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You searched for subject:( Variable sweep wing). Showing records 1 – 30 of 4153 total matches.

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RMIT University

1. Guo, D. Modelling and experimental investigations of a bi-modal unmanned underwater/air system.

Degree: 2019, RMIT University

 The ability to perform underwater and coastal area monitoring missions without surfacing would increase submarine's safety and its combat ability. An innovative bi-modal unmanned/underwater air… (more)

Subjects/Keywords: Fields of Research; BUUAS; Transition propulsion system; Hybrid propulsion system; Variable sweep wing configuration; Wind tunnel test; Numerical simulation; Composite materials; Stability analysis

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APA (6th Edition):

Guo, D. (2019). Modelling and experimental investigations of a bi-modal unmanned underwater/air system. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:162852

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):

Guo, D. “Modelling and experimental investigations of a bi-modal unmanned underwater/air system.” 2019. Thesis, RMIT University. Accessed January 17, 2021. http://researchbank.rmit.edu.au/view/rmit:162852.

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

MLA Handbook (7th Edition):

Guo, D. “Modelling and experimental investigations of a bi-modal unmanned underwater/air system.” 2019. Web. 17 Jan 2021.

Vancouver:

Guo D. Modelling and experimental investigations of a bi-modal unmanned underwater/air system. [Internet] [Thesis]. RMIT University; 2019. [cited 2021 Jan 17]. Available from: http://researchbank.rmit.edu.au/view/rmit:162852.

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

Council of Science Editors:

Guo D. Modelling and experimental investigations of a bi-modal unmanned underwater/air system. [Thesis]. RMIT University; 2019. Available from: http://researchbank.rmit.edu.au/view/rmit:162852

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


University of Pretoria

2. [No author]. Longitudinal handling characteristics of a tailless gull-wing aircraft .

Degree: 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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APA (6th Edition):

author], [. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-09182008-132941/

Chicago Manual of Style (16th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Masters Thesis, University of Pretoria. Accessed January 17, 2021. http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

MLA Handbook (7th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Web. 17 Jan 2021.

Vancouver:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 17]. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

Council of Science Editors:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/


University of Pretoria

3. Agenbag, Daniel Sarel. Longitudinal handling characteristics of a tailless gull-wing aircraft.

Degree: Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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APA (6th Edition):

Agenbag, D. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/28011

Chicago Manual of Style (16th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Masters Thesis, University of Pretoria. Accessed January 17, 2021. http://hdl.handle.net/2263/28011.

MLA Handbook (7th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Web. 17 Jan 2021.

Vancouver:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/2263/28011.

Council of Science Editors:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/28011


University of Manchester

4. 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 17, 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. 17 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 17]. 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


Arizona State University

5. Kirkman, Jeffrey Jordan. Transonic Flow Around Swept Wings: Revisiting Von Kármán’s Similarity Rule.

Degree: Aerospace Engineering, 2016, Arizona State University

 Modern aircraft are expected to fly faster and more efficiently than their predecessors. To improve aerodynamic efficiency, designers must carefully consider and handle shock wave… (more)

Subjects/Keywords: Aerospace engineering; Aircraft Wing Sweep; Critical Pressure Coefficient; Shock Formation; Transonic Similarity Rule

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APA (6th Edition):

Kirkman, J. J. (2016). Transonic Flow Around Swept Wings: Revisiting Von Kármán’s Similarity Rule. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/38688

Chicago Manual of Style (16th Edition):

Kirkman, Jeffrey Jordan. “Transonic Flow Around Swept Wings: Revisiting Von Kármán’s Similarity Rule.” 2016. Masters Thesis, Arizona State University. Accessed January 17, 2021. http://repository.asu.edu/items/38688.

MLA Handbook (7th Edition):

Kirkman, Jeffrey Jordan. “Transonic Flow Around Swept Wings: Revisiting Von Kármán’s Similarity Rule.” 2016. Web. 17 Jan 2021.

Vancouver:

Kirkman JJ. Transonic Flow Around Swept Wings: Revisiting Von Kármán’s Similarity Rule. [Internet] [Masters thesis]. Arizona State University; 2016. [cited 2021 Jan 17]. Available from: http://repository.asu.edu/items/38688.

