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University of Notre Dame

1. Donald Allan Tillotson. Drag Reduction and Directional Control of a Projectile Using Plasma Actuators</h1>.

Degree: MSAeroE, Aerospace and Mechanical Engineering, 2009, University of Notre Dame

URL: https://curate.nd.edu/show/pn89d507363

► High-speed projectiles experience flow separation at their blunt downstream end. Previous research has demonstrated the ability for plasma actuators to prevent flow separation as…
(more)

Subjects/Keywords: controlability; subsonic

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APA (6^{th} Edition):

Tillotson, D. A. (2009). Drag Reduction and Directional Control of a Projectile Using Plasma Actuators</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/pn89d507363

Chicago Manual of Style (16^{th} Edition):

Tillotson, Donald Allan. “Drag Reduction and Directional Control of a Projectile Using Plasma Actuators</h1>.” 2009. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/pn89d507363.

MLA Handbook (7^{th} Edition):

Tillotson, Donald Allan. “Drag Reduction and Directional Control of a Projectile Using Plasma Actuators</h1>.” 2009. Web. 14 Oct 2019.

Vancouver:

Tillotson DA. Drag Reduction and Directional Control of a Projectile Using Plasma Actuators</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2009. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/pn89d507363.

Council of Science Editors:

Tillotson DA. Drag Reduction and Directional Control of a Projectile Using Plasma Actuators</h1>. [Masters Thesis]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/pn89d507363

University of Notre Dame

2. Joseph A. Valerioti. Pressure Dependence of Plasma Actuated Flow Control</h1>.

Degree: MSAeroE, Aerospace and Mechanical Engineering, 2010, University of Notre Dame

URL: https://curate.nd.edu/show/3x816m32x83

► Novel applications for plasma actuators necessitate performance predictions that are reliable at a range of environmental conditions. An experimental setup is used to determine…
(more)

Subjects/Keywords: space-time lumped element model; filament; plasma actuator; single dielectric barrier discharge; pressure

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APA (6^{th} Edition):

Valerioti, J. A. (2010). Pressure Dependence of Plasma Actuated Flow Control</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/3x816m32x83

Chicago Manual of Style (16^{th} Edition):

Valerioti, Joseph A.. “Pressure Dependence of Plasma Actuated Flow Control</h1>.” 2010. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/3x816m32x83.

MLA Handbook (7^{th} Edition):

Valerioti, Joseph A.. “Pressure Dependence of Plasma Actuated Flow Control</h1>.” 2010. Web. 14 Oct 2019.

Vancouver:

Valerioti JA. Pressure Dependence of Plasma Actuated Flow Control</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2010. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/3x816m32x83.

Council of Science Editors:

Valerioti JA. Pressure Dependence of Plasma Actuated Flow Control</h1>. [Masters Thesis]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/3x816m32x83

University of Notre Dame

3. Jin Hao. Aeroacoustics of Small Gaps and Steps in Low-Mach-Number Turbulent Boundary Layers</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2014, University of Notre Dame

URL: https://curate.nd.edu/show/n296ww74p4s

► The existence of small surface discontinuities beneath a turbulent boundary layer plays a significant role in generating enhanced wall-pressure fluctuations and acoustic radiation. This…
(more)

Subjects/Keywords: Turbulent Boundary Layer; Surface Pressure Fluctuation; Large-Eddy Simulation; Gap/Step Acoustic Non-Compactness; Aeroacoustics

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APA (6^{th} Edition):

Hao, J. (2014). Aeroacoustics of Small Gaps and Steps in Low-Mach-Number Turbulent Boundary Layers</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/n296ww74p4s

Chicago Manual of Style (16^{th} Edition):

Hao, Jin. “Aeroacoustics of Small Gaps and Steps in Low-Mach-Number Turbulent Boundary Layers</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/n296ww74p4s.

MLA Handbook (7^{th} Edition):

Hao, Jin. “Aeroacoustics of Small Gaps and Steps in Low-Mach-Number Turbulent Boundary Layers</h1>.” 2014. Web. 14 Oct 2019.

