configurations: Validation and Application of Low-Order Numerical Models Adapted to Include Propeller-Induced Velocities.

Degree: 2017, Delft University of Technology

 Even though propellers are the oldest form of propulsion, they are still a popular choice for unmanned aerial vehicles (UAVs) and passenger aircraft in certain… (more)

Subjects/Keywords: propeller-wing interaction; optimisation; vortex lattice method; lifting line; propeller; wing

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APA (6th Edition):

Epema, K. (. (2017). Wing Optimisation for Tractor Propeller Configurations: Validation and Application of Low-Order Numerical Models Adapted to Include Propeller-Induced Velocities. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b091880e-7a0a-423c-a11e-6afe9b9575e3

Chicago Manual of Style (16th Edition):

Epema, Kitso (author). “Wing Optimisation for Tractor Propeller Configurations: Validation and Application of Low-Order Numerical Models Adapted to Include Propeller-Induced Velocities.” 2017. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:b091880e-7a0a-423c-a11e-6afe9b9575e3.

MLA Handbook (7th Edition):

Epema, Kitso (author). “Wing Optimisation for Tractor Propeller Configurations: Validation and Application of Low-Order Numerical Models Adapted to Include Propeller-Induced Velocities.” 2017. Web. 25 Jan 2021.

Vancouver:

Epema K(. Wing Optimisation for Tractor Propeller Configurations: Validation and Application of Low-Order Numerical Models Adapted to Include Propeller-Induced Velocities. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:b091880e-7a0a-423c-a11e-6afe9b9575e3.

Council of Science Editors:

Epema K(. Wing Optimisation for Tractor Propeller Configurations: Validation and Application of Low-Order Numerical Models Adapted to Include Propeller-Induced Velocities. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:b091880e-7a0a-423c-a11e-6afe9b9575e3


Delft University of Technology

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

Degree: 2015, Delft University of Technology

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

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

MLA Handbook (7th Edition):

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

Vancouver:

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

Council of Science Editors:

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


University of Helsinki

23. Pullinen, Leena. Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland: Suomalaisten mielikuvat vasemmiston ja oikeiston arvoista sekä erot vasemmistolaisten ja oikeistolaisten mielikuvien välillä.

Degree: Institute of Behavioural Sciences; Helsingfors universitet, Beteendevetenskapliga fakulteten, Institutionen för beteendevetenskaper, 2014, University of Helsinki

 Tavoitteet. Vasemmisto ja oikeisto ovat politiikassa laajalti käytettyjä termejä. Niillä ei ole tarkkoja akateemisia määritelmiä, mutta oikeisto on usein liitetty konservatiivisuuteen ja autoritaarisuuteen, ja vasemmisto… (more)

Subjects/Keywords: left-wing; right-wing; values; impressions; Psychology; Psykologia; Psykologi

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APA (6th Edition):

Pullinen, L. (2014). Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland: Suomalaisten mielikuvat vasemmiston ja oikeiston arvoista sekä erot vasemmistolaisten ja oikeistolaisten mielikuvien välillä. (Masters Thesis). University of Helsinki. Retrieved from http://hdl.handle.net/10138/154861

Chicago Manual of Style (16th Edition):

Pullinen, Leena. “Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland: Suomalaisten mielikuvat vasemmiston ja oikeiston arvoista sekä erot vasemmistolaisten ja oikeistolaisten mielikuvien välillä.” 2014. Masters Thesis, University of Helsinki. Accessed January 25, 2021. http://hdl.handle.net/10138/154861.

MLA Handbook (7th Edition):

Pullinen, Leena. “Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland: Suomalaisten mielikuvat vasemmiston ja oikeiston arvoista sekä erot vasemmistolaisten ja oikeistolaisten mielikuvien välillä.” 2014. Web. 25 Jan 2021.

Vancouver:

Pullinen L. Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland: Suomalaisten mielikuvat vasemmiston ja oikeiston arvoista sekä erot vasemmistolaisten ja oikeistolaisten mielikuvien välillä. [Internet] [Masters thesis]. University of Helsinki; 2014. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/10138/154861.

Council of Science Editors:

Pullinen L. Impressions of left-wing and right-wing values, and differences in impressions of left-wing and right-wing values between left-wingers and right-wingers in Finland: Suomalaisten mielikuvat vasemmiston ja oikeiston arvoista sekä erot vasemmistolaisten ja oikeistolaisten mielikuvien välillä. [Masters Thesis]. University of Helsinki; 2014. Available from: http://hdl.handle.net/10138/154861


University of Louisville

24. Broering, Timothy Michael, 1985-. The characterization of wing-wing vortex interactions of a tandem flapping wing configuration and its relationship to the phase angle and wing spacing.

