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You searched for +publisher:"University of Notre Dame" +contributor:("Meng Wang, Committee Member"). Showing records 1 – 16 of 16 total matches.

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University of Notre Dame

1. Grady Charles Crahan. Turret Optimization Using Passive Flow Control to Minimize Aero-Optic Effects</h1>.

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

  Over the past several decades, optical systems have begun to be deployed regularly on aircraft that fly at compressible flow speeds. During this time,… (more)

Subjects/Keywords: Aero Optics; Optimization

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APA (6th Edition):

Crahan, G. C. (2014). Turret Optimization Using Passive Flow Control to Minimize Aero-Optic Effects</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/v405s754p44

Chicago Manual of Style (16th Edition):

Crahan, Grady Charles. “Turret Optimization Using Passive Flow Control to Minimize Aero-Optic Effects</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/v405s754p44.

MLA Handbook (7th Edition):

Crahan, Grady Charles. “Turret Optimization Using Passive Flow Control to Minimize Aero-Optic Effects</h1>.” 2014. Web. 31 Mar 2020.

Vancouver:

Crahan GC. Turret Optimization Using Passive Flow Control to Minimize Aero-Optic Effects</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/v405s754p44.

Council of Science Editors:

Crahan GC. Turret Optimization Using Passive Flow Control to Minimize Aero-Optic Effects</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/v405s754p44


University of Notre Dame

2. Carl Ross Berntsen. The Remote Microphone Probe for Unsteady Surface Pressure Measurement</h1>.

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

  This study aimed to develop a remote microphone probe to measure unsteady surface pressure in order to localize and identify force-induced sound and/or vibration… (more)

Subjects/Keywords: unsteady surface pressure measurement; experiment; turbulent boundary layer; measurement; remote microphone probe

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APA (6th Edition):

Berntsen, C. R. (2014). The Remote Microphone Probe for Unsteady Surface Pressure Measurement</h1>. (Masters Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/dn39x061h6c

Chicago Manual of Style (16th Edition):

Berntsen, Carl Ross. “The Remote Microphone Probe for Unsteady Surface Pressure Measurement</h1>.” 2014. Masters Thesis, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/dn39x061h6c.

MLA Handbook (7th Edition):

Berntsen, Carl Ross. “The Remote Microphone Probe for Unsteady Surface Pressure Measurement</h1>.” 2014. Web. 31 Mar 2020.

Vancouver:

Berntsen CR. The Remote Microphone Probe for Unsteady Surface Pressure Measurement</h1>. [Internet] [Masters thesis]. University of Notre Dame; 2014. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/dn39x061h6c.

Council of Science Editors:

Berntsen CR. The Remote Microphone Probe for Unsteady Surface Pressure Measurement</h1>. [Masters Thesis]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/dn39x061h6c


University of Notre Dame

3. Kan Wang. Computational Investigation of Aero-Optical Distortions by Turbulent Boundary Layers and Separated Shear Layers</h1>.

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

  Aero-optical distortions are detrimental to airborne optical systems. To study distortion mechanisms, compressible large-eddy simulations are performed for a Mach 0.5 turbulent boundary layer… (more)

Subjects/Keywords: aero-optics; compressible flows; turbulence simulation

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APA (6th Edition):

Wang, K. (2012). Computational Investigation of Aero-Optical Distortions by Turbulent Boundary Layers and Separated Shear Layers</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/9p29086341n

Chicago Manual of Style (16th Edition):

Wang, Kan. “Computational Investigation of Aero-Optical Distortions by Turbulent Boundary Layers and Separated Shear Layers</h1>.” 2012. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/9p29086341n.

MLA Handbook (7th Edition):

Wang, Kan. “Computational Investigation of Aero-Optical Distortions by Turbulent Boundary Layers and Separated Shear Layers</h1>.” 2012. Web. 31 Mar 2020.

Vancouver:

Wang K. Computational Investigation of Aero-Optical Distortions by Turbulent Boundary Layers and Separated Shear Layers</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2012. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/9p29086341n.

Council of Science Editors:

Wang K. Computational Investigation of Aero-Optical Distortions by Turbulent Boundary Layers and Separated Shear Layers</h1>. [Doctoral Dissertation]. University of Notre Dame; 2012. Available from: https://curate.nd.edu/show/9p29086341n


University of Notre Dame

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

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

  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 (6th 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 (16th Edition):

Wu, Teng. “Nonlinear Bluff-Body Aerodynamics</h1>.” 2013. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/wm117m03w99.

