Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:( Wing). Showing records 1 – 30 of 771 total matches.

[1] [2] [3] [4] [5] … [26]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

Languages

Country

▼ Search Limiters


Texas A&M University

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

Degree: 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

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):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Thesis, Texas A&M University. Accessed August 18, 2019. http://hdl.handle.net/1969.1/153426.

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

MLA Handbook (7th Edition):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Web. 18 Aug 2019.

Vancouver:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1969.1/153426.

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

Council of Science Editors:

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

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


University of Manchester

2. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 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. 18 Aug 2019.

Vancouver:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Aug 18]. 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


NSYSU

3. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Pan C. A Preliminary Study of Left Wing in Taiwan - from the Perspective of Historical Institutionalism. [Internet] [Thesis]. NSYSU; 2018. [cited 2019 Aug 18]. 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

4. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 August 18, 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. 18 Aug 2019.

Vancouver:

Abdul Hamid MF. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Aug 18]. 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 Helsinki

5. 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.

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

Aims of the study. The left and right are widely used terms in politics. The terms do not have exact academic definitions, but right-wing stances… (more)

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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. (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.” 2014. Masters Thesis, University of Helsinki. Accessed August 18, 2019. 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.” 2014. Web. 18 Aug 2019.

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. [Internet] [Masters thesis]. University of Helsinki; 2014. [cited 2019 Aug 18]. 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. [Masters Thesis]. University of Helsinki; 2014. Available from: http://hdl.handle.net/10138/154861


University of Kansas

6. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

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 2019 Aug 18]. 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

7. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

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 2019 Aug 18]. 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


Indian Institute of Science

8. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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://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 August 18, 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. 18 Aug 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Aug 18]. 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

9. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 August 18, 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. 18 Aug 2019.

Vancouver:

Mukherjee S. Structural Modeling And Analysis Of Insect Scale Flapping Wing. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Aug 18]. 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


Carnegie Mellon University

10. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

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 2019 Aug 18]. 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

11. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

El Ouardi O. Design, Analysis And Testing Of An Aircraft Wing Model With Morphing Mechanism. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Aug 18]. 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


Texas A&M University

12. Jackson, Justin Patrick. Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.

Degree: 2009, Texas A&M University

 This thesis presents a method for designing a flapping wing stroke for a flapping wing vehicle. A flapping wing vehicle is a vehicle such as… (more)

Subjects/Keywords: flapping wing; control; optimal

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jackson, J. P. (2009). Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2854

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):

Jackson, Justin Patrick. “Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.” 2009. Thesis, Texas A&M University. Accessed August 18, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2854.

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

MLA Handbook (7th Edition):

Jackson, Justin Patrick. “Modelling and control of a symmetric flapping wing vehicle: an optimal control approach.” 2009. Web. 18 Aug 2019.

Vancouver:

Jackson JP. Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2854.

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

Council of Science Editors:

Jackson JP. Modelling and control of a symmetric flapping wing vehicle: an optimal control approach. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2854

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


Virginia Tech

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

Degree: MS, Aerospace and Ocean 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2019 Aug 18]. 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


Delft University of Technology

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

Degree: 2012, Delft University of Technology

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

Subjects/Keywords: nonlinear; finite; wing structure

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Riahi, G. “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.” 2012. Masters Thesis, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:ab0d4288-3dfd-468d-a6d8-cdafa3ea2164.

MLA Handbook (7th Edition):

Riahi, G. “Model Order Reduction for a Nonlinear Finite Element Model of a Joined Wing Structure:.” 2012. Web. 18 Aug 2019.

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 2019 Aug 18]. 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


University of Melbourne

15. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. http://hdl.handle.net/11343/92383.

MLA Handbook (7th Edition):

Brett, James Daniel. “Numerical study of the flow over delta wings.” 2016. Web. 18 Aug 2019.