Vancouver:

Hao J. Aeroacoustics of Small Gaps and Steps in Low-Mach-Number Turbulent Boundary Layers</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/n296ww74p4s.

Council of Science Editors:

Hao J. Aeroacoustics of Small Gaps and Steps in Low-Mach-Number Turbulent Boundary Layers</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/n296ww74p4s

University of Notre Dame

4. Anne L Tufts. Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2018, University of Notre Dame

URL: https://curate.nd.edu/show/d217qn62j1g

► Large-eddy simulation of a turbulent shear layer interacting with a thin airfoil is performed to investigate the sound generation. The turbulent shear layer is…
(more)

Subjects/Keywords: Aeroacoustics; Large-Eddy Simulation

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APA (6^{th} Edition):

Tufts, A. L. (2018). Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/d217qn62j1g

Chicago Manual of Style (16^{th} Edition):

Tufts, Anne L. “Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>.” 2018. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/d217qn62j1g.

MLA Handbook (7^{th} Edition):

Tufts, Anne L. “Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>.” 2018. Web. 14 Oct 2019.

Vancouver:

Tufts AL. Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2018. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/d217qn62j1g.

Council of Science Editors:

Tufts AL. Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>. [Doctoral Dissertation]. University of Notre Dame; 2018. Available from: https://curate.nd.edu/show/d217qn62j1g

University of Notre Dame

5. Andrew J Lombardi. Closed-Loop Dynamic Stall Control Using a Plasma Actuator</h1>.

Degree: MSAeroE, Aerospace and Mechanical Engineering, 2011, University of Notre Dame

URL: https://curate.nd.edu/show/ws859c70f4x

► A closed-loop plasma actuated control scheme which relies on the ability to detect incipient flow separation is presented. It is known that the receptivity…
(more)

Subjects/Keywords: flow control; separation control; dynamic stall; plasma actuator; closed-loop; pitching airfoil

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APA (6^{th} Edition):

Lombardi, A. J. (2011). Closed-Loop Dynamic Stall Control Using a Plasma Actuator</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/ws859c70f4x

Chicago Manual of Style (16^{th} Edition):

Lombardi, Andrew J. “Closed-Loop Dynamic Stall Control Using a Plasma Actuator</h1>.” 2011. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/ws859c70f4x.

MLA Handbook (7^{th} Edition):

Lombardi, Andrew J. “Closed-Loop Dynamic Stall Control Using a Plasma Actuator</h1>.” 2011. Web. 14 Oct 2019.

Vancouver:

Lombardi AJ. Closed-Loop Dynamic Stall Control Using a Plasma Actuator</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2011. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/ws859c70f4x.

Council of Science Editors:

Lombardi AJ. Closed-Loop Dynamic Stall Control Using a Plasma Actuator</h1>. [Masters Thesis]. University of Notre Dame; 2011. Available from: https://curate.nd.edu/show/ws859c70f4x

University of Notre Dame

6. Cory Allen McElrath. Experimental Investigation of Suction on the Boundary Layer Flow Over a Rotating Disk</h1>.

Degree: MSAeroE, Aerospace and Mechanical Engineering, 2009, University of Notre Dame

URL: https://curate.nd.edu/show/zp38w952q53

► An experiment was performed to study the effects of applying a uniform normal flow of suction to the surface of a flat disk rotating…
(more)

Subjects/Keywords: rotating disk flow; suction; Type I crossflow instability modes

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APA (6^{th} Edition):

McElrath, C. A. (2009). Experimental Investigation of Suction on the Boundary Layer Flow Over a Rotating Disk</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/zp38w952q53

Chicago Manual of Style (16^{th} Edition):

McElrath, Cory Allen. “Experimental Investigation of Suction on the Boundary Layer Flow Over a Rotating Disk</h1>.” 2009. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/zp38w952q53.

MLA Handbook (7^{th} Edition):

McElrath, Cory Allen. “Experimental Investigation of Suction on the Boundary Layer Flow Over a Rotating Disk</h1>.” 2009. Web. 14 Oct 2019.

