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You searched for +publisher:"University of Toronto" +contributor:("Lavoie, Philippe"). Showing records 1 – 19 of 19 total matches.

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University of Toronto

1. Li, Leon. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.

Degree: 2013, University of Toronto

This work is focused on the aerodynamics for a proprietary laminar flow airfoil for Unmanned Aerial Vehicle (UAV) applications. The two main focuses are (1)… (more)

Subjects/Keywords: low Reynolds number airfoil; laminar separation bubble; oil film interferometry; 0538

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APA (6th Edition):

Li, L. (2013). Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43077

Chicago Manual of Style (16th Edition):

Li, Leon. “Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.” 2013. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/43077.

MLA Handbook (7th Edition):

Li, Leon. “Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.” 2013. Web. 10 Jul 2020.

Vancouver:

Li L. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/43077.

Council of Science Editors:

Li L. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43077


University of Toronto

2. Chekiri, Rafik. Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller.

Degree: 2014, University of Toronto

An aeroacoustic study of a two-strut, two-wheel, nacelle-mounted landing gear was conducted to investigate the effects of an upstream propeller on the radiated noise. The… (more)

Subjects/Keywords: Aeroacoustics; Airframe Noise; Landing Gear Noise; 0538

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APA (6th Edition):

Chekiri, R. (2014). Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/67867

Chicago Manual of Style (16th Edition):

Chekiri, Rafik. “Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller.” 2014. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/67867.

MLA Handbook (7th Edition):

Chekiri, Rafik. “Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller.” 2014. Web. 10 Jul 2020.

Vancouver:

Chekiri R. Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/67867.

Council of Science Editors:

Chekiri R. Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/67867


University of Toronto

3. Feero, Mark. Active Control of Separation on a Low Reynolds Number Airfoil Using Synthetic Jet Actuation.

Degree: 2014, University of Toronto

Wind tunnel experiments were used to study the effect of excitation amplitude and frequency on flow separation using synthetic jet actuation. A synthetic jet actuator… (more)

Subjects/Keywords: Boundary layer; Flow control; Fluid mechanics; Synthetic jet; 0538

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APA (6th Edition):

Feero, M. (2014). Active Control of Separation on a Low Reynolds Number Airfoil Using Synthetic Jet Actuation. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/67919

Chicago Manual of Style (16th Edition):

Feero, Mark. “Active Control of Separation on a Low Reynolds Number Airfoil Using Synthetic Jet Actuation.” 2014. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/67919.

MLA Handbook (7th Edition):

Feero, Mark. “Active Control of Separation on a Low Reynolds Number Airfoil Using Synthetic Jet Actuation.” 2014. Web. 10 Jul 2020.

Vancouver:

Feero M. Active Control of Separation on a Low Reynolds Number Airfoil Using Synthetic Jet Actuation. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/67919.

Council of Science Editors:

Feero M. Active Control of Separation on a Low Reynolds Number Airfoil Using Synthetic Jet Actuation. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/67919


University of Toronto

4. Chow, Derrick. Design and Characterization of the UTIAS Anechoic Wind Tunnel.

Degree: 2016, University of Toronto

The anechoic open-jet wind tunnel facility at the University of Toronto Institute for Aerospace Studies was updated and characterized to meet the needs of current… (more)

Subjects/Keywords: aeroacoustic; anechoic; wind tunnel; 0538

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APA (6th Edition):

Chow, D. (2016). Design and Characterization of the UTIAS Anechoic Wind Tunnel. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/71668

Chicago Manual of Style (16th Edition):

Chow, Derrick. “Design and Characterization of the UTIAS Anechoic Wind Tunnel.” 2016. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/71668.

MLA Handbook (7th Edition):

Chow, Derrick. “Design and Characterization of the UTIAS Anechoic Wind Tunnel.” 2016. Web. 10 Jul 2020.

Vancouver:

Chow D. Design and Characterization of the UTIAS Anechoic Wind Tunnel. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/71668.

Council of Science Editors:

Chow D. Design and Characterization of the UTIAS Anechoic Wind Tunnel. [Masters Thesis]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/71668


University of Toronto

5. Rajasekaran, Jagannath. On the Flow Characteristics behind a Backward-facing Step and the Design of a New Axisymmetric Model for their Study.