MLA Handbook (7th Edition):

Wu, Teng. “Nonlinear Bluff-Body Aerodynamics</h1>.” 2013. Web. 31 Mar 2020.

Vancouver:

Wu T. Nonlinear Bluff-Body Aerodynamics</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2013. [cited 2020 Mar 31]. 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

5. Paul Edward Slaboch. Fluid Mechanics and Passive Control of the Flow-Excited Helmholtz Resonator</h1>.

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

  A flow excited Helmholtz resonator was investigated experimentally and theoretically. The analysis was focused on a simplified momentum balance integrated over the region of… (more)

Subjects/Keywords: PIV; flow excited resonance; window buffeting; Helmholz Resonator

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APA (6th Edition):

Slaboch, P. E. (2009). Fluid Mechanics and Passive Control of the Flow-Excited Helmholtz Resonator</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/cz30pr78j0g

Chicago Manual of Style (16th Edition):

Slaboch, Paul Edward. “Fluid Mechanics and Passive Control of the Flow-Excited Helmholtz Resonator</h1>.” 2009. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/cz30pr78j0g.

MLA Handbook (7th Edition):

Slaboch, Paul Edward. “Fluid Mechanics and Passive Control of the Flow-Excited Helmholtz Resonator</h1>.” 2009. Web. 31 Mar 2020.

Vancouver:

Slaboch PE. Fluid Mechanics and Passive Control of the Flow-Excited Helmholtz Resonator</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2009. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/cz30pr78j0g.

Council of Science Editors:

Slaboch PE. Fluid Mechanics and Passive Control of the Flow-Excited Helmholtz Resonator</h1>. [Doctoral Dissertation]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/cz30pr78j0g


University of Notre Dame

6. Jason Robert Tomko. Fluid-Loaded Vibration of Thin Structures Due to Turbulent Excitation</h1>.

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

  Flow-induced structural acoustics involves the study of the vibration of a structure induced by a fluid flow as well as the resulting sound generated… (more)

Subjects/Keywords: duct vibration; structural vibration; ducted rotor; duct acoustics; fluid loading; duct; velocimetry

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APA (6th Edition):

Tomko, J. R. (2014). Fluid-Loaded Vibration of Thin Structures Due to Turbulent Excitation</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/2514nk33v98

Chicago Manual of Style (16th Edition):

Tomko, Jason Robert. “Fluid-Loaded Vibration of Thin Structures Due to Turbulent Excitation</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/2514nk33v98.

MLA Handbook (7th Edition):

Tomko, Jason Robert. “Fluid-Loaded Vibration of Thin Structures Due to Turbulent Excitation</h1>.” 2014. Web. 31 Mar 2020.

Vancouver:

Tomko JR. Fluid-Loaded Vibration of Thin Structures Due to Turbulent Excitation</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/2514nk33v98.

Council of Science Editors:

Tomko JR. Fluid-Loaded Vibration of Thin Structures Due to Turbulent Excitation</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/2514nk33v98


University of Notre Dame

7. Jonathan C Silver. The Acoustics and Unsteady Wall Pressure of a Circulation Control Airfoil</h1>.

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

  A Circulation Control (CC) airfoil uses a wall jet exiting onto a rounded trailing edge to generate lift via the Coanda effect. The aerodynamics… (more)

Subjects/Keywords: howe model; unsteady wall pressure; circulation control; cc airfoil; rmp; acoustics; curle’s equation; coanda jet

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APA (6th Edition):

Silver, J. C. (2014). The Acoustics and Unsteady Wall Pressure of a Circulation Control Airfoil</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/zw12z319876

Chicago Manual of Style (16th Edition):

Silver, Jonathan C. “The Acoustics and Unsteady Wall Pressure of a Circulation Control Airfoil</h1>.” 2014. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/zw12z319876.

MLA Handbook (7th Edition):

Silver, Jonathan C. “The Acoustics and Unsteady Wall Pressure of a Circulation Control Airfoil</h1>.” 2014. Web. 31 Mar 2020.

Vancouver:

Silver JC. The Acoustics and Unsteady Wall Pressure of a Circulation Control Airfoil</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2014. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/zw12z319876.