Vancouver:

McElrath CA. Experimental Investigation of Suction on the Boundary Layer Flow Over a Rotating Disk</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2009. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/zp38w952q53.

Council of Science Editors:

McElrath CA. Experimental Investigation of Suction on the Boundary Layer Flow Over a Rotating Disk</h1>. [Masters Thesis]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/zp38w952q53

University of Notre Dame

7. Brendan Joseph McGann. Simultaneous Species Concentration and Temperature Measurements Using Laser Induced Breakdown Spectroscopy with Direct Spectrum Matching</h1>.

Degree: MSAeroE, Aerospace and Mechanical Engineering, 2015, University of Notre Dame

URL: https://curate.nd.edu/show/4f16c24991v

► Laser induced breakdown spectroscopy (LIBS) is used to simultaneously measure hydrocarbon fuel concentration and temperature in high temperature, high speed, compressible, and reacting flows,…
(more)

Subjects/Keywords: Laser Diagnostics; Combustion; LIBS; Reacting Flows

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APA (6^{th} Edition):

McGann, B. J. (2015). Simultaneous Species Concentration and Temperature Measurements Using Laser Induced Breakdown Spectroscopy with Direct Spectrum Matching</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/4f16c24991v

Chicago Manual of Style (16^{th} Edition):

McGann, Brendan Joseph. “Simultaneous Species Concentration and Temperature Measurements Using Laser Induced Breakdown Spectroscopy with Direct Spectrum Matching</h1>.” 2015. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/4f16c24991v.

MLA Handbook (7^{th} Edition):

McGann, Brendan Joseph. “Simultaneous Species Concentration and Temperature Measurements Using Laser Induced Breakdown Spectroscopy with Direct Spectrum Matching</h1>.” 2015. Web. 14 Oct 2019.

Vancouver:

McGann BJ. Simultaneous Species Concentration and Temperature Measurements Using Laser Induced Breakdown Spectroscopy with Direct Spectrum Matching</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2015. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/4f16c24991v.

Council of Science Editors:

McGann BJ. Simultaneous Species Concentration and Temperature Measurements Using Laser Induced Breakdown Spectroscopy with Direct Spectrum Matching</h1>. [Masters Thesis]. University of Notre Dame; 2015. Available from: https://curate.nd.edu/show/4f16c24991v

University of Notre Dame

8. Qin Yang. Computational Study of Sound Generation by Surface Roughness in Turbulent Boundary Layers</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2012, University of Notre Dame

URL: https://curate.nd.edu/show/9w032229p1s

► Noise generated by flow over rough surfaces is an important issue in naval applications and in aeronautical engineering. This work numerically investigates roughness-induced noise…
(more)

Subjects/Keywords: aeroacoustics; aerodynamic noise; turbulence simulation; surface pressure fluctuations; incompressible flow

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APA (6^{th} Edition):

Yang, Q. (2012). Computational Study of Sound Generation by Surface Roughness in Turbulent Boundary Layers</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/9w032229p1s

Chicago Manual of Style (16^{th} Edition):

Yang, Qin. “Computational Study of Sound Generation by Surface Roughness in Turbulent Boundary Layers</h1>.” 2012. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/9w032229p1s.

MLA Handbook (7^{th} Edition):

Yang, Qin. “Computational Study of Sound Generation by Surface Roughness in Turbulent Boundary Layers</h1>.” 2012. Web. 14 Oct 2019.

Vancouver:

Yang Q. Computational Study of Sound Generation by Surface Roughness in Turbulent Boundary Layers</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2012. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/9w032229p1s.