Council of Science Editors:

Kirkman JJ. Transonic Flow Around Swept Wings: Revisiting Von Kármán’s Similarity Rule. [Masters Thesis]. Arizona State University; 2016. Available from: http://repository.asu.edu/items/38688

6. Felício, João Miguel Inácio. Development and testing of a variable-spam morphing wing.

Degree: 2010, RCAAP

 The present work focuses on the development and validation of a variable-span morphing wing (VSW) to be fitted to a mini UAV. An electro-mechanical actuation… (more)

Subjects/Keywords: Aeronaves - Asa; Asa morphing; Aeronaves - Asa de envergadura variável; VSW (Variable Spam Wing); Variable spam wing

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APA (6th Edition):

Felício, J. M. I. (2010). Development and testing of a variable-spam morphing wing. (Thesis). RCAAP. Retrieved from http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3663

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):

Felício, João Miguel Inácio. “Development and testing of a variable-spam morphing wing.” 2010. Thesis, RCAAP. Accessed January 17, 2021. http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3663.

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

MLA Handbook (7th Edition):

Felício, João Miguel Inácio. “Development and testing of a variable-spam morphing wing.” 2010. Web. 17 Jan 2021.

Vancouver:

Felício JMI. Development and testing of a variable-spam morphing wing. [Internet] [Thesis]. RCAAP; 2010. [cited 2021 Jan 17]. Available from: http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3663.

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

Council of Science Editors:

Felício JMI. Development and testing of a variable-spam morphing wing. [Thesis]. RCAAP; 2010. Available from: http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3663

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


University of Florida

7. Speer, Kelly. Dispersal of Bats in an Island System.

Degree: MS, Zoology - Biology, 2015, University of Florida

 Dispersal is a key variable in many fields of biology, including phylogenetics, epidemiology, and conservation. Dispersal can be difficult to quantify, requiring intensive fieldwork, thorough… (more)

Subjects/Keywords: Bats; Caves; Ecology; Microsatellites; Museums; Population estimates; Population genetics; Population structure; Species; Variable sweep wings; bats  – dispersal; City of Gainesville ( local )

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APA (6th Edition):

Speer, K. (2015). Dispersal of Bats in an Island System. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0049349

Chicago Manual of Style (16th Edition):

Speer, Kelly. “Dispersal of Bats in an Island System.” 2015. Masters Thesis, University of Florida. Accessed January 17, 2021. https://ufdc.ufl.edu/UFE0049349.

MLA Handbook (7th Edition):

Speer, Kelly. “Dispersal of Bats in an Island System.” 2015. Web. 17 Jan 2021.

Vancouver:

Speer K. Dispersal of Bats in an Island System. [Internet] [Masters thesis]. University of Florida; 2015. [cited 2021 Jan 17]. Available from: https://ufdc.ufl.edu/UFE0049349.

Council of Science Editors:

Speer K. Dispersal of Bats in an Island System. [Masters Thesis]. University of Florida; 2015. Available from: https://ufdc.ufl.edu/UFE0049349


Virginia Tech

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

Degree: PhD, Aerospace Engineering, 2016, Virginia Tech

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Mallik, Wrik. “Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.” 2016. Doctoral Dissertation, Virginia Tech. Accessed January 17, 2021. http://hdl.handle.net/10919/71650.

MLA Handbook (7th Edition):

Mallik, Wrik. “Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization.” 2016. Web. 17 Jan 2021.

Vancouver:

Mallik W. Aeroelastic Analysis of Truss-Braced Wing Aircraft: Applications for Multidisciplinary Design Optimization. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/10919/71650.

Council of Science Editors:

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


University of Dayton

9. Zientarski, Lauren Ann. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.

Degree: MS(M.S.), Aerospace Engineering, 2015, University of Dayton

 This thesis describes the design, setup, and testing of a unique mounting fixture built for the Variable Camber Compliant Wing developed by the U.S. Air… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Variable Camber Compliant Wing; Dual Load Cell; Test Fixture Validation; Calibration Loading

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APA (6th Edition):

Zientarski, L. A. (2015). Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315

Chicago Manual of Style (16th Edition):

Zientarski, Lauren Ann. “Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.” 2015. Masters Thesis, University of Dayton. Accessed January 17, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315.

MLA Handbook (7th Edition):

Zientarski, Lauren Ann. “Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.” 2015. Web. 17 Jan 2021.

Vancouver:

Zientarski LA. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. [Internet] [Masters thesis]. University of Dayton; 2015. [cited 2021 Jan 17]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315.

