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 +publisher:"University of Arizona" +contributor:("Shkarayev, Sergey"). Showing records 1 – 14 of 14 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Arizona

1. Planchenault, Pascal. Modification of Wingtip Vortices using Pulsed and Steady Jets .

Degree: 2017, University of Arizona

 Wingtip vortices, created as a byproduct of lift, are both a hazard and a significant limiting factor in the increase of air traffic. In order… (more)

Subjects/Keywords: Aerodynamics; Balance; PIV; Vortex; Vortices; Wingtip

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Planchenault, P. (2017). Modification of Wingtip Vortices using Pulsed and Steady Jets . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/624126

Chicago Manual of Style (16th Edition):

Planchenault, Pascal. “Modification of Wingtip Vortices using Pulsed and Steady Jets .” 2017. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/624126.

MLA Handbook (7th Edition):

Planchenault, Pascal. “Modification of Wingtip Vortices using Pulsed and Steady Jets .” 2017. Web. 03 Aug 2020.

Vancouver:

Planchenault P. Modification of Wingtip Vortices using Pulsed and Steady Jets . [Internet] [Masters thesis]. University of Arizona; 2017. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/624126.

Council of Science Editors:

Planchenault P. Modification of Wingtip Vortices using Pulsed and Steady Jets . [Masters Thesis]. University of Arizona; 2017. Available from: http://hdl.handle.net/10150/624126


University of Arizona

2. Bahamonde Pascual, Rodrigo. Theoretical and Experimental Method for Determining Flow and Structural Response of Parafoil Models .

Degree: 2020, University of Arizona

 The experimental study of parafoil structures is not an easy task, as the properties of the model make testing uncertain and imprecise. Parafoils are structures… (more)

Subjects/Keywords: Aerodynamics; ANSYS; CFD; FEM; Parafoil; Structures

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bahamonde Pascual, R. (2020). Theoretical and Experimental Method for Determining Flow and Structural Response of Parafoil Models . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/641657

Chicago Manual of Style (16th Edition):

Bahamonde Pascual, Rodrigo. “Theoretical and Experimental Method for Determining Flow and Structural Response of Parafoil Models .” 2020. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/641657.

MLA Handbook (7th Edition):

Bahamonde Pascual, Rodrigo. “Theoretical and Experimental Method for Determining Flow and Structural Response of Parafoil Models .” 2020. Web. 03 Aug 2020.

Vancouver:

Bahamonde Pascual R. Theoretical and Experimental Method for Determining Flow and Structural Response of Parafoil Models . [Internet] [Masters thesis]. University of Arizona; 2020. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/641657.

Council of Science Editors:

Bahamonde Pascual R. Theoretical and Experimental Method for Determining Flow and Structural Response of Parafoil Models . [Masters Thesis]. University of Arizona; 2020. Available from: http://hdl.handle.net/10150/641657


University of Arizona

3. Stoner, Ryan Michael. Study of Swirling Jets on an Impingement Surface .

Degree: 2020, University of Arizona

 There has been extensive research performed on the turbulent jet stream flow including unimpeded and impinged flow. Vortex jet streams however has not been studied… (more)

Subjects/Keywords: Flow Interaction; Swirling Jet Stream; Wall Impingement

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Stoner, R. M. (2020). Study of Swirling Jets on an Impingement Surface . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/641704

Chicago Manual of Style (16th Edition):

Stoner, Ryan Michael. “Study of Swirling Jets on an Impingement Surface .” 2020. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/641704.

MLA Handbook (7th Edition):

Stoner, Ryan Michael. “Study of Swirling Jets on an Impingement Surface .” 2020. Web. 03 Aug 2020.

Vancouver:

Stoner RM. Study of Swirling Jets on an Impingement Surface . [Internet] [Masters thesis]. University of Arizona; 2020. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/641704.