Degree: 2011, University of Toronto

An extensive review was made to study the wake characteristics of a backward-facing step. Experimental and numerical studies of the backward-facing step suggest that the… (more)

Subjects/Keywords: separated shear flows; backward-facing step; 0538

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APA (6th Edition):

Rajasekaran, J. (2011). On the Flow Characteristics behind a Backward-facing Step and the Design of a New Axisymmetric Model for their Study. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/31402

Chicago Manual of Style (16th Edition):

Rajasekaran, Jagannath. “On the Flow Characteristics behind a Backward-facing Step and the Design of a New Axisymmetric Model for their Study.” 2011. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/31402.

MLA Handbook (7th Edition):

Rajasekaran, Jagannath. “On the Flow Characteristics behind a Backward-facing Step and the Design of a New Axisymmetric Model for their Study.” 2011. Web. 10 Jul 2020.

Vancouver:

Rajasekaran J. On the Flow Characteristics behind a Backward-facing Step and the Design of a New Axisymmetric Model for their Study. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/31402.

Council of Science Editors:

Rajasekaran J. On the Flow Characteristics behind a Backward-facing Step and the Design of a New Axisymmetric Model for their Study. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31402


University of Toronto

6. Palmeiro, Denis. Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations.

Degree: 2011, University of Toronto

Single-dielectric-barrier-discharge (SDBD) plasma actuators have shown much promise as an actuator for active flow control. Proper design and optimization of plasma actuators requires a model… (more)

Subjects/Keywords: Fluid Dynamics; Plasma Physics; 0538

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APA (6th Edition):

Palmeiro, D. (2011). Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/31378

Chicago Manual of Style (16th Edition):

Palmeiro, Denis. “Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations.” 2011. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/31378.

MLA Handbook (7th Edition):

Palmeiro, Denis. “Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations.” 2011. Web. 10 Jul 2020.

Vancouver:

Palmeiro D. Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/31378.

Council of Science Editors:

Palmeiro D. Modeling of Dielectric Barrier Discharge Plasma Actuators for Flow Control Simulations. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31378


University of Toronto

7. Yuan, Zhou. Development and Error Analysis of a Conrad Probe for Measurements of 2D Velocity in a Laminar Boundary Layer.

Degree: 2012, University of Toronto

The present study proposes to use a Conrad probe for transient growth study by measuring the two-dimensional velocity behind an array of roughness elements in… (more)

Subjects/Keywords: Conrad probe; two-dimensional velocity measurements; transient growth; look-up table method; velocity correction; laminar boundary layer; 0538

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APA (6th Edition):

Yuan, Z. (2012). Development and Error Analysis of a Conrad Probe for Measurements of 2D Velocity in a Laminar Boundary Layer. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/33601

Chicago Manual of Style (16th Edition):

Yuan, Zhou. “Development and Error Analysis of a Conrad Probe for Measurements of 2D Velocity in a Laminar Boundary Layer.” 2012. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/33601.

MLA Handbook (7th Edition):

Yuan, Zhou. “Development and Error Analysis of a Conrad Probe for Measurements of 2D Velocity in a Laminar Boundary Layer.” 2012. Web. 10 Jul 2020.

Vancouver:

Yuan Z. Development and Error Analysis of a Conrad Probe for Measurements of 2D Velocity in a Laminar Boundary Layer. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/33601.

Council of Science Editors:

Yuan Z. Development and Error Analysis of a Conrad Probe for Measurements of 2D Velocity in a Laminar Boundary Layer. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/33601


University of Toronto

8. Osmokrovic, Luke. Receptivity of Laminar Boundary Layers to Spanwise-periodic Forcing by an Array of Plasma Actuators.

Degree: 2012, University of Toronto

This work is concerned with the response of a Blasius boundary layer to dielectric-barrier-discharge (DBD) plasma actuators for the purpose of using these devices in… (more)

Subjects/Keywords: plasma actuator; transition; transient growth; laminar; boundary layer; streaks; power consumption; wind tunnel; turbulence; hot-wire; anemometry; disturbance velocity; power spectrum; nanofabrication; data collapse; electrode geometry; 0538

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APA (6th Edition):

Osmokrovic, L. (2012). Receptivity of Laminar Boundary Layers to Spanwise-periodic Forcing by an Array of Plasma Actuators. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/33483

Chicago Manual of Style (16th Edition):

Osmokrovic, Luke. “Receptivity of Laminar Boundary Layers to Spanwise-periodic Forcing by an Array of Plasma Actuators.” 2012. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/33483.

MLA Handbook (7th Edition):

Osmokrovic, Luke. “Receptivity of Laminar Boundary Layers to Spanwise-periodic Forcing by an Array of Plasma Actuators.” 2012. Web. 10 Jul 2020.

Vancouver:

Osmokrovic L. Receptivity of Laminar Boundary Layers to Spanwise-periodic Forcing by an Array of Plasma Actuators. [Internet] [Masters thesis]. University of Toronto; 2012. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/33483.