Council of Science Editors:

Zientarski LA. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. [Masters Thesis]. University of Dayton; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315

10. Boulamatsis, Achilles. Active control of wind turbines through varying blade tip sweep.

Degree: 2017, University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας

In this research work an introduction to an innovative control method, concerning horizontal axis wind turbines, is presented. The concept refers to variable tip swept… (more)

Subjects/Keywords: Ανεμογεννήτρια; Wind turbine; Sweep

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APA (6th Edition):

Boulamatsis, A. (2017). Active control of wind turbines through varying blade tip sweep. (Thesis). University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας. Retrieved from http://hdl.handle.net/10442/hedi/40592

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):

Boulamatsis, Achilles. “Active control of wind turbines through varying blade tip sweep.” 2017. Thesis, University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας. Accessed January 17, 2021. http://hdl.handle.net/10442/hedi/40592.

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

MLA Handbook (7th Edition):

Boulamatsis, Achilles. “Active control of wind turbines through varying blade tip sweep.” 2017. Web. 17 Jan 2021.

Vancouver:

Boulamatsis A. Active control of wind turbines through varying blade tip sweep. [Internet] [Thesis]. University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας; 2017. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/10442/hedi/40592.

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

Council of Science Editors:

Boulamatsis A. Active control of wind turbines through varying blade tip sweep. [Thesis]. University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας; 2017. Available from: http://hdl.handle.net/10442/hedi/40592

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

11. Camarinha Fujiwara, Gustavo. Design of 3D swept wing hybrid models for icing wind tunnel tests.

Degree: MS, 4048, 2015, University of Illinois – Urbana-Champaign

 The study of aircraft icing is critical to ensure the safety of any aircraft that might experience icing conditions in flight, including general, commercial, and… (more)

Subjects/Keywords: Aerodynamics; aircraft icing; wind tunnel; icing; ice shape; Accretion; hybrid; sweep; swept; wing; computational fluid dynamics (CFD); aircraft certification; wing design

…a transonic wing having a quarter-chord sweep angle of 35◦ . The supercritical wing was… …designed utilizing the stations in the normal direction, applying simple sweep wing theory, as… …to extrude a rectangular wing of the same leading-edge sweep angle, and then takes the… …1.2 Previous Work . . . . . . . . . . . . . . . . . . . . . 1.3 Large-Scale Swept-Wing Ice… …Sidewalls . . . . . . . . . 4.2.2 Effect of Sweep Angle . . . . . . . . . . . . . . . 4.2.3 Effect… 

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APA (6th Edition):

Camarinha Fujiwara, G. (2015). Design of 3D swept wing hybrid models for icing wind tunnel tests. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/72880

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):

Camarinha Fujiwara, Gustavo. “Design of 3D swept wing hybrid models for icing wind tunnel tests.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed January 17, 2021. http://hdl.handle.net/2142/72880.

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

MLA Handbook (7th Edition):

Camarinha Fujiwara, Gustavo. “Design of 3D swept wing hybrid models for icing wind tunnel tests.” 2015. Web. 17 Jan 2021.

Vancouver:

Camarinha Fujiwara G. Design of 3D swept wing hybrid models for icing wind tunnel tests. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/2142/72880.

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

Council of Science Editors:

Camarinha Fujiwara G. Design of 3D swept wing hybrid models for icing wind tunnel tests. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/72880

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

12. Wiberg, Brock. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D.

Degree: MS, 4048, 2014, University of Illinois – Urbana-Champaign

 The study of aircraft icing is necessary to ensure the safety of commercial, military, and general aviation aircraft. The certification of modern commercial transports requires… (more)

Subjects/Keywords: aircraft icing; icing; ice shape; Accretion; sweep; swept; wing; computational fluid dynamics (CFD); aircraft certification; hybrid; similitude

…2.2.2 Simple Sweep Theory . . . . . . . . . . . . . . . . 2.2.3 Wing Model Design… …sweep angle λ = wing taper ratio µ = dynamic viscosity ν = kinematic viscosity ρ… …chord sweep of 35 deg. The supercritical wing was designed for a cruise Mach number of M… …having a quarter-chord sweep of Λ = 35 deg. (see Table 1.1). The supercritical wing… …1.2 Previous Work . . . . . . . . . . . . . . . . . . . . . 1.3 Large-Scale Swept-Wing Ice… 

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APA (6th Edition):

Wiberg, B. (2014). Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46609

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):

Wiberg, Brock. “Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed January 17, 2021. http://hdl.handle.net/2142/46609.