Council of Science Editors:

Yang Q. Computational Study of Sound Generation by Surface Roughness in Turbulent Boundary Layers</h1>. [Doctoral Dissertation]. University of Notre Dame; 2012. Available from: https://curate.nd.edu/show/9w032229p1s

University of Notre Dame

9. Joanna Ho. Experimental Investigation of the Effect of Wall Suction on Cross-Flow Absolute Instability in a Rotating Disk Boundary Layer</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2014, University of Notre Dame

URL: https://curate.nd.edu/show/3x816m32z0n

► The proposed research is intended to investigate if wall suction in the boundary layer over a rotating disk will transform the absolute instability cross-flow…
(more)

Subjects/Keywords: rotating disk; absolute instability

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APA (6^{th} Edition):

Ho, J. (2014). Experimental Investigation of the Effect of Wall Suction on Cross-Flow Absolute Instability in a Rotating Disk Boundary Layer</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/3x816m32z0n

Chicago Manual of Style (16^{th} Edition):

Ho, Joanna. “Experimental Investigation of the Effect of Wall Suction on Cross-Flow Absolute Instability in a Rotating Disk Boundary Layer</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/3x816m32z0n.

MLA Handbook (7^{th} Edition):

Ho, Joanna. “Experimental Investigation of the Effect of Wall Suction on Cross-Flow Absolute Instability in a Rotating Disk Boundary Layer</h1>.” 2014. Web. 14 Oct 2019.

Vancouver:

Ho J. Experimental Investigation of the Effect of Wall Suction on Cross-Flow Absolute Instability in a Rotating Disk Boundary Layer</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/3x816m32z0n.

Council of Science Editors:

Ho J. Experimental Investigation of the Effect of Wall Suction on Cross-Flow Absolute Instability in a Rotating Disk Boundary Layer</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/3x816m32z0n

University of Notre Dame

10. Michael Arthur. Separation Control Using Plasma Actuators in a High Pressure Bend</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2014, University of Notre Dame

URL: https://curate.nd.edu/show/pv63fx73q51

► Wind tunnel experiments were performed with active flow control using a dielectric barrier discharge (DBD) plasma actuator to determine the effects of flow control…
(more)

Subjects/Keywords: Plasma Actuators; Aerospace Engineering

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APA (6^{th} Edition):

Arthur, M. (2014). Separation Control Using Plasma Actuators in a High Pressure Bend</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/pv63fx73q51

Chicago Manual of Style (16^{th} Edition):

Arthur, Michael. “Separation Control Using Plasma Actuators in a High Pressure Bend</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/pv63fx73q51.

MLA Handbook (7^{th} Edition):

Arthur, Michael. “Separation Control Using Plasma Actuators in a High Pressure Bend</h1>.” 2014. Web. 14 Oct 2019.

Vancouver:

Arthur M. Separation Control Using Plasma Actuators in a High Pressure Bend</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/pv63fx73q51.

Council of Science Editors:

Arthur M. Separation Control Using Plasma Actuators in a High Pressure Bend</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/pv63fx73q51

University of Notre Dame

11. Teng Wu. Nonlinear Bluff-Body Aerodynamics</h1>.

Degree: PhD, Civil Engineering and Geological Sciences, 2013, University of Notre Dame

URL: https://curate.nd.edu/show/wm117m03w99

► Wind induced effects on structures governed by the Navier-Stokes equations are not adequately represented by the conventional linear analysis framework. This shortcoming is becoming…
(more)

Subjects/Keywords: fluid-structure interaction; reduced-order modeling; bridge; nonlinearity; aerodynamics; aeroelasticity

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APA (6^{th} Edition):

Wu, T. (2013). Nonlinear Bluff-Body Aerodynamics</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/wm117m03w99

Chicago Manual of Style (16^{th} Edition):

Wu, Teng. “Nonlinear Bluff-Body Aerodynamics</h1>.” 2013. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/wm117m03w99.

MLA Handbook (7^{th} Edition):

Wu, Teng. “Nonlinear Bluff-Body Aerodynamics</h1>.” 2013. Web. 14 Oct 2019.

Vancouver:

Wu T. Nonlinear Bluff-Body Aerodynamics</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2013. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/wm117m03w99.