Council of Science Editors:

Silver JC. The Acoustics and Unsteady Wall Pressure of a Circulation Control Airfoil</h1>. [Doctoral Dissertation]. University of Notre Dame; 2014. Available from: https://curate.nd.edu/show/zw12z319876


University of Notre Dame

8. Donald Wittich. Subsonic Flow over Open and Partially Covered, Rectangular Cavities</h1>.

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

  The unsteady pressure and optical properties of subsonic flow over open and partially covered rectangular cavities were investigated through a series of wind-tunnel experiments.… (more)

Subjects/Keywords: fluid dynamics

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APA (6th Edition):

Wittich, D. (2009). Subsonic Flow over Open and Partially Covered, Rectangular Cavities</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/47429882s5v

Chicago Manual of Style (16th Edition):

Wittich, Donald. “Subsonic Flow over Open and Partially Covered, Rectangular Cavities</h1>.” 2009. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/47429882s5v.

MLA Handbook (7th Edition):

Wittich, Donald. “Subsonic Flow over Open and Partially Covered, Rectangular Cavities</h1>.” 2009. Web. 31 Mar 2020.

Vancouver:

Wittich D. Subsonic Flow over Open and Partially Covered, Rectangular Cavities</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2009. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/47429882s5v.

Council of Science Editors:

Wittich D. Subsonic Flow over Open and Partially Covered, Rectangular Cavities</h1>. [Doctoral Dissertation]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/47429882s5v


University of Notre Dame

9. Alice M. Nightingale. Adaptive-Optic Approach to Mitigating Aero-Optic Disturbances for a Forced Shear Layer</h1>.

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

  Non-uniform, variable-density fields, resulting from compressibility effects in turbulent flows, are the source of aero-optical distortions which cause significant reductions in optical system performance.… (more)

Subjects/Keywords: flow control; Adaptive-Optic controller; optical shear layer charaterization; phase-lock-loop

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APA (6th Edition):

Nightingale, A. M. (2010). Adaptive-Optic Approach to Mitigating Aero-Optic Disturbances for a Forced Shear Layer</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/kk91fj25g8b

Chicago Manual of Style (16th Edition):

Nightingale, Alice M.. “Adaptive-Optic Approach to Mitigating Aero-Optic Disturbances for a Forced Shear Layer</h1>.” 2010. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/kk91fj25g8b.

MLA Handbook (7th Edition):

Nightingale, Alice M.. “Adaptive-Optic Approach to Mitigating Aero-Optic Disturbances for a Forced Shear Layer</h1>.” 2010. Web. 31 Mar 2020.

Vancouver:

Nightingale AM. Adaptive-Optic Approach to Mitigating Aero-Optic Disturbances for a Forced Shear Layer</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/kk91fj25g8b.

Council of Science Editors:

Nightingale AM. Adaptive-Optic Approach to Mitigating Aero-Optic Disturbances for a Forced Shear Layer</h1>. [Doctoral Dissertation]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/kk91fj25g8b


University of Notre Dame

10. Alexey Vitalyevich Kozlov. Plasma Actuators for Bluff Body Flow Control</h1>.

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

  The aerodynamic plasma actuators have shown to be efficient flow control devices in various applications. In this study the results of flow control experiments… (more)

Subjects/Keywords: subcritical flow; plasma actuator; cylinder in a crossflow; tandem cylinder; subsonic flow; flow control

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APA (6th Edition):

Kozlov, A. V. (2010). Plasma Actuators for Bluff Body Flow Control</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/4j03cz32m4k

Chicago Manual of Style (16th Edition):

Kozlov, Alexey Vitalyevich. “Plasma Actuators for Bluff Body Flow Control</h1>.” 2010. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/4j03cz32m4k.

MLA Handbook (7th Edition):

Kozlov, Alexey Vitalyevich. “Plasma Actuators for Bluff Body Flow Control</h1>.” 2010. Web. 31 Mar 2020.

Vancouver:

Kozlov AV. Plasma Actuators for Bluff Body Flow Control</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/4j03cz32m4k.