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

MLA Handbook (7th Edition):

Wiberg, Brock. “Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D.” 2014. Web. 17 Jan 2021.

Vancouver:

Wiberg B. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/2142/46609.

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

Council of Science Editors:

Wiberg B. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46609

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


Penn State University

13. Harris, Alexandre. Improved methods for detecting, quantifying, and classifying genetic diversity in natural populations.

Degree: 2020, Penn State University

 The field of population genetics has made impressive advances over the two decades since the sequencing of the human genome, and specifically in the last… (more)

Subjects/Keywords: Unbiased estimator; Haplotype; Multilocus genotype; Selective sweep; Maximum likelihood; Soft sweep

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APA (6th Edition):

Harris, A. (2020). Improved methods for detecting, quantifying, and classifying genetic diversity in natural populations. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/17977amh522

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):

Harris, Alexandre. “Improved methods for detecting, quantifying, and classifying genetic diversity in natural populations.” 2020. Thesis, Penn State University. Accessed January 17, 2021. https://submit-etda.libraries.psu.edu/catalog/17977amh522.

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

MLA Handbook (7th Edition):

Harris, Alexandre. “Improved methods for detecting, quantifying, and classifying genetic diversity in natural populations.” 2020. Web. 17 Jan 2021.

Vancouver:

Harris A. Improved methods for detecting, quantifying, and classifying genetic diversity in natural populations. [Internet] [Thesis]. Penn State University; 2020. [cited 2021 Jan 17]. Available from: https://submit-etda.libraries.psu.edu/catalog/17977amh522.

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

Council of Science Editors:

Harris A. Improved methods for detecting, quantifying, and classifying genetic diversity in natural populations. [Thesis]. Penn State University; 2020. Available from: https://submit-etda.libraries.psu.edu/catalog/17977amh522

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


University of Alberta

14. Urbissinova, Tolkynay. Experimental investigation of the effect of elasticity on the sweep efficiency in viscoelastic polymer flooding operations.

Degree: MS, Department of Civil and Environmental Engineering, 2010, University of Alberta

 This study aims to investigate the effect of elastic properties of viscoelastic polymer solutions on the microscopic sweep efficiency in enhanced oil recovery (EOR) operations.… (more)

Subjects/Keywords: sweep efficiency; viscoelastic polymer flooding; elasticity

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APA (6th Edition):

Urbissinova, T. (2010). Experimental investigation of the effect of elasticity on the sweep efficiency in viscoelastic polymer flooding operations. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/h702q654f

Chicago Manual of Style (16th Edition):

Urbissinova, Tolkynay. “Experimental investigation of the effect of elasticity on the sweep efficiency in viscoelastic polymer flooding operations.” 2010. Masters Thesis, University of Alberta. Accessed January 17, 2021. https://era.library.ualberta.ca/files/h702q654f.

MLA Handbook (7th Edition):

Urbissinova, Tolkynay. “Experimental investigation of the effect of elasticity on the sweep efficiency in viscoelastic polymer flooding operations.” 2010. Web. 17 Jan 2021.

Vancouver:

Urbissinova T. Experimental investigation of the effect of elasticity on the sweep efficiency in viscoelastic polymer flooding operations. [Internet] [Masters thesis]. University of Alberta; 2010. [cited 2021 Jan 17]. Available from: https://era.library.ualberta.ca/files/h702q654f.

Council of Science Editors:

Urbissinova T. Experimental investigation of the effect of elasticity on the sweep efficiency in viscoelastic polymer flooding operations. [Masters Thesis]. University of Alberta; 2010. Available from: https://era.library.ualberta.ca/files/h702q654f


Delft University of Technology

15. Sulistyo, Adhitomo (author). Injection of Water above Gas for Improved Sweep in Gas EOR: Non-uniform Injection and Sweep.

Degree: 2017, Delft University of Technology

 One proposed method to delay the onset of gravity segregation between water and gas in enhanced oil and gas projects and extend the period of… (more)

Subjects/Keywords: reservoir simulation; sweep efficiency; non-uniform injection

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APA (6th Edition):

Sulistyo, A. (. (2017). Injection of Water above Gas for Improved Sweep in Gas EOR: Non-uniform Injection and Sweep. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:7c2ddae2-257e-4693-a47f-b2ba72c7a7d5

Chicago Manual of Style (16th Edition):

Sulistyo, Adhitomo (author). “Injection of Water above Gas for Improved Sweep in Gas EOR: Non-uniform Injection and Sweep.” 2017. Masters Thesis, Delft University of Technology. Accessed January 17, 2021. http://resolver.tudelft.nl/uuid:7c2ddae2-257e-4693-a47f-b2ba72c7a7d5.