Council of Science Editors:

Wu T. Nonlinear Bluff-Body Aerodynamics</h1>. [Doctoral Dissertation]. University of Notre Dame; 2013. Available from: https://curate.nd.edu/show/wm117m03w99

University of Notre Dame

12. Benjamin Emery Mertz. Refinement, Validation, and Implementation of Lumped Circuit Element Model for Single Dielectric Barrier Discharge Plasma Actuators</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2010, University of Notre Dame

URL: https://curate.nd.edu/show/xw42n586h92

► Single dielectric barrier discharge (SDBD) plasma actuators have been applied to a wide variety of aerodynamic flow control applications ranging from stall suppression of…
(more)

Subjects/Keywords: empirical model; plasma actuator; lumped circuit element; model

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APA (6^{th} Edition):

Mertz, B. E. (2010). Refinement, Validation, and Implementation of Lumped Circuit Element Model for Single Dielectric Barrier Discharge Plasma Actuators</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/xw42n586h92

Chicago Manual of Style (16^{th} Edition):

Mertz, Benjamin Emery. “Refinement, Validation, and Implementation of Lumped Circuit Element Model for Single Dielectric Barrier Discharge Plasma Actuators</h1>.” 2010. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/xw42n586h92.

MLA Handbook (7^{th} Edition):

Mertz, Benjamin Emery. “Refinement, Validation, and Implementation of Lumped Circuit Element Model for Single Dielectric Barrier Discharge Plasma Actuators</h1>.” 2010. Web. 14 Oct 2019.

Vancouver:

Mertz BE. Refinement, Validation, and Implementation of Lumped Circuit Element Model for Single Dielectric Barrier Discharge Plasma Actuators</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/xw42n586h92.

Council of Science Editors:

Mertz BE. Refinement, Validation, and Implementation of Lumped Circuit Element Model for Single Dielectric Barrier Discharge Plasma Actuators</h1>. [Doctoral Dissertation]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/xw42n586h92

University of Notre Dame

13. Nicholas Giovanni De Lucca. Studies of the Pressure Field and Related Beam Jitter for Hemisphere-on-Cylinder Turrets</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2016, University of Notre Dame

URL: https://curate.nd.edu/show/0v838051c2x

► Beam jitter is defined as the unsteady variation of a laser beam’s propagation direction. For airborne directed energy systems that feature turrets, the high…
(more)

Subjects/Keywords: Flight Experiments; Fluid Dynamics; Beam Jitter; Turrets; Directed Energy; Aero-Optics

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APA (6^{th} Edition):

Lucca, N. G. D. (2016). Studies of the Pressure Field and Related Beam Jitter for Hemisphere-on-Cylinder Turrets</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/0v838051c2x

Chicago Manual of Style (16^{th} Edition):

Lucca, Nicholas Giovanni De. “Studies of the Pressure Field and Related Beam Jitter for Hemisphere-on-Cylinder Turrets</h1>.” 2016. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/0v838051c2x.

MLA Handbook (7^{th} Edition):

Lucca, Nicholas Giovanni De. “Studies of the Pressure Field and Related Beam Jitter for Hemisphere-on-Cylinder Turrets</h1>.” 2016. Web. 14 Oct 2019.

Vancouver:

Lucca NGD. Studies of the Pressure Field and Related Beam Jitter for Hemisphere-on-Cylinder Turrets</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2016. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/0v838051c2x.

Council of Science Editors:

Lucca NGD. Studies of the Pressure Field and Related Beam Jitter for Hemisphere-on-Cylinder Turrets</h1>. [Doctoral Dissertation]. University of Notre Dame; 2016. Available from: https://curate.nd.edu/show/0v838051c2x

University of Notre Dame

14. John A. Cooney, Jr. Increasing Power Generation in Horizontal Axis Wind Turbines Using Optimized Flow Control</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2014, University of Notre Dame

URL: https://curate.nd.edu/show/8w32r496w2v

► In order to effectively realize future goals for wind energy, the efficiency of wind turbines must increase beyond existing technology. One direct method for…
(more)

Subjects/Keywords: optimized performance; flow control; wind energy; wind turbine; lift control

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APA (6^{th} Edition):

John A. Cooney, J. (2014). Increasing Power Generation in Horizontal Axis Wind Turbines Using Optimized Flow Control</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/8w32r496w2v

Chicago Manual of Style (16^{th} Edition):

John A. Cooney, Jr. “Increasing Power Generation in Horizontal Axis Wind Turbines Using Optimized Flow Control</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/8w32r496w2v.