Council of Science Editors:

Osmokrovic L. Receptivity of Laminar Boundary Layers to Spanwise-periodic Forcing by an Array of Plasma Actuators. [Masters Thesis]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/33483


University of Toronto

9. Lane, Creighton. Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations.

Degree: 2018, University of Toronto

The turbulent boundary layer (TBL) noise generated inside an aircraft can have a detrimental impact on humans. In an effort to better understand TBL physics… (more)

Subjects/Keywords: Aeroacoustics; Turbulent boundary layer; Wall-pressure; 0538

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APA (6th Edition):

Lane, C. (2018). Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/89620

Chicago Manual of Style (16th Edition):

Lane, Creighton. “Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations.” 2018. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/89620.

MLA Handbook (7th Edition):

Lane, Creighton. “Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations.” 2018. Web. 10 Jul 2020.

Vancouver:

Lane C. Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/89620.

Council of Science Editors:

Lane C. Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations. [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/89620


University of Toronto

10. Azzam, Abdullah. On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid.

Degree: 2018, University of Toronto

Unsteady flows are pervasive in nature and engineering applications such as UAVs. Simulating these flows in an experimental setting is key to avoiding detrimental changes… (more)

Subjects/Keywords: active grid; unsteady aerodynamics; unsteady turbulence; 0538

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APA (6th Edition):

Azzam, A. (2018). On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/91605

Chicago Manual of Style (16th Edition):

Azzam, Abdullah. “On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid.” 2018. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/91605.

MLA Handbook (7th Edition):

Azzam, Abdullah. “On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid.” 2018. Web. 10 Jul 2020.

Vancouver:

Azzam A. On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/91605.

Council of Science Editors:

Azzam A. On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid. [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/91605


University of Toronto

11. Houser, Nicole. Manufacturing of Dielectric Barrier Discharge Plasma Actuators for Degradation Resistance.

Degree: 2013, University of Toronto

The performance and broader application of dielectric barrier discharge (DBD) plasma actuators are restricted by the manufacturing methods currently employed. In the current work, two… (more)

Subjects/Keywords: plasma actuator; degradation; 0538

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APA (6th Edition):

Houser, N. (2013). Manufacturing of Dielectric Barrier Discharge Plasma Actuators for Degradation Resistance. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/42867

Chicago Manual of Style (16th Edition):

Houser, Nicole. “Manufacturing of Dielectric Barrier Discharge Plasma Actuators for Degradation Resistance.” 2013. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/42867.

MLA Handbook (7th Edition):

Houser, Nicole. “Manufacturing of Dielectric Barrier Discharge Plasma Actuators for Degradation Resistance.” 2013. Web. 10 Jul 2020.

Vancouver:

Houser N. Manufacturing of Dielectric Barrier Discharge Plasma Actuators for Degradation Resistance. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/42867.

Council of Science Editors:

Houser N. Manufacturing of Dielectric Barrier Discharge Plasma Actuators for Degradation Resistance. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/42867


University of Toronto

12. Sutton, David Michael. Experimental Characterization of the Effects of Freestream Turbulence Intensity on the SD7003 Airfoil at Low Reynolds Numbers.

Degree: 2015, University of Toronto

The effect of freestream turbulence intensities ranging from Tu = 1.26% to Tu = 3.2% is studied. Skin friction measurements made on the surface of… (more)

Subjects/Keywords: Aerodynamics; Low Reynolds; Turbulence; UAV; 0538

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APA (6th Edition):

Sutton, D. M. (2015). Experimental Characterization of the Effects of Freestream Turbulence Intensity on the SD7003 Airfoil at Low Reynolds Numbers. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/73417

Chicago Manual of Style (16th Edition):

Sutton, David Michael. “Experimental Characterization of the Effects of Freestream Turbulence Intensity on the SD7003 Airfoil at Low Reynolds Numbers.” 2015. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/73417.

MLA Handbook (7th Edition):

Sutton, David Michael. “Experimental Characterization of the Effects of Freestream Turbulence Intensity on the SD7003 Airfoil at Low Reynolds Numbers.” 2015. Web. 10 Jul 2020.

Vancouver:

Sutton DM. Experimental Characterization of the Effects of Freestream Turbulence Intensity on the SD7003 Airfoil at Low Reynolds Numbers. [Internet] [Masters thesis]. University of Toronto; 2015. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/73417.