MLA Handbook (7th Edition):

Sulistyo, Adhitomo (author). “Injection of Water above Gas for Improved Sweep in Gas EOR: Non-uniform Injection and Sweep.” 2017. Web. 17 Jan 2021.

Vancouver:

Sulistyo A(. Injection of Water above Gas for Improved Sweep in Gas EOR: Non-uniform Injection and Sweep. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 17]. Available from: http://resolver.tudelft.nl/uuid:7c2ddae2-257e-4693-a47f-b2ba72c7a7d5.

Council of Science Editors:

Sulistyo A(. Injection of Water above Gas for Improved Sweep in Gas EOR: Non-uniform Injection and Sweep. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:7c2ddae2-257e-4693-a47f-b2ba72c7a7d5

16. Chuang, Jason C. Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design.

Degree: MSEgr, Mechanical Engineering, 2014, Wright State University

 Flapping wing micro air vehicles (FWMAV) have very unique flight mechanics in two-wing orientation. Many challenges arise with two wing configuration: lift production, design construction,… (more)

Subjects/Keywords: Aerospace Engineering; MAV; micro air vehicle, CVT, continuous variable transmission; flapping wing micro air vehicle; FWMAV

…method of variable flapping in MAVs is using two motors to control each wing independently… …39 x CHAPTER 1 INTRODUCTION 1.1 Flapping Wing Micro Air Vehicle Flapping Wing Micro Air… …inspired dragonfly lead to the development of the Wright State’s Four Wing Flapper, Delfly’s… …Delfly I and II. These four wing FWMAVs use the flight mechanism of a two-fixed wing structure… …their two wing designs. In evolution their second wing was adapted into halters, which are… 

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APA (6th Edition):

Chuang, J. C. (2014). Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452

Chicago Manual of Style (16th Edition):

Chuang, Jason C. “Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design.” 2014. Masters Thesis, Wright State University. Accessed January 17, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452.

MLA Handbook (7th Edition):

Chuang, Jason C. “Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design.” 2014. Web. 17 Jan 2021.

Vancouver:

Chuang JC. Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design. [Internet] [Masters thesis]. Wright State University; 2014. [cited 2021 Jan 17]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452.

Council of Science Editors:

Chuang JC. Variable Speed Flapping Wing Micro Air Vehicle using a Continuous Variable Transmission Design. [Masters Thesis]. Wright State University; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1401813452


Virginia Tech

17. Natarajan, Anand. Aeroelasticity of Morphing Wings Using Neural Networks.

Degree: PhD, Aerospace and Ocean Engineering, 2002, Virginia Tech

 In this dissertation, neural networks are designed to effectively model static non-linear aeroelastic problems in adaptive structures and linear dynamic aeroelastic systems with time varying… (more)

Subjects/Keywords: Time Varying Systems; Morphing Wings; Aeroelasticity; Adaptable Bump; Variable Stiffness Wing; Neural Networks; Flutter

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APA (6th Edition):

Natarajan, A. (2002). Aeroelasticity of Morphing Wings Using Neural Networks. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28267

Chicago Manual of Style (16th Edition):

Natarajan, Anand. “Aeroelasticity of Morphing Wings Using Neural Networks.” 2002. Doctoral Dissertation, Virginia Tech. Accessed January 17, 2021. http://hdl.handle.net/10919/28267.

MLA Handbook (7th Edition):

Natarajan, Anand. “Aeroelasticity of Morphing Wings Using Neural Networks.” 2002. Web. 17 Jan 2021.

Vancouver:

Natarajan A. Aeroelasticity of Morphing Wings Using Neural Networks. [Internet] [Doctoral dissertation]. Virginia Tech; 2002. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/10919/28267.

Council of Science Editors:

Natarajan A. Aeroelasticity of Morphing Wings Using Neural Networks. [Doctoral Dissertation]. Virginia Tech; 2002. Available from: http://hdl.handle.net/10919/28267


Texas A&M University

18. 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 17, 2021. http://hdl.handle.net/1969.1/153426.

