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You searched for +publisher:"University of Cincinnati" +contributor:("Gutmark, Ephraim"). Showing records 1 – 30 of 35 total matches.

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University of Cincinnati

1. Cuppoletti, Daniel R. Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 Supersonic jets provide unique challenges in the aeroacoustic field due to very high jet velocities, shock associated noise components, flow dependence on jet expansion, and… (more)

Subjects/Keywords: Aerospace Materials; Jet Noise; Aeroacoustics; Fluid Dynamics; Particle Image Velocimetry; Acoustics; Supersonic

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APA (6th Edition):

Cuppoletti, D. R. (2013). Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927

Chicago Manual of Style (16th Edition):

Cuppoletti, Daniel R. “Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques.” 2013. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927.

MLA Handbook (7th Edition):

Cuppoletti, Daniel R. “Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques.” 2013. Web. 16 Sep 2019.

Vancouver:

Cuppoletti DR. Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques. [Internet] [Doctoral dissertation]. University of Cincinnati; 2013. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927.

Council of Science Editors:

Cuppoletti DR. Supersonic Jet Noise Reduction with Novel Fluidic Injection Techniques. [Doctoral Dissertation]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1384333927


University of Cincinnati

2. Hummer, Christopher J. Computational Study of a Plate Mounted Finite Cylinder: Aspect Ratio and Boundary Layer Thickness Effects.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 The integration of protrusions on aircraft, whether they are antennas or sensorturrets, can impact both aircraft safety and performance. The protrusions vary in sizeand shape… (more)

Subjects/Keywords: Aerospace Materials; protrusion; turret; finite cylinder; aspect ratio; thickness; flow

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APA (6th Edition):

Hummer, C. J. (2013). Computational Study of a Plate Mounted Finite Cylinder: Aspect Ratio and Boundary Layer Thickness Effects. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377869576

Chicago Manual of Style (16th Edition):

Hummer, Christopher J. “Computational Study of a Plate Mounted Finite Cylinder: Aspect Ratio and Boundary Layer Thickness Effects.” 2013. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377869576.

MLA Handbook (7th Edition):

Hummer, Christopher J. “Computational Study of a Plate Mounted Finite Cylinder: Aspect Ratio and Boundary Layer Thickness Effects.” 2013. Web. 16 Sep 2019.

Vancouver:

Hummer CJ. Computational Study of a Plate Mounted Finite Cylinder: Aspect Ratio and Boundary Layer Thickness Effects. [Internet] [Masters thesis]. University of Cincinnati; 2013. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377869576.

Council of Science Editors:

Hummer CJ. Computational Study of a Plate Mounted Finite Cylinder: Aspect Ratio and Boundary Layer Thickness Effects. [Masters Thesis]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377869576


University of Cincinnati

3. Grage, Danielle L. Study of jet exhaust noise sources and their mitigation through lobed mixers and chevrons.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2011, University of Cincinnati

 As regulations to reduce noise pollution become more stringent, understanding the noise sources within jet exhaust and how they can be mitigated is important as… (more)

Subjects/Keywords: Aerospace Materials; jet exhaust; lobed mixer; acoustic; chevron; PIV; CFD

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APA (6th Edition):

Grage, D. L. (2011). Study of jet exhaust noise sources and their mitigation through lobed mixers and chevrons. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323368

Chicago Manual of Style (16th Edition):

Grage, Danielle L. “Study of jet exhaust noise sources and their mitigation through lobed mixers and chevrons.” 2011. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323368.

MLA Handbook (7th Edition):

Grage, Danielle L. “Study of jet exhaust noise sources and their mitigation through lobed mixers and chevrons.” 2011. Web. 16 Sep 2019.

Vancouver:

Grage DL. Study of jet exhaust noise sources and their mitigation through lobed mixers and chevrons. [Internet] [Masters thesis]. University of Cincinnati; 2011. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323368.

Council of Science Editors:

Grage DL. Study of jet exhaust noise sources and their mitigation through lobed mixers and chevrons. [Masters Thesis]. University of Cincinnati; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323368


University of Cincinnati

4. Mindel, Scott A. Design of Experimental Facility to Simulate Pulsating Flow Through a Blockage.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2011, University of Cincinnati

  In order to investigate the feasibility of noninvasively detecting blockages in pipelines, experimental research was by designing a facility at the University of Cincinnati(more)

Subjects/Keywords: Aerospace Materials; Coronary Artery Disease Detection; Pipe Flow; Blockages in Pipes; Pulsating Flow

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APA (6th Edition):

Mindel, S. A. (2011). Design of Experimental Facility to Simulate Pulsating Flow Through a Blockage. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307457366

Chicago Manual of Style (16th Edition):

Mindel, Scott A. “Design of Experimental Facility to Simulate Pulsating Flow Through a Blockage.” 2011. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307457366.