Degree: PhD, 2013, University of Louisville

 A number of flying insects make use of tandem wing configurations, suggesting that such a setup may have potential advantages over a single wing at… (more)

Subjects/Keywords: CFD; Tandem wing; Fluid dynamics; Dragonfly; Flapping wing; Aerospace engineering

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APA (6th Edition):

Broering, Timothy Michael, 1. (2013). The characterization of wing-wing vortex interactions of a tandem flapping wing configuration and its relationship to the phase angle and wing spacing. (Doctoral Dissertation). University of Louisville. Retrieved from 10.18297/etd/157 ; https://ir.library.louisville.edu/etd/157

Chicago Manual of Style (16th Edition):

Broering, Timothy Michael, 1985-. “The characterization of wing-wing vortex interactions of a tandem flapping wing configuration and its relationship to the phase angle and wing spacing.” 2013. Doctoral Dissertation, University of Louisville. Accessed January 25, 2021. 10.18297/etd/157 ; https://ir.library.louisville.edu/etd/157.

MLA Handbook (7th Edition):

Broering, Timothy Michael, 1985-. “The characterization of wing-wing vortex interactions of a tandem flapping wing configuration and its relationship to the phase angle and wing spacing.” 2013. Web. 25 Jan 2021.

Vancouver:

Broering, Timothy Michael 1. The characterization of wing-wing vortex interactions of a tandem flapping wing configuration and its relationship to the phase angle and wing spacing. [Internet] [Doctoral dissertation]. University of Louisville; 2013. [cited 2021 Jan 25]. Available from: 10.18297/etd/157 ; https://ir.library.louisville.edu/etd/157.

Council of Science Editors:

Broering, Timothy Michael 1. The characterization of wing-wing vortex interactions of a tandem flapping wing configuration and its relationship to the phase angle and wing spacing. [Doctoral Dissertation]. University of Louisville; 2013. Available from: 10.18297/etd/157 ; https://ir.library.louisville.edu/etd/157


University of New South Wales

25. Shahzad, Aamer. Numerical analysis of the effects of flexibility, shapes and aspect ratios on hovering wing aerodynamics.

Degree: Engineering & Information Technology, 2018, University of New South Wales

 Biological flight has inspired the development of micro aerial vehicles but the effects of flexibility, shapes and aspect ratios (AR) on hovering wing aerodynamics are… (more)

Subjects/Keywords: Aspect ratio; Flapping wing; Wing shape; Flexibility; Fluid-structure interaction

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APA (6th Edition):

Shahzad, A. (2018). Numerical analysis of the effects of flexibility, shapes and aspect ratios on hovering wing aerodynamics. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/60041 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51369/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Shahzad, Aamer. “Numerical analysis of the effects of flexibility, shapes and aspect ratios on hovering wing aerodynamics.” 2018. Doctoral Dissertation, University of New South Wales. Accessed January 25, 2021. http://handle.unsw.edu.au/1959.4/60041 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51369/SOURCE02?view=true.

MLA Handbook (7th Edition):

Shahzad, Aamer. “Numerical analysis of the effects of flexibility, shapes and aspect ratios on hovering wing aerodynamics.” 2018. Web. 25 Jan 2021.

Vancouver:

Shahzad A. Numerical analysis of the effects of flexibility, shapes and aspect ratios on hovering wing aerodynamics. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2021 Jan 25]. Available from: http://handle.unsw.edu.au/1959.4/60041 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51369/SOURCE02?view=true.

Council of Science Editors:

Shahzad A. Numerical analysis of the effects of flexibility, shapes and aspect ratios on hovering wing aerodynamics. [Doctoral Dissertation]. University of New South Wales; 2018. Available from: http://handle.unsw.edu.au/1959.4/60041 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:51369/SOURCE02?view=true


The Ohio State University

26. Trussa, Colin Weidner. Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips.

Degree: MS, Aero/Astro Engineering, 2020, The Ohio State University

 The purpose of this work was to investigate the low-speed aerodynamic characteristics of a novel delta wing layout with deflected wing tips. This project is… (more)

Subjects/Keywords: Aerospace Engineering; delta wing; deflected wing tips; low-speed aerodynamics

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APA (6th Edition):

Trussa, C. W. (2020). Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1586450691890636

Chicago Manual of Style (16th Edition):

Trussa, Colin Weidner. “Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips.” 2020. Masters Thesis, The Ohio State University. Accessed January 25, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=osu1586450691890636.

MLA Handbook (7th Edition):

Trussa, Colin Weidner. “Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips.” 2020. Web. 25 Jan 2021.

Vancouver:

Trussa CW. Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips. [Internet] [Masters thesis]. The Ohio State University; 2020. [cited 2021 Jan 25]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1586450691890636.