Council of Science Editors:

Stoner RM. Study of Swirling Jets on an Impingement Surface . [Masters Thesis]. University of Arizona; 2020. Available from: http://hdl.handle.net/10150/641704


University of Arizona

4. Pidaparthi, Bharath. Stochastic Optimization of Nonlinear Energy Sinks for Nonlinear Aeroelasticity .

Degree: 2019, University of Arizona

 Nonlinear Energy Sinks (NESs) are found to be promising for mitigating vibrations passively. The focus of this thesis is to investigate the mitigation of limit… (more)

Subjects/Keywords: Aeroelasticity; Limit Cycle Oscillations; Nonlinear Energy Sinks; Stochastic Optimization; Wagner's Unsteady Aerodynamic Model

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pidaparthi, B. (2019). Stochastic Optimization of Nonlinear Energy Sinks for Nonlinear Aeroelasticity . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/636508

Chicago Manual of Style (16th Edition):

Pidaparthi, Bharath. “Stochastic Optimization of Nonlinear Energy Sinks for Nonlinear Aeroelasticity .” 2019. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/636508.

MLA Handbook (7th Edition):

Pidaparthi, Bharath. “Stochastic Optimization of Nonlinear Energy Sinks for Nonlinear Aeroelasticity .” 2019. Web. 03 Aug 2020.

Vancouver:

Pidaparthi B. Stochastic Optimization of Nonlinear Energy Sinks for Nonlinear Aeroelasticity . [Internet] [Masters thesis]. University of Arizona; 2019. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/636508.

Council of Science Editors:

Pidaparthi B. Stochastic Optimization of Nonlinear Energy Sinks for Nonlinear Aeroelasticity . [Masters Thesis]. University of Arizona; 2019. Available from: http://hdl.handle.net/10150/636508


University of Arizona

5. Footohi, Parisa. Aerodynamic Characterization of Long Range VTOL UAV .

Degree: 2018, University of Arizona

 The blended-wing-body vertical takeoff and landing unmanned aerial vehicle (BWB VTOL UAV) combines the hovering and VTOL capabilities of a helicopter with the efficiency of… (more)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Footohi, P. (2018). Aerodynamic Characterization of Long Range VTOL UAV . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/630133

Chicago Manual of Style (16th Edition):

Footohi, Parisa. “Aerodynamic Characterization of Long Range VTOL UAV .” 2018. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/630133.

MLA Handbook (7th Edition):

Footohi, Parisa. “Aerodynamic Characterization of Long Range VTOL UAV .” 2018. Web. 03 Aug 2020.

Vancouver:

Footohi P. Aerodynamic Characterization of Long Range VTOL UAV . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/630133.

Council of Science Editors:

Footohi P. Aerodynamic Characterization of Long Range VTOL UAV . [Masters Thesis]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/630133


University of Arizona

6. Boroson, Ethan Rain. Optimization Under Uncertainty of Nonlinear Energy Sinks .

Degree: 2015, University of Arizona

 Nonlinear Energy Sinks (NESs) are a promising technique for passively reducing the amplitude of vibrations. Through nonlinear stiffness properties, a NES is able to passively… (more)

Subjects/Keywords: Optimization; Uncertainty; Mechanical Engineering; NES

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Boroson, E. R. (2015). Optimization Under Uncertainty of Nonlinear Energy Sinks . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/595972

Chicago Manual of Style (16th Edition):

Boroson, Ethan Rain. “Optimization Under Uncertainty of Nonlinear Energy Sinks .” 2015. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/595972.

MLA Handbook (7th Edition):

Boroson, Ethan Rain. “Optimization Under Uncertainty of Nonlinear Energy Sinks .” 2015. Web. 03 Aug 2020.

Vancouver:

Boroson ER. Optimization Under Uncertainty of Nonlinear Energy Sinks . [Internet] [Masters thesis]. University of Arizona; 2015. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/595972.

Council of Science Editors:

Boroson ER. Optimization Under Uncertainty of Nonlinear Energy Sinks . [Masters Thesis]. University of Arizona; 2015. Available from: http://hdl.handle.net/10150/595972

7. Wilson, Lee Alexander. The Development of an Experimental Facility and Investigation of Rapidly Maneuvering Micro-Air-Vehicle Wings .