MLA Handbook (7^{th} Edition):

John A. Cooney, Jr. “Increasing Power Generation in Horizontal Axis Wind Turbines Using Optimized Flow Control</h1>.” 2014. Web. 14 Oct 2019.

Vancouver:

John A. Cooney J. Increasing Power Generation in Horizontal Axis Wind Turbines Using Optimized Flow Control</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/8w32r496w2v.

Council of Science Editors:

John A. Cooney J. Increasing Power Generation in Horizontal Axis Wind Turbines Using Optimized Flow Control</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/8w32r496w2v

University of Notre Dame

15. Thomas R. Szarek. On the Use Of Microcontrollers for Data Acquisition in an Introductory Measurments Course</h1>.

Degree: MSin Aerospace Engineering, Aerospace and Mechanical Engineering, 2003, University of Notre Dame

URL: https://curate.nd.edu/show/z029p269t3p

► A microcontroller-based, miniature data acquisition system was developed for use in a sophomore-level Introduction to Measurement course. This board demonstrates that principles of proper…
(more)

Subjects/Keywords: microprocessor

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APA (6^{th} Edition):

Szarek, T. R. (2003). On the Use Of Microcontrollers for Data Acquisition in an Introductory Measurments Course</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/z029p269t3p

Chicago Manual of Style (16^{th} Edition):

Szarek, Thomas R.. “On the Use Of Microcontrollers for Data Acquisition in an Introductory Measurments Course</h1>.” 2003. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/z029p269t3p.

MLA Handbook (7^{th} Edition):

Szarek, Thomas R.. “On the Use Of Microcontrollers for Data Acquisition in an Introductory Measurments Course</h1>.” 2003. Web. 14 Oct 2019.

Vancouver:

Szarek TR. On the Use Of Microcontrollers for Data Acquisition in an Introductory Measurments Course</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2003. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/z029p269t3p.

Council of Science Editors:

Szarek TR. On the Use Of Microcontrollers for Data Acquisition in an Introductory Measurments Course</h1>. [Masters Thesis]. University of Notre Dame; 2003. Available from: https://curate.nd.edu/show/z029p269t3p

University of Notre Dame

16. James Buckingham Leighton. Pressure and Diffusion Driven Bubble Growth on a Static Surface</h1>.

Degree: MSAeroE, Aerospace and Mechanical Engineering, 2006, University of Notre Dame

URL: https://curate.nd.edu/show/fn106w9499f

► This thesis describes the growth of gas bubbles on a static surface. During the course of normal operation, flow within devices such as pumps,…
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Subjects/Keywords: diffusion; bubble; cavitation; polytropic

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

APA (6^{th} Edition):

Leighton, J. B. (2006). Pressure and Diffusion Driven Bubble Growth on a Static Surface</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/fn106w9499f

Chicago Manual of Style (16^{th} Edition):

Leighton, James Buckingham. “Pressure and Diffusion Driven Bubble Growth on a Static Surface</h1>.” 2006. Masters Thesis, University of Notre Dame. Accessed October 14, 2019. https://curate.nd.edu/show/fn106w9499f.

MLA Handbook (7^{th} Edition):

Leighton, James Buckingham. “Pressure and Diffusion Driven Bubble Growth on a Static Surface</h1>.” 2006. Web. 14 Oct 2019.

Vancouver:

Leighton JB. Pressure and Diffusion Driven Bubble Growth on a Static Surface</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2006. [cited 2019 Oct 14]. Available from: https://curate.nd.edu/show/fn106w9499f.

Council of Science Editors:

Leighton JB. Pressure and Diffusion Driven Bubble Growth on a Static Surface</h1>. [Masters Thesis]. University of Notre Dame; 2006. Available from: https://curate.nd.edu/show/fn106w9499f