MLA Handbook (7th Edition):

Mindel, Scott A. “Design of Experimental Facility to Simulate Pulsating Flow Through a Blockage.” 2011. Web. 16 Sep 2019.

Vancouver:

Mindel SA. Design of Experimental Facility to Simulate Pulsating Flow Through a Blockage. [Internet] [Masters thesis]. University of Cincinnati; 2011. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307457366.

Council of Science Editors:

Mindel SA. Design of Experimental Facility to Simulate Pulsating Flow Through a Blockage. [Masters Thesis]. University of Cincinnati; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307457366


University of Cincinnati

5. Pinchak, Matthew D. Enhanced Flame Stability and Control: The Reacting Jet in Vitiated Cross-Flow and Ozone-Assisted Combustion.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 The operation of gas turbine engines in increasingly harsh environments while constrained by stringent emissions regulations requires multiple advances in combustion technology. This dissertation addresses… (more)

Subjects/Keywords: Aerospace Materials; Reacting jet in cross flow; Plasma-assisted combustion; Ozone-Assisted Combustion; Particle image velocimetry; Fluidic flame stabilization

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APA (6th Edition):

Pinchak, M. D. (2018). Enhanced Flame Stability and Control: The Reacting Jet in Vitiated Cross-Flow and Ozone-Assisted Combustion. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1522319737952261

Chicago Manual of Style (16th Edition):

Pinchak, Matthew D. “Enhanced Flame Stability and Control: The Reacting Jet in Vitiated Cross-Flow and Ozone-Assisted Combustion.” 2018. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1522319737952261.

MLA Handbook (7th Edition):

Pinchak, Matthew D. “Enhanced Flame Stability and Control: The Reacting Jet in Vitiated Cross-Flow and Ozone-Assisted Combustion.” 2018. Web. 16 Sep 2019.

Vancouver:

Pinchak MD. Enhanced Flame Stability and Control: The Reacting Jet in Vitiated Cross-Flow and Ozone-Assisted Combustion. [Internet] [Doctoral dissertation]. University of Cincinnati; 2018. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1522319737952261.

Council of Science Editors:

Pinchak MD. Enhanced Flame Stability and Control: The Reacting Jet in Vitiated Cross-Flow and Ozone-Assisted Combustion. [Doctoral Dissertation]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1522319737952261


University of Cincinnati

6. Aghasi, Paul P. Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 To investigate the viability of using additive manufacturing technology for flat plate film cooling experiments a new experiential facility was constructed using gas analysis and… (more)

Subjects/Keywords: Aerospace Materials; Film Cooling; Heat transfer; mass transfer; pressure sensitive paint; roughness; 3D printing

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APA (6th Edition):

Aghasi, P. P. (2016). Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416

Chicago Manual of Style (16th Edition):

Aghasi, Paul P. “Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes.” 2016. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416.

MLA Handbook (7th Edition):

Aghasi, Paul P. “Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes.” 2016. Web. 16 Sep 2019.

Vancouver:

Aghasi PP. Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416.

Council of Science Editors:

Aghasi PP. Dependence of Film Cooling Effectiveness on 3D Printed Cooling Holes. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893416


University of Cincinnati

7. Driscoll, Robert B. Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 An experimental study is conducted on a Pulse Detonation Engine-Crossover System to investigate the feasibility of repeated, shock-initiated combustion and characterize the initiation performance. A… (more)

Subjects/Keywords: Aerospace Materials; Detonation; Pulse Detonation Engine; Rotating Detonation Engine; PDE-Crossover System; Reactant Injection Mixing

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APA (6th Edition):

Driscoll, R. B. (2016). Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1459155478

Chicago Manual of Style (16th Edition):

Driscoll, Robert B. “Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1459155478.

MLA Handbook (7th Edition):

Driscoll, Robert B. “Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System.” 2016. Web. 16 Sep 2019.

Vancouver:

Driscoll RB. Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1459155478.

Council of Science Editors:

Driscoll RB. Investigation of Sustained Detonation Devices: the Pulse Detonation Engine-Crossover System and the Rotating Detonation Engine System. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1459155478


University of Cincinnati

8. Farbos De Luzan, Charles. Numerical Analysis of Turbulent Flows in Channels of Complex Geometry.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 The current study proposes to follow a systematic validated approach to applied fluid mechanics problems in order to evaluate the ability of different computational fluid… (more)

Subjects/Keywords: Aerospace Materials; aerodynamics; fluidics; computational fluid dynamics; turbulence modeling

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APA (6th Edition):

Farbos De Luzan, C. (2016). Numerical Analysis of Turbulent Flows in Channels of Complex Geometry. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1468511618

Chicago Manual of Style (16th Edition):

Farbos De Luzan, Charles. “Numerical Analysis of Turbulent Flows in Channels of Complex Geometry.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1468511618.