Degree: 2012, University of Arizona

 Vertical Takeoff-and-Landing (VTOL) Micro Air Vehicles (MAVs) provide a versatile operational platform which combines the capabilities of fixed wing and rotary wing MAVs. In order… (more)

Subjects/Keywords: pitching manuevers; Aerospace Engineering; Flow Visulization; Micro Air Vehicles

…Edge University of Arizona Unmanned Aerial Vehicle Volts Variable Frequency Drive Virtual… …at The University of Arizona, consists of: a closed loop open test section wind tunnel… …University of Arizona in Tucson (UA) have successfully developed a series of VTOL MAVs.2… …the University of Arizona (UA) low speed wind tunnel was used. This wind tunnel… …visualization experiments. The facility, located at the University of Arizona Department of… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wilson, L. A. (2012). The Development of an Experimental Facility and Investigation of Rapidly Maneuvering Micro-Air-Vehicle Wings . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/242382

Chicago Manual of Style (16th Edition):

Wilson, Lee Alexander. “The Development of an Experimental Facility and Investigation of Rapidly Maneuvering Micro-Air-Vehicle Wings .” 2012. Masters Thesis, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/242382.

MLA Handbook (7th Edition):

Wilson, Lee Alexander. “The Development of an Experimental Facility and Investigation of Rapidly Maneuvering Micro-Air-Vehicle Wings .” 2012. Web. 03 Aug 2020.

Vancouver:

Wilson LA. The Development of an Experimental Facility and Investigation of Rapidly Maneuvering Micro-Air-Vehicle Wings . [Internet] [Masters thesis]. University of Arizona; 2012. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/242382.

Council of Science Editors:

Wilson LA. The Development of an Experimental Facility and Investigation of Rapidly Maneuvering Micro-Air-Vehicle Wings . [Masters Thesis]. University of Arizona; 2012. Available from: http://hdl.handle.net/10150/242382

8. Fooladi, Samaneh. Distributed Point Source Method for Modeling Wave Propagation in Anisotropic Media .

Degree: 2018, University of Arizona

 Distributed Point Source Method (DPSM) is a modeling technique for solving various engineering problems including ultrasonic and electromagnetic wave propagation problems. The DPSM is extended… (more)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Fooladi, S. (2018). Distributed Point Source Method for Modeling Wave Propagation in Anisotropic Media . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/628045

Chicago Manual of Style (16th Edition):

Fooladi, Samaneh. “Distributed Point Source Method for Modeling Wave Propagation in Anisotropic Media .” 2018. Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/628045.

MLA Handbook (7th Edition):

Fooladi, Samaneh. “Distributed Point Source Method for Modeling Wave Propagation in Anisotropic Media .” 2018. Web. 03 Aug 2020.

Vancouver:

Fooladi S. Distributed Point Source Method for Modeling Wave Propagation in Anisotropic Media . [Internet] [Doctoral dissertation]. University of Arizona; 2018. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/628045.

Council of Science Editors:

Fooladi S. Distributed Point Source Method for Modeling Wave Propagation in Anisotropic Media . [Doctoral Dissertation]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/628045


University of Arizona

9. Banerjee, Sourav. Elastic Wave Propagation in Corrugated Wave Guides .

Degree: 2005, University of Arizona

 Elastic Wave propagation in structures with irregular boundaries is studied by transforming the plates with irregular surfaces to sinusoidal wave-guides. Guided elastic wave in a… (more)

Subjects/Keywords: Corrugated wave guide; Distributed Point Source Method; stop band; pass band; stress green's function; wave propagation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Banerjee, S. (2005). Elastic Wave Propagation in Corrugated Wave Guides . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/193809

Chicago Manual of Style (16th Edition):

Banerjee, Sourav. “Elastic Wave Propagation in Corrugated Wave Guides .” 2005. Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/193809.

MLA Handbook (7th Edition):

Banerjee, Sourav. “Elastic Wave Propagation in Corrugated Wave Guides .” 2005. Web. 03 Aug 2020.

Vancouver:

Banerjee S. Elastic Wave Propagation in Corrugated Wave Guides . [Internet] [Doctoral dissertation]. University of Arizona; 2005. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/193809.