MLA Handbook (7th Edition):

Cooper, Jacob. “Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics.” 2014. Web. 17 Jan 2021.

Vancouver:

Cooper J. Multi-Resolution Simulations of Delta/Diamond Wing Aerodynamics. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Jan 17]. 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

19. 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 17, 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. 17 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 17]. 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

20. 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 17, 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. 17 Jan 2021.

Vancouver:

Abdul Hamid MF. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Jan 17]. 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

21. 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 17, 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. 17 Jan 2021.

Vancouver:

Abdul Hamid MFB. Aerodynamic models for insect flight. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2021 Jan 17]. 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

22. 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 17, 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. 17 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 17]. 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

23. 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 17, 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. 17 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 17]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264.

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

Council of Science Editors:

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

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


University of New South Wales

24. McKinnon, Douglas John. Novel efficiency evaluation methods and analysis for three-phase induction machines.

Degree: Electrical Engineering and Telecommunications, 2005, University of New South Wales

 This thesis describes new methods of evaluating the efficiency of three-phase induction machines using synthetic loading. Synthetic loading causes the induction machine to draw full-load… (more)

Subjects/Keywords: synthetic loading; induction motor; parameter identification; parameter; efficiency testing; efficiency; dual frequency; sweep frequency; constant speed of rotating magnetic field; three phase induction motor; three phase induction machine; variable rotor parameter; electric machinery; induction

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APA (6th Edition):

McKinnon, D. J. (2005). Novel efficiency evaluation methods and analysis for three-phase induction machines. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/21869 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:704/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

McKinnon, Douglas John. “Novel efficiency evaluation methods and analysis for three-phase induction machines.” 2005. Doctoral Dissertation, University of New South Wales. Accessed January 17, 2021. http://handle.unsw.edu.au/1959.4/21869 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:704/SOURCE01?view=true.

MLA Handbook (7th Edition):

McKinnon, Douglas John. “Novel efficiency evaluation methods and analysis for three-phase induction machines.” 2005. Web. 17 Jan 2021.

Vancouver:

McKinnon DJ. Novel efficiency evaluation methods and analysis for three-phase induction machines. [Internet] [Doctoral dissertation]. University of New South Wales; 2005. [cited 2021 Jan 17]. Available from: http://handle.unsw.edu.au/1959.4/21869 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:704/SOURCE01?view=true.

Council of Science Editors:

McKinnon DJ. Novel efficiency evaluation methods and analysis for three-phase induction machines. [Doctoral Dissertation]. University of New South Wales; 2005. Available from: http://handle.unsw.edu.au/1959.4/21869 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:704/SOURCE01?view=true

25. Bidoggia, Benoit. Fuel cell and power converter systems : model and design : Systèmes pile à combustible et convertisseur de puissance : modélisation et conception.

Degree: Docteur es, Electronique de puissance, 2009, Tours; Università degli studi (Padoue, Italie)

Les piles à combustible sont des dispositifs qui permettent de transformer directement l’énergie chimique potentielle d’un carburant en énergie électrique. Elle sont presque toujours couplées… (more)

Subjects/Keywords: Fréquence variable

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APA (6th Edition):

Bidoggia, B. (2009). Fuel cell and power converter systems : model and design : Systèmes pile à combustible et convertisseur de puissance : modélisation et conception. (Doctoral Dissertation). Tours; Università degli studi (Padoue, Italie). Retrieved from http://www.theses.fr/2009TOUR4027

Chicago Manual of Style (16th Edition):

Bidoggia, Benoit. “Fuel cell and power converter systems : model and design : Systèmes pile à combustible et convertisseur de puissance : modélisation et conception.” 2009. Doctoral Dissertation, Tours; Università degli studi (Padoue, Italie). Accessed January 17, 2021. http://www.theses.fr/2009TOUR4027.

MLA Handbook (7th Edition):

Bidoggia, Benoit. “Fuel cell and power converter systems : model and design : Systèmes pile à combustible et convertisseur de puissance : modélisation et conception.” 2009. Web. 17 Jan 2021.

Vancouver:

Bidoggia B. Fuel cell and power converter systems : model and design : Systèmes pile à combustible et convertisseur de puissance : modélisation et conception. [Internet] [Doctoral dissertation]. Tours; Università degli studi (Padoue, Italie); 2009. [cited 2021 Jan 17]. Available from: http://www.theses.fr/2009TOUR4027.