Vancouver:

Brett JD. Numerical study of the flow over delta wings. [Internet] [Doctoral dissertation]. University of Melbourne; 2016. [cited 2019 Aug 18]. 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


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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Goates JT. Development of an Improved Low-Order Model for Propeller-Wing Interactions. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2019 Aug 18]. 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 Rochester

17. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Loehlin, David Walker (1981 - ); Werren JH. Genetics of size and shape evolution in Nasonia. [Internet] [Doctoral dissertation]. University of Rochester; 2012. [cited 2019 Aug 18]. 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


University of New South Wales

18. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Liu Z. Numerical analysis of the performance of flapping foil power generators. [Internet] [Doctoral dissertation]. University of New South Wales; 2018. [cited 2019 Aug 18]. 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


Univerzitet u Beogradu

19. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Đorić, Marija R. 1. Идеолошки мотивисан екстремизам као генератор политичкиг насиља. [Internet] [Thesis]. Univerzitet u Beogradu; 2015. [cited 2019 Aug 18]. 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


University of Louisville

20. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

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 2019 Aug 18]. 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


Universidade Nova

21. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Ponte SIPd. The role of Grainy head in epithelial tissue growth. [Internet] [Thesis]. Universidade Nova; 2014. [cited 2019 Aug 18]. 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

22. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Eder A. Motive im Wing Chun. [Internet] [Thesis]. University of Vienna; 2017. [cited 2019 Aug 18]. 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


Delft University of Technology

23. Sol, M.B. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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. “Conceptual Design of Swept Wing Root Aerofoils:.” 2015. Masters Thesis, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:5bf482f6-5910-4346-abd5-785748980bc9.

MLA Handbook (7th Edition):

Sol, M B. “Conceptual Design of Swept Wing Root Aerofoils:.” 2015. Web. 18 Aug 2019.

Vancouver:

Sol MB. Conceptual Design of Swept Wing Root Aerofoils:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Aug 18]. 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 Vermont

24. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 August 18, 2019. 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. 18 Aug 2019.

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 2019 Aug 18]. 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


Indian Institute of Science

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

Degree: 2013, 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mysa, R. C. (2013). Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2706

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):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Thesis, Indian Institute of Science. Accessed August 18, 2019. http://hdl.handle.net/2005/2706.

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

MLA Handbook (7th Edition):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Web. 18 Aug 2019.

Vancouver:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2005/2706.

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

Council of Science Editors:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Thesis]. Indian Institute of Science; 2013. Available from: http://hdl.handle.net/2005/2706

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


Indian Institute of Science

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

Degree: 2013, 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mysa, R. C. (2013). Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-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):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Thesis, Indian Institute of Science. Accessed August 18, 2019. http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-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):

Mysa, Ravi Chaithanya. “Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion.” 2013. Web. 18 Aug 2019.

Vancouver:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Internet] [Thesis]. Indian Institute of Science; 2013. [cited 2019 Aug 18]. Available from: http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-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:

Mysa RC. Fluid-Elastic Interactions in Flutter And Flapping Wing Propulsion. [Thesis]. Indian Institute of Science; 2013. Available from: http://etd.iisc.ernet.in/handle/2005/2706 ; http://etd.ncsi.iisc.ernet.in/abstracts/3529/G26380-Abs.pdf

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


Grand Valley State University

27. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 August 18, 2019. 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. 18 Aug 2019.

Vancouver:

Durrer S. Aerodynamics of Race Car Wings: A CFD Study. [Internet] [Thesis]. Grand Valley State University; 2016. [cited 2019 Aug 18]. 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


Coventry University

28. Buckler, Scott R. Sects and violence : development of an inclusive taxonomy to hermeneutically explore the histo-philosophical motivators for the inception and development of the martial art, Wing Chun Kuen.

Degree: PhD, 2010, Coventry University

 Martial arts participation rates exceed those reported for a number of higher- profile physical activities (Sport England, 2002), however little research has been conducted to… (more)

Subjects/Keywords: 796.8; martial arts, Wing Chun; Martial arts

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Buckler, S. R. (2010). Sects and violence : development of an inclusive taxonomy to hermeneutically explore the histo-philosophical motivators for the inception and development of the martial art, Wing Chun Kuen. (Doctoral Dissertation). Coventry University. Retrieved from http://curve.coventry.ac.uk/open/items/4b1d8ab6-a860-4d0d-887d-67e73a7b18c5/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.633633

Chicago Manual of Style (16th Edition):

Buckler, Scott R. “Sects and violence : development of an inclusive taxonomy to hermeneutically explore the histo-philosophical motivators for the inception and development of the martial art, Wing Chun Kuen.” 2010. Doctoral Dissertation, Coventry University. Accessed August 18, 2019. http://curve.coventry.ac.uk/open/items/4b1d8ab6-a860-4d0d-887d-67e73a7b18c5/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.633633.