Council of Science Editors:

Trussa CW. Low-Speed Aerodynamic Characteristics of a Delta Wing with Deflected Wing Tips. [Masters Thesis]. The Ohio State University; 2020. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1586450691890636


Indian Institute of Science

27. Mysa, Ravi Chaithanya. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.

Degree: PhD, Faculty of Engineering, 2017, Indian Institute of Science

 This study seeks to understand the interplay of vorticity and elasto-dynamics that forms the basis for a fluttering flag and flapping wing propulsion, and factors… (more)

Subjects/Keywords: Wing Propulsion; Flapping Wing Propulsion; Fluttering Wing Propulsion; Fluttering Flags; Flapping Foils; Wing Propulsion Vorticity; Wing Propulsion Elasto-Dynamics; Viscous Fluid Flow; Flexible Foil; Aerospace Engineering

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APA (6th Edition):

Mysa, R. C. (2017). Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2706

Chicago Manual of Style (16th Edition):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2017. Doctoral Dissertation, Indian Institute of Science. Accessed January 25, 2021. http://etd.iisc.ac.in/handle/2005/2706.

MLA Handbook (7th Edition):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2017. Web. 25 Jan 2021.

Vancouver:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2017. [cited 2021 Jan 25]. Available from: http://etd.iisc.ac.in/handle/2005/2706.

Council of Science Editors:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Doctoral Dissertation]. Indian Institute of Science; 2017. Available from: http://etd.iisc.ac.in/handle/2005/2706


Grand Valley State University

28. Durrer, Simon. Aerodynamics of Race Car Wings: A CFD Study.

Degree: 2016, Grand Valley State University

 Formula 1 racing is one of the most advanced technological sports. The aerodynamic on open wheel race cars is essential for the performance during a… (more)

Subjects/Keywords: CFD; race car wing; aerodynamics; race car wing operating in ground effect; race car wing operating in wake; Engineering

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

APA (6th Edition):

Durrer, S. (2016). Aerodynamics of Race Car Wings: A CFD Study. (Thesis). Grand Valley State University. Retrieved from https://scholarworks.gvsu.edu/theses/798

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):

Durrer, Simon. “Aerodynamics of Race Car Wings: A CFD Study.” 2016. Thesis, Grand Valley State University. Accessed January 25, 2021. https://scholarworks.gvsu.edu/theses/798.

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

MLA Handbook (7th Edition):

Durrer, Simon. “Aerodynamics of Race Car Wings: A CFD Study.” 2016. Web. 25 Jan 2021.

Vancouver:

Durrer S. Aerodynamics of Race Car Wings: A CFD Study. [Internet] [Thesis]. Grand Valley State University; 2016. [cited 2021 Jan 25]. Available from: https://scholarworks.gvsu.edu/theses/798.

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

Council of Science Editors:

Durrer S. Aerodynamics of Race Car Wings: A CFD Study. [Thesis]. Grand Valley State University; 2016. Available from: https://scholarworks.gvsu.edu/theses/798

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


University of Michigan

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

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

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

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

MLA Handbook (7th Edition):

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

Vancouver:

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

Council of Science Editors:

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


Michigan State University

30. Fitzgerald, Sarah. The impact of religion on domestic right wing extremist groups and organizational violence.

Degree: 2011, Michigan State University

Thesis M.S. Michigan State University. Criminal Justice 2011.

The purpose of this study is to investigate the relationship between religion and violent activity among domestic… (more)

Subjects/Keywords: Right-wing extremists – United States; Right-wing extremists – United States – Religious aspects; Organizational sociology; Right-wing extremists; Criminology; Religion

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

APA (6th Edition):

Fitzgerald, S. (2011). The impact of religion on domestic right wing extremist groups and organizational violence. (Thesis). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:441

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):

Fitzgerald, Sarah. “The impact of religion on domestic right wing extremist groups and organizational violence.” 2011. Thesis, Michigan State University. Accessed January 25, 2021. http://etd.lib.msu.edu/islandora/object/etd:441.

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

MLA Handbook (7th Edition):

Fitzgerald, Sarah. “The impact of religion on domestic right wing extremist groups and organizational violence.” 2011. Web. 25 Jan 2021.

Vancouver:

Fitzgerald S. The impact of religion on domestic right wing extremist groups and organizational violence. [Internet] [Thesis]. Michigan State University; 2011. [cited 2021 Jan 25]. Available from: http://etd.lib.msu.edu/islandora/object/etd:441.

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

Council of Science Editors:

Fitzgerald S. The impact of religion on domestic right wing extremist groups and organizational violence. [Thesis]. Michigan State University; 2011. Available from: http://etd.lib.msu.edu/islandora/object/etd:441

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

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