Council of Science Editors:

Bidoggia B. Fuel cell and power converter systems : model and design : Systèmes pile à combustible et convertisseur de puissance : modélisation et conception. [Doctoral Dissertation]. Tours; Università degli studi (Padoue, Italie); 2009. Available from: http://www.theses.fr/2009TOUR4027


University of California – San Diego

26. Roberts, Benjamin Zalman. Towards the Development of a Rat Model of Human Targeted Cognitive Training.

Degree: Biology, 2018, University of California – San Diego

 Cognitive deficits are characteristic symptoms of schizophrenia, but remain largely untreated. Targeted Cognitive Training (TCT), a computerized training regimen designed to enhance spared function, is… (more)

Subjects/Keywords: Biology; Behavioral sciences; Neurosciences; Auditory Sweep Discrimination Task; Rat Sweep Discrimination Task; Schizophrenia; Targeted Cognitive Training

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APA (6th Edition):

Roberts, B. Z. (2018). Towards the Development of a Rat Model of Human Targeted Cognitive Training. (Thesis). University of California – San Diego. Retrieved from http://www.escholarship.org/uc/item/12v8418r

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):

Roberts, Benjamin Zalman. “Towards the Development of a Rat Model of Human Targeted Cognitive Training.” 2018. Thesis, University of California – San Diego. Accessed January 17, 2021. http://www.escholarship.org/uc/item/12v8418r.

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

MLA Handbook (7th Edition):

Roberts, Benjamin Zalman. “Towards the Development of a Rat Model of Human Targeted Cognitive Training.” 2018. Web. 17 Jan 2021.

Vancouver:

Roberts BZ. Towards the Development of a Rat Model of Human Targeted Cognitive Training. [Internet] [Thesis]. University of California – San Diego; 2018. [cited 2021 Jan 17]. Available from: http://www.escholarship.org/uc/item/12v8418r.

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

Council of Science Editors:

Roberts BZ. Towards the Development of a Rat Model of Human Targeted Cognitive Training. [Thesis]. University of California – San Diego; 2018. Available from: http://www.escholarship.org/uc/item/12v8418r

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


Brno University of Technology

27. Paliesek, Jakub. Změření vlivu akustiky prostředí na úspěšnost rozpoznávače řeči: Measurment of Impact of Environment Acoustics on Speech Recognition Accuracy.

Degree: 2019, Brno University of Technology

 This bachelor thesis deals with investigation of impacts of acoustical parameters on automatic speech recognition (ASR) accuracy. Used ASRs were evaluated on Speecon, Temic and… (more)

Subjects/Keywords: rozpoznávanie reči; akustika; impulzná odozva; exponential sine sweep; speech recognition; acoustics; impulse response; exponential sine sweep

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APA (6th Edition):

Paliesek, J. (2019). Změření vlivu akustiky prostředí na úspěšnost rozpoznávače řeči: Measurment of Impact of Environment Acoustics on Speech Recognition Accuracy. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/85195

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):

Paliesek, Jakub. “Změření vlivu akustiky prostředí na úspěšnost rozpoznávače řeči: Measurment of Impact of Environment Acoustics on Speech Recognition Accuracy.” 2019. Thesis, Brno University of Technology. Accessed January 17, 2021. http://hdl.handle.net/11012/85195.

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

MLA Handbook (7th Edition):

Paliesek, Jakub. “Změření vlivu akustiky prostředí na úspěšnost rozpoznávače řeči: Measurment of Impact of Environment Acoustics on Speech Recognition Accuracy.” 2019. Web. 17 Jan 2021.

Vancouver:

Paliesek J. Změření vlivu akustiky prostředí na úspěšnost rozpoznávače řeči: Measurment of Impact of Environment Acoustics on Speech Recognition Accuracy. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 17]. Available from: http://hdl.handle.net/11012/85195.

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

Council of Science Editors:

Paliesek J. Změření vlivu akustiky prostředí na úspěšnost rozpoznávače řeči: Measurment of Impact of Environment Acoustics on Speech Recognition Accuracy. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/85195

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


Carnegie Mellon University

28. 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 · 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 January 17, 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. 17 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 17]. 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


Indian Institute of Science

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

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 17, 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. 17 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 17]. 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

30. 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 · 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 January 17, 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. 17 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 17]. 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

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