MLA Handbook (7th Edition):

Buckler, Scott R. “Sects and violence : development of an inclusive taxonomy to hermeneutically explore the histo-philosophical motivators for the inception and development of the martial art, Wing Chun Kuen.” 2010. Web. 18 Aug 2019.

Vancouver:

Buckler SR. Sects and violence : development of an inclusive taxonomy to hermeneutically explore the histo-philosophical motivators for the inception and development of the martial art, Wing Chun Kuen. [Internet] [Doctoral dissertation]. Coventry University; 2010. [cited 2019 Aug 18]. Available from: http://curve.coventry.ac.uk/open/items/4b1d8ab6-a860-4d0d-887d-67e73a7b18c5/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.633633.

Council of Science Editors:

Buckler SR. Sects and violence : development of an inclusive taxonomy to hermeneutically explore the histo-philosophical motivators for the inception and development of the martial art, Wing Chun Kuen. [Doctoral Dissertation]. Coventry University; 2010. Available from: http://curve.coventry.ac.uk/open/items/4b1d8ab6-a860-4d0d-887d-67e73a7b18c5/1 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.633633


University of Limerick

29. O'Regan, Micheál Seán. A numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near-field.

Degree: 2014, University of Limerick

peer-reviewed

Turbulent wing-tip vortices are an extremely important fluid dynamics phenomena for their negative impact in several applications. Despite the many numerical and experimental studies… (more)

Subjects/Keywords: wing-tip vortices; numerical methods; equations

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

O'Regan, M. S. (2014). A numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near-field. (Thesis). University of Limerick. Retrieved from http://hdl.handle.net/10344/4275

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):

O'Regan, Micheál Seán. “A numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near-field.” 2014. Thesis, University of Limerick. Accessed August 18, 2019. http://hdl.handle.net/10344/4275.

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

MLA Handbook (7th Edition):

O'Regan, Micheál Seán. “A numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near-field.” 2014. Web. 18 Aug 2019.

Vancouver:

O'Regan MS. A numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near-field. [Internet] [Thesis]. University of Limerick; 2014. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10344/4275.

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

Council of Science Editors:

O'Regan MS. A numerical and experimental investigation of the mean and turbulent characteristics of a wing-tip vortex in the near-field. [Thesis]. University of Limerick; 2014. Available from: http://hdl.handle.net/10344/4275

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


University of Utah

30. Newport, Melanie Diane. Grassroots power: the Utah Eagle Forum, 1972-2009.

Degree: MA;, History;, 2009, University of Utah

 How and why has a group of conservative housewives become the most powerful lobbying group in one of the most populous states in the Mountain… (more)

Subjects/Keywords: Utah politics; Extremism; Right-wing activism

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Newport, M. D. (2009). Grassroots power: the Utah Eagle Forum, 1972-2009. (Masters Thesis). University of Utah. Retrieved from http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/1352/rec/558

Chicago Manual of Style (16th Edition):

Newport, Melanie Diane. “Grassroots power: the Utah Eagle Forum, 1972-2009.” 2009. Masters Thesis, University of Utah. Accessed August 18, 2019. http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/1352/rec/558.

MLA Handbook (7th Edition):

Newport, Melanie Diane. “Grassroots power: the Utah Eagle Forum, 1972-2009.” 2009. Web. 18 Aug 2019.

Vancouver:

Newport MD. Grassroots power: the Utah Eagle Forum, 1972-2009. [Internet] [Masters thesis]. University of Utah; 2009. [cited 2019 Aug 18]. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/1352/rec/558.

Council of Science Editors:

Newport MD. Grassroots power: the Utah Eagle Forum, 1972-2009. [Masters Thesis]. University of Utah; 2009. Available from: http://content.lib.utah.edu/cdm/singleitem/collection/etd2/id/1352/rec/558

[1] [2] [3] [4] [5] … [26]

.