Council of Science Editors:

Banerjee S. Elastic Wave Propagation in Corrugated Wave Guides . [Doctoral Dissertation]. University of Arizona; 2005. Available from: http://hdl.handle.net/10150/193809


University of Arizona

10. Koessler, Jeffrey H. Dynamic Soaring UAV Gliders .

Degree: University of Arizona

 Dynamic soaring in the atmospheric boundary layer of a vertical variation of horizontal winds over arbitrary terrain offers small unmanned aerial vehicle gliders the ability… (more)

Subjects/Keywords: dynamic; glider; soaring; uav

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Koessler, J. H. (n.d.). Dynamic Soaring UAV Gliders . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/627980

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

Chicago Manual of Style (16th Edition):

Koessler, Jeffrey H. “Dynamic Soaring UAV Gliders .” Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/627980.

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

MLA Handbook (7th Edition):

Koessler, Jeffrey H. “Dynamic Soaring UAV Gliders .” Web. 03 Aug 2020.

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

Vancouver:

Koessler JH. Dynamic Soaring UAV Gliders . [Internet] [Doctoral dissertation]. University of Arizona; [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/627980.

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

Council of Science Editors:

Koessler JH. Dynamic Soaring UAV Gliders . [Doctoral Dissertation]. University of Arizona; Available from: http://hdl.handle.net/10150/627980

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


University of Arizona

11. Krashanitsa, Roman Yurievich. An Inverse Computational Approach for the Identification of the Parameters of the Constitutive Model for Damaged Ceramics Subjected to Impact Loading .

Degree: 2005, University of Arizona

 In the present study, a computational method was developed, validated and applied for the determination of parameters of a constitutive model for a ceramic material.… (more)

Subjects/Keywords: Identification; ceramics; impact loading; constitutive model; FEM; finite difference; numerical method

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Krashanitsa, R. Y. (2005). An Inverse Computational Approach for the Identification of the Parameters of the Constitutive Model for Damaged Ceramics Subjected to Impact Loading . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/193721

Chicago Manual of Style (16th Edition):

Krashanitsa, Roman Yurievich. “An Inverse Computational Approach for the Identification of the Parameters of the Constitutive Model for Damaged Ceramics Subjected to Impact Loading .” 2005. Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/193721.

MLA Handbook (7th Edition):

Krashanitsa, Roman Yurievich. “An Inverse Computational Approach for the Identification of the Parameters of the Constitutive Model for Damaged Ceramics Subjected to Impact Loading .” 2005. Web. 03 Aug 2020.

Vancouver:

Krashanitsa RY. An Inverse Computational Approach for the Identification of the Parameters of the Constitutive Model for Damaged Ceramics Subjected to Impact Loading . [Internet] [Doctoral dissertation]. University of Arizona; 2005. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/193721.

Council of Science Editors:

Krashanitsa RY. An Inverse Computational Approach for the Identification of the Parameters of the Constitutive Model for Damaged Ceramics Subjected to Impact Loading . [Doctoral Dissertation]. University of Arizona; 2005. Available from: http://hdl.handle.net/10150/193721


University of Arizona

12. Luo, Huiyang. EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF DYNAMIC COMPRESSIVE BEHAVIOR OF INTACT AND DAMAGED CERAMICS .

Degree: 2005, University of Arizona

 The mechanical responses of the comminuted ceramic under impact is important in understanding penetration resistance of the target, modeling the penetration process, developing ceramic models… (more)

Subjects/Keywords: Ceramics; Dynamic Compressive Response; SHPB; Constitutive Behavior; Silicon Carbide; Alumina

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Luo, H. (2005). EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF DYNAMIC COMPRESSIVE BEHAVIOR OF INTACT AND DAMAGED CERAMICS . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/193906

Chicago Manual of Style (16th Edition):

Luo, Huiyang. “EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF DYNAMIC COMPRESSIVE BEHAVIOR OF INTACT AND DAMAGED CERAMICS .” 2005. Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/193906.