MLA Handbook (7th Edition):

Farbos De Luzan, Charles. “Numerical Analysis of Turbulent Flows in Channels of Complex Geometry.” 2016. Web. 16 Sep 2019.

Vancouver:

Farbos De Luzan C. Numerical Analysis of Turbulent Flows in Channels of Complex Geometry. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1468511618.

Council of Science Editors:

Farbos De Luzan C. Numerical Analysis of Turbulent Flows in Channels of Complex Geometry. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1468511618


University of Cincinnati

9. Wilhite, Jarred M. Investigation of Various Novel Air-Breathing Propulsion Systems.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 The current research investigates the operation and performance of various air-breathing propulsion systems, which are capable of utilizing different types of fuel. This study first… (more)

Subjects/Keywords: Aerospace Materials; Rotating Detonation Engine; RDE; Inverse Brayton Cycle

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APA (6th Edition):

Wilhite, J. M. (2016). Investigation of Various Novel Air-Breathing Propulsion Systems. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin147981623341895

Chicago Manual of Style (16th Edition):

Wilhite, Jarred M. “Investigation of Various Novel Air-Breathing Propulsion Systems.” 2016. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin147981623341895.

MLA Handbook (7th Edition):

Wilhite, Jarred M. “Investigation of Various Novel Air-Breathing Propulsion Systems.” 2016. Web. 16 Sep 2019.

Vancouver:

Wilhite JM. Investigation of Various Novel Air-Breathing Propulsion Systems. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin147981623341895.

Council of Science Editors:

Wilhite JM. Investigation of Various Novel Air-Breathing Propulsion Systems. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin147981623341895


University of Cincinnati

10. Heeb, Nicholas S. Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2015, University of Cincinnati

 An experimental investigation into the effect of azimuthal variance of chevrons and fluidically enhanced chevrons applied to supersonic jets is presented. Flow field measurements of… (more)

Subjects/Keywords: Aerospace Materials; Supersonic Jet; Aeroacoustics; Jet Noise; Chevrons; Fluidic Injection; Compressible Flow

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APA (6th Edition):

Heeb, N. S. (2015). Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666

Chicago Manual of Style (16th Edition):

Heeb, Nicholas S. “Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets.” 2015. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666.

MLA Handbook (7th Edition):

Heeb, Nicholas S. “Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets.” 2015. Web. 16 Sep 2019.

Vancouver:

Heeb NS. Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets. [Internet] [Doctoral dissertation]. University of Cincinnati; 2015. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666.

Council of Science Editors:

Heeb NS. Azimuthally Varying Noise Reduction Techniques Applied to Supersonic Jets. [Doctoral Dissertation]. University of Cincinnati; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1445342666


University of Cincinnati

11. Mora Sánchez, Pablo A. Investigation of the Noise Radiation from Heated Supersonic Jets.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 This work focuses in the investigation of crackle and Mach wave radiation in heated supersonic jets. The skewness and kurtosis of the acoustic pressure signal… (more)

Subjects/Keywords: Aerospace Materials; Supersonic Jet Noise; Crackle; Mach Wave Radiation; Supersonic Heated Jets

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APA (6th Edition):

Mora Sánchez, P. A. (2016). Investigation of the Noise Radiation from Heated Supersonic Jets. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041

Chicago Manual of Style (16th Edition):

Mora Sánchez, Pablo A. “Investigation of the Noise Radiation from Heated Supersonic Jets.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041.

MLA Handbook (7th Edition):

Mora Sánchez, Pablo A. “Investigation of the Noise Radiation from Heated Supersonic Jets.” 2016. Web. 16 Sep 2019.

Vancouver:

Mora Sánchez PA. Investigation of the Noise Radiation from Heated Supersonic Jets. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041.

Council of Science Editors:

Mora Sánchez PA. Investigation of the Noise Radiation from Heated Supersonic Jets. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479818582442041


University of Cincinnati

12. Dolan, Brian. Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 The first major chapter of original research (Chapter 3) examines thermoacoustic oscillations in a low-emission staged multiple-nozzle lean direct injection (MLDI) combustor. This experimental program… (more)

Subjects/Keywords: Aerospace Materials; Gas Turbines; Combustors; Lean Direct Injection; Thermoacoustics; Nozzle Interaction; Alternating Flow Pattern

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APA (6th Edition):

Dolan, B. (2016). Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822588098224

Chicago Manual of Style (16th Edition):

Dolan, Brian. “Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822588098224.