Council of Science Editors:

Kozlov AV. Plasma Actuators for Bluff Body Flow Control</h1>. [Doctoral Dissertation]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/4j03cz32m4k


University of Notre Dame

11. Ashraf N Al-Khateeb. Fine Scale Phenomena in Reacting Systems: Identification and Analysis for Their Reduction</h1>.

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

  A robust method for rational reduction of chemically reacting models is developed using a rigorous scale analysis. All the physical scales, spatial and temporal,… (more)

Subjects/Keywords: multicomponent transport; dimensional reduction; scale analysis; manifold method; detailed kinetics; premixed flame

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APA (6th Edition):

Al-Khateeb, A. N. (2010). Fine Scale Phenomena in Reacting Systems: Identification and Analysis for Their Reduction</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/3197xk83c7t

Chicago Manual of Style (16th Edition):

Al-Khateeb, Ashraf N. “Fine Scale Phenomena in Reacting Systems: Identification and Analysis for Their Reduction</h1>.” 2010. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/3197xk83c7t.

MLA Handbook (7th Edition):

Al-Khateeb, Ashraf N. “Fine Scale Phenomena in Reacting Systems: Identification and Analysis for Their Reduction</h1>.” 2010. Web. 31 Mar 2020.

Vancouver:

Al-Khateeb AN. Fine Scale Phenomena in Reacting Systems: Identification and Analysis for Their Reduction</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/3197xk83c7t.

Council of Science Editors:

Al-Khateeb AN. Fine Scale Phenomena in Reacting Systems: Identification and Analysis for Their Reduction</h1>. [Doctoral Dissertation]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/3197xk83c7t


University of Notre Dame

12. Adam Edwin Smith. Evaluation of Passive Boundary Layer Flow Control Techniques for Aero-Optic Mitigation</h1>.

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

  The effect of two passive boundary layer flow control techniques, Large-Eddy Break-Up (LEBU) devices and wall heating/cooling, on turbulent boundary layer induced aero-optical aberrations… (more)

Subjects/Keywords: LEBU; turbulent boundary layer; flow control; Aero-optics

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APA (6th Edition):

Smith, A. E. (2015). Evaluation of Passive Boundary Layer Flow Control Techniques for Aero-Optic Mitigation</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/q237hq4074k

Chicago Manual of Style (16th Edition):

Smith, Adam Edwin. “Evaluation of Passive Boundary Layer Flow Control Techniques for Aero-Optic Mitigation</h1>.” 2015. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/q237hq4074k.

MLA Handbook (7th Edition):

Smith, Adam Edwin. “Evaluation of Passive Boundary Layer Flow Control Techniques for Aero-Optic Mitigation</h1>.” 2015. Web. 31 Mar 2020.

Vancouver:

Smith AE. Evaluation of Passive Boundary Layer Flow Control Techniques for Aero-Optic Mitigation</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2015. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/q237hq4074k.

Council of Science Editors:

Smith AE. Evaluation of Passive Boundary Layer Flow Control Techniques for Aero-Optic Mitigation</h1>. [Doctoral Dissertation]. University of Notre Dame; 2015. Available from: https://curate.nd.edu/show/q237hq4074k


University of Notre Dame

13. Ryan T. Kelly. Numerical Prediction of the Spatial and Temporal Characteristics of the Aero-Optical Disturbance Produced by a Helicopter in Hover</h1>.

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

  Aero-optical disturbances produced from turbulent compressible flow-fields can seriously degrade the performance of an optical signal. At compressible flight speeds these disturbances stem from… (more)

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APA (6th Edition):

Kelly, R. T. (2015). Numerical Prediction of the Spatial and Temporal Characteristics of the Aero-Optical Disturbance Produced by a Helicopter in Hover</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/jd472v2654b

Chicago Manual of Style (16th Edition):

Kelly, Ryan T.. “Numerical Prediction of the Spatial and Temporal Characteristics of the Aero-Optical Disturbance Produced by a Helicopter in Hover</h1>.” 2015. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/jd472v2654b.

MLA Handbook (7th Edition):

Kelly, Ryan T.. “Numerical Prediction of the Spatial and Temporal Characteristics of the Aero-Optical Disturbance Produced by a Helicopter in Hover</h1>.” 2015. Web. 31 Mar 2020.

Vancouver:

Kelly RT. Numerical Prediction of the Spatial and Temporal Characteristics of the Aero-Optical Disturbance Produced by a Helicopter in Hover</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2015. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/jd472v2654b.