Council of Science Editors:

Sutton DM. Experimental Characterization of the Effects of Freestream Turbulence Intensity on the SD7003 Airfoil at Low Reynolds Numbers. [Masters Thesis]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/73417


University of Toronto

13. ZHAO, WENYI. Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body.

Degree: 2017, University of Toronto

This thesis studies the effect of turbulent boundary layer thickness on the wake dynamics of a blunt trailing edge profiled body, and investigates a flow… (more)

Subjects/Keywords: blunt trailing edge; boundary layer thickness; flow control; passive vortex generator; secondary instability; wake; 0538

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APA (6th Edition):

ZHAO, W. (2017). Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79054

Chicago Manual of Style (16th Edition):

ZHAO, WENYI. “Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body.” 2017. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/79054.

MLA Handbook (7th Edition):

ZHAO, WENYI. “Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body.” 2017. Web. 10 Jul 2020.

Vancouver:

ZHAO W. Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/79054.

Council of Science Editors:

ZHAO W. Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79054


University of Toronto

14. Zilli, Jacob. Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil.

Degree: 2017, University of Toronto

The effect of freestream turbulence intensity on the laminar separation bubble and flow transition over an SD7003 airfoil was investigated. Measurements were performed for Reynolds… (more)

Subjects/Keywords: Freestream Turbulence Effects; Laminar Separation Bubbles; Low Reynolds Airfoil; 0538

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APA (6th Edition):

Zilli, J. (2017). Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79058

Chicago Manual of Style (16th Edition):

Zilli, Jacob. “Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil.” 2017. Masters Thesis, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/79058.

MLA Handbook (7th Edition):

Zilli, Jacob. “Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil.” 2017. Web. 10 Jul 2020.

Vancouver:

Zilli J. Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/79058.

Council of Science Editors:

Zilli J. Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79058


University of Toronto

15. Hanson, Ronald. Control of Transient Growth Induced Transition in a Zero-pressure Gradient Boundary Layer Using Plasma Actuators.

Degree: 2013, University of Toronto

The level of the skin friction drag depends on the boundary layer state, either low, for the laminar case or high for the turbulent case.… (more)

Subjects/Keywords: Bypass Transition; Plasma Actuators; Transient Growth; Flow Control; Laminar Boundary Layer; 0538

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APA (6th Edition):

Hanson, R. (2013). Control of Transient Growth Induced Transition in a Zero-pressure Gradient Boundary Layer Using Plasma Actuators. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/70544

Chicago Manual of Style (16th Edition):

Hanson, Ronald. “Control of Transient Growth Induced Transition in a Zero-pressure Gradient Boundary Layer Using Plasma Actuators.” 2013. Doctoral Dissertation, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/70544.

MLA Handbook (7th Edition):

Hanson, Ronald. “Control of Transient Growth Induced Transition in a Zero-pressure Gradient Boundary Layer Using Plasma Actuators.” 2013. Web. 10 Jul 2020.

Vancouver:

Hanson R. Control of Transient Growth Induced Transition in a Zero-pressure Gradient Boundary Layer Using Plasma Actuators. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/70544.

Council of Science Editors:

Hanson R. Control of Transient Growth Induced Transition in a Zero-pressure Gradient Boundary Layer Using Plasma Actuators. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/70544


University of Toronto

16. Feero, Mark Alexander. Investigation of Synthetic Jet Flow Control Parameters for the Mitigation of Laminar Boundary Layer Separation.

Degree: PhD, 2018, University of Toronto

 An experimental study was performed to elucidate the effects of forcing parameters on the mitigation of boundary layer separation on an airfoil at low Reynolds… (more)

Subjects/Keywords: 0538

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APA (6th Edition):

Feero, M. A. (2018). Investigation of Synthetic Jet Flow Control Parameters for the Mitigation of Laminar Boundary Layer Separation. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/82937

Chicago Manual of Style (16th Edition):

Feero, Mark Alexander. “Investigation of Synthetic Jet Flow Control Parameters for the Mitigation of Laminar Boundary Layer Separation.” 2018. Doctoral Dissertation, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/82937.

MLA Handbook (7th Edition):

Feero, Mark Alexander. “Investigation of Synthetic Jet Flow Control Parameters for the Mitigation of Laminar Boundary Layer Separation.” 2018. Web. 10 Jul 2020.

Vancouver:

Feero MA. Investigation of Synthetic Jet Flow Control Parameters for the Mitigation of Laminar Boundary Layer Separation. [Internet] [Doctoral dissertation]. University of Toronto; 2018. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/82937.