MLA Handbook (7th Edition):

Dolan, Brian. “Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors.” 2016. Web. 16 Sep 2019.

Vancouver:

Dolan B. Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822588098224.

Council of Science Editors:

Dolan B. Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822588098224


University of Cincinnati

13. Shekhar, Anjali. Study and Numerical Simulation of Unconventional Engine Technology.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 The aim of this thesis is to understand the working of two unconventional aircraft propulsionsystems and to setup a two-dimensional transient simulation to analyze its… (more)

Subjects/Keywords: Aerospace Materials; Aircraft Propulsion; Computational Fluid Dynamics; Pressure Gain Combustion; Pulsejets; Transient Simulation

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APA (6th Edition):

Shekhar, A. (2018). Study and Numerical Simulation of Unconventional Engine Technology. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961

Chicago Manual of Style (16th Edition):

Shekhar, Anjali. “Study and Numerical Simulation of Unconventional Engine Technology.” 2018. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961.

MLA Handbook (7th Edition):

Shekhar, Anjali. “Study and Numerical Simulation of Unconventional Engine Technology.” 2018. Web. 16 Sep 2019.

Vancouver:

Shekhar A. Study and Numerical Simulation of Unconventional Engine Technology. [Internet] [Masters thesis]. University of Cincinnati; 2018. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961.

Council of Science Editors:

Shekhar A. Study and Numerical Simulation of Unconventional Engine Technology. [Masters Thesis]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1544098607675961


University of Cincinnati

14. Perelstein, Yuri. Investigation of Erosive Flow Injected Through Apertures into a Narrow Annulus.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 It is common to convey solid particulates using liquids, forming a slurry. Those slurries conveyed in conduits generate erosion caused by particulate impingements on the… (more)

Subjects/Keywords: Aerospace Materials; Solid particle erosion; Slurry erosion; Vortex-induced wear; Flow through aperture; Impaction statistics; Particle Image Velocimetry

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APA (6th Edition):

Perelstein, Y. (2016). Investigation of Erosive Flow Injected Through Apertures into a Narrow Annulus. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1463073062

Chicago Manual of Style (16th Edition):

Perelstein, Yuri. “Investigation of Erosive Flow Injected Through Apertures into a Narrow Annulus.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1463073062.

MLA Handbook (7th Edition):

Perelstein, Yuri. “Investigation of Erosive Flow Injected Through Apertures into a Narrow Annulus.” 2016. Web. 16 Sep 2019.

Vancouver:

Perelstein Y. Investigation of Erosive Flow Injected Through Apertures into a Narrow Annulus. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1463073062.

Council of Science Editors:

Perelstein Y. Investigation of Erosive Flow Injected Through Apertures into a Narrow Annulus. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1463073062


University of Cincinnati

15. Stoddard, William A. Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 PDE's (Pulse Detonation Engines) and RDE's (Rotating Detonation Engines) utilize a shock coupled burning wave to combust fuel and oxidizer or air at a near… (more)

Subjects/Keywords: Aerospace Materials; Detonation; PDE; RDE; CFD; Experimental; Combustor

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APA (6th Edition):

Stoddard, W. A. (2018). Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073

Chicago Manual of Style (16th Edition):

Stoddard, William A. “Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors.” 2018. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073.

MLA Handbook (7th Edition):

Stoddard, William A. “Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors.” 2018. Web. 16 Sep 2019.

Vancouver:

Stoddard WA. Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors. [Internet] [Doctoral dissertation]. University of Cincinnati; 2018. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073.

Council of Science Editors:

Stoddard WA. Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors. [Doctoral Dissertation]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073

16. Giri, Ritangshu. Numerical Analysis of Non-Reacting Flow in a Multi-nozzle Swirl Stabilized Lean Direct Injection Combustor.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2015, University of Cincinnati

 A multipoint lean direct injection (MLDI) concept was introduced recently in non-premixed combustion to obtain both low NOx emissions and good combustion stability. In this… (more)

Subjects/Keywords: Aerospace Materials; MLDI; Swirl stabilized nozzles; LRZ; CRZ; CTRZ; SWJ

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APA (6th Edition):

Giri, R. (2015). Numerical Analysis of Non-Reacting Flow in a Multi-nozzle Swirl Stabilized Lean Direct Injection Combustor. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447690568

Chicago Manual of Style (16th Edition):

Giri, Ritangshu. “Numerical Analysis of Non-Reacting Flow in a Multi-nozzle Swirl Stabilized Lean Direct Injection Combustor.” 2015. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447690568.

MLA Handbook (