Council of Science Editors:

Kelly RT. Numerical Prediction of the Spatial and Temporal Characteristics of the Aero-Optical Disturbance Produced by a Helicopter in Hover</h1>. [Doctoral Dissertation]. University of Notre Dame; 2015. Available from: https://curate.nd.edu/show/jd472v2654b


University of Notre Dame

14. Jacob Allen Cress. Optical Aberrations Caused by Coherent Structures in a Subsonic, Compressible, Turbulent Boundary Layer</h1>.

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

  The relationship between optical aberrations and coherent structures in the turbulent boundary layer is investigated in a series of experiments. A statistical model is… (more)

Subjects/Keywords: communication; boundary layer; aero-optics

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APA (6th Edition):

Cress, J. A. (2010). Optical Aberrations Caused by Coherent Structures in a Subsonic, Compressible, Turbulent Boundary Layer</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/tb09j388g29

Chicago Manual of Style (16th Edition):

Cress, Jacob Allen. “Optical Aberrations Caused by Coherent Structures in a Subsonic, Compressible, Turbulent Boundary Layer</h1>.” 2010. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/tb09j388g29.

MLA Handbook (7th Edition):

Cress, Jacob Allen. “Optical Aberrations Caused by Coherent Structures in a Subsonic, Compressible, Turbulent Boundary Layer</h1>.” 2010. Web. 31 Mar 2020.

Vancouver:

Cress JA. Optical Aberrations Caused by Coherent Structures in a Subsonic, Compressible, Turbulent Boundary Layer</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/tb09j388g29.

Council of Science Editors:

Cress JA. Optical Aberrations Caused by Coherent Structures in a Subsonic, Compressible, Turbulent Boundary Layer</h1>. [Doctoral Dissertation]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/tb09j388g29


University of Notre Dame

15. David Bruce Stephens. Sound Sources in a Low Speed Ducted Rotor</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2008, University of Notre Dame

  The objective of this research was to improve the understanding of the sound source mechanisms in a low speed ducted fan through experimental and… (more)

Subjects/Keywords: ducted rotor sound

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APA (6th Edition):

Stephens, D. B. (2008). Sound Sources in a Low Speed Ducted Rotor</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/ns064457m51

Chicago Manual of Style (16th Edition):

Stephens, David Bruce. “Sound Sources in a Low Speed Ducted Rotor</h1>.” 2008. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/ns064457m51.

MLA Handbook (7th Edition):

Stephens, David Bruce. “Sound Sources in a Low Speed Ducted Rotor</h1>.” 2008. Web. 31 Mar 2020.

Vancouver:

Stephens DB. Sound Sources in a Low Speed Ducted Rotor</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2008. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/ns064457m51.

Council of Science Editors:

Stephens DB. Sound Sources in a Low Speed Ducted Rotor</h1>. [Doctoral Dissertation]. University of Notre Dame; 2008. Available from: https://curate.nd.edu/show/ns064457m51


University of Notre Dame

16. Daniel W Shannon. Flow Field and Acoustic Measurements of a Blunt Trailing Edge</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2007, University of Notre Dame

  This dissertation presents experimental results regarding the phenomenon of trailing edge noise. The objective of the present research was to experimentally measure flow field… (more)

Subjects/Keywords: Acoustic Array; Trailing Edge Noise; PIV; Aeroacoustics; Beamforming

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APA (6th Edition):

Shannon, D. W. (2007). Flow Field and Acoustic Measurements of a Blunt Trailing Edge</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/4t64gm82f29

Chicago Manual of Style (16th Edition):

Shannon, Daniel W. “Flow Field and Acoustic Measurements of a Blunt Trailing Edge</h1>.” 2007. Doctoral Dissertation, University of Notre Dame. Accessed March 31, 2020. https://curate.nd.edu/show/4t64gm82f29.

MLA Handbook (7th Edition):

Shannon, Daniel W. “Flow Field and Acoustic Measurements of a Blunt Trailing Edge</h1>.” 2007. Web. 31 Mar 2020.

Vancouver:

Shannon DW. Flow Field and Acoustic Measurements of a Blunt Trailing Edge</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2007. [cited 2020 Mar 31]. Available from: https://curate.nd.edu/show/4t64gm82f29.

Council of Science Editors:

Shannon DW. Flow Field and Acoustic Measurements of a Blunt Trailing Edge</h1>. [Doctoral Dissertation]. University of Notre Dame; 2007. Available from: https://curate.nd.edu/show/4t64gm82f29

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