Council of Science Editors:

Feero MA. Investigation of Synthetic Jet Flow Control Parameters for the Mitigation of Laminar Boundary Layer Separation. [Doctoral Dissertation]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/82937


University of Toronto

17. Hearst, Robert Jason. Fractal, Classical, and Active Grid Turbulence: From Production to Decay.

Degree: PhD, 2015, University of Toronto

 The turbulence produced in the wake of fractal grids has been shown to exhibit peculiar decay properties that contrast with expectations for canonical grid turbulence… (more)

Subjects/Keywords: fractal; homogeneous; isotropic; turbulence; 0538

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APA (6th Edition):

Hearst, R. J. (2015). Fractal, Classical, and Active Grid Turbulence: From Production to Decay. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/69306

Chicago Manual of Style (16th Edition):

Hearst, Robert Jason. “Fractal, Classical, and Active Grid Turbulence: From Production to Decay.” 2015. Doctoral Dissertation, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/69306.

MLA Handbook (7th Edition):

Hearst, Robert Jason. “Fractal, Classical, and Active Grid Turbulence: From Production to Decay.” 2015. Web. 10 Jul 2020.

Vancouver:

Hearst RJ. Fractal, Classical, and Active Grid Turbulence: From Production to Decay. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/69306.

Council of Science Editors:

Hearst RJ. Fractal, Classical, and Active Grid Turbulence: From Production to Decay. [Doctoral Dissertation]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/69306


University of Toronto

18. Clark, Heather. Characterization and Estimation of Three-dimensional Structure in Unforced and Forced Blunt Trailing Edge Wake Flows.

Degree: PhD, 2016, University of Toronto

 Blunt trailing edge airfoils offer structural and aerodynamic advantages in modern wind turbine and aircraft applications. However, penalties are introduced concurrently by vortex shedding at… (more)

Subjects/Keywords: blunt trailing edge; estimation; flow control; reduced-order modelling; surface pressure; wake flow; 0538

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APA (6th Edition):

Clark, H. (2016). Characterization and Estimation of Three-dimensional Structure in Unforced and Forced Blunt Trailing Edge Wake Flows. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/72958

Chicago Manual of Style (16th Edition):

Clark, Heather. “Characterization and Estimation of Three-dimensional Structure in Unforced and Forced Blunt Trailing Edge Wake Flows.” 2016. Doctoral Dissertation, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/72958.

MLA Handbook (7th Edition):

Clark, Heather. “Characterization and Estimation of Three-dimensional Structure in Unforced and Forced Blunt Trailing Edge Wake Flows.” 2016. Web. 10 Jul 2020.

Vancouver:

Clark H. Characterization and Estimation of Three-dimensional Structure in Unforced and Forced Blunt Trailing Edge Wake Flows. [Internet] [Doctoral dissertation]. University of Toronto; 2016. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/72958.

Council of Science Editors:

Clark H. Characterization and Estimation of Three-dimensional Structure in Unforced and Forced Blunt Trailing Edge Wake Flows. [Doctoral Dissertation]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/72958


University of Toronto

19. Sadeghi, Hamed. On the Scaling, Structure and Evolution of the Near to Intermediate Fields of the Round Turbulent Jet.

Degree: PhD, 2016, University of Toronto

 This thesis concerns the structure of turbulence and energy budget equations in the near to intermediate fields of the turbulent, round free jet. A transport… (more)

Subjects/Keywords: similarity analysis; transport equation; turbulence; turbulent jet; 0538

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

APA (6th Edition):

Sadeghi, H. (2016). On the Scaling, Structure and Evolution of the Near to Intermediate Fields of the Round Turbulent Jet. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/73152

Chicago Manual of Style (16th Edition):

Sadeghi, Hamed. “On the Scaling, Structure and Evolution of the Near to Intermediate Fields of the Round Turbulent Jet.” 2016. Doctoral Dissertation, University of Toronto. Accessed July 10, 2020. http://hdl.handle.net/1807/73152.

MLA Handbook (7th Edition):

Sadeghi, Hamed. “On the Scaling, Structure and Evolution of the Near to Intermediate Fields of the Round Turbulent Jet.” 2016. Web. 10 Jul 2020.

Vancouver:

Sadeghi H. On the Scaling, Structure and Evolution of the Near to Intermediate Fields of the Round Turbulent Jet. [Internet] [Doctoral dissertation]. University of Toronto; 2016. [cited 2020 Jul 10]. Available from: http://hdl.handle.net/1807/73152.

Council of Science Editors:

Sadeghi H. On the Scaling, Structure and Evolution of the Near to Intermediate Fields of the Round Turbulent Jet. [Doctoral Dissertation]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/73152

.