MLA Handbook (7th Edition):

Luo, Huiyang. “EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF DYNAMIC COMPRESSIVE BEHAVIOR OF INTACT AND DAMAGED CERAMICS .” 2005. Web. 03 Aug 2020.

Vancouver:

Luo H. EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF DYNAMIC COMPRESSIVE BEHAVIOR OF INTACT AND DAMAGED CERAMICS . [Internet] [Doctoral dissertation]. University of Arizona; 2005. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/193906.

Council of Science Editors:

Luo H. EXPERIMENTAL AND ANALYTICAL INVESTIGATION OF DYNAMIC COMPRESSIVE BEHAVIOR OF INTACT AND DAMAGED CERAMICS . [Doctoral Dissertation]. University of Arizona; 2005. Available from: http://hdl.handle.net/10150/193906


University of Arizona

13. Silin, Dmytro. AERODYNAMICS AND FLIGHT PERFORMANCE OF FLAPPING WING MICRO AIR VEHICLES .

Degree: 2010, University of Arizona

 Research efforts in this dissertation address aerodynamics and flight performance of flapping wing aircraft (ornithopters). Flapping wing aerodynamics was studied for various wing sizes, flapping… (more)

Subjects/Keywords: aerodynamics; flapping; lift; performance; testing; wing

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Silin, D. (2010). AERODYNAMICS AND FLIGHT PERFORMANCE OF FLAPPING WING MICRO AIR VEHICLES . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/194755

Chicago Manual of Style (16th Edition):

Silin, Dmytro. “AERODYNAMICS AND FLIGHT PERFORMANCE OF FLAPPING WING MICRO AIR VEHICLES .” 2010. Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/194755.

MLA Handbook (7th Edition):

Silin, Dmytro. “AERODYNAMICS AND FLIGHT PERFORMANCE OF FLAPPING WING MICRO AIR VEHICLES .” 2010. Web. 03 Aug 2020.

Vancouver:

Silin D. AERODYNAMICS AND FLIGHT PERFORMANCE OF FLAPPING WING MICRO AIR VEHICLES . [Internet] [Doctoral dissertation]. University of Arizona; 2010. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/194755.

Council of Science Editors:

Silin D. AERODYNAMICS AND FLIGHT PERFORMANCE OF FLAPPING WING MICRO AIR VEHICLES . [Doctoral Dissertation]. University of Arizona; 2010. Available from: http://hdl.handle.net/10150/194755


University of Arizona

14. Chen, Chunmei. SEPARATION AND CIRCULATION CONTROL ON A THICK BLUNT ELLIPTICAL AIRFOIL .

Degree: 2009, University of Arizona

 Various methods of Active Flow Control (AFC) were experimentally investigated on an elliptic airfoil to improve our understanding of the flow mechanisms and identify the… (more)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chen, C. (2009). SEPARATION AND CIRCULATION CONTROL ON A THICK BLUNT ELLIPTICAL AIRFOIL . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/195452

Chicago Manual of Style (16th Edition):

Chen, Chunmei. “SEPARATION AND CIRCULATION CONTROL ON A THICK BLUNT ELLIPTICAL AIRFOIL .” 2009. Doctoral Dissertation, University of Arizona. Accessed August 03, 2020. http://hdl.handle.net/10150/195452.

MLA Handbook (7th Edition):

Chen, Chunmei. “SEPARATION AND CIRCULATION CONTROL ON A THICK BLUNT ELLIPTICAL AIRFOIL .” 2009. Web. 03 Aug 2020.

Vancouver:

Chen C. SEPARATION AND CIRCULATION CONTROL ON A THICK BLUNT ELLIPTICAL AIRFOIL . [Internet] [Doctoral dissertation]. University of Arizona; 2009. [cited 2020 Aug 03]. Available from: http://hdl.handle.net/10150/195452.

Council of Science Editors:

Chen C. SEPARATION AND CIRCULATION CONTROL ON A THICK BLUNT ELLIPTICAL AIRFOIL . [Doctoral Dissertation]. University of Arizona; 2009. Available from: http://hdl.handle.net/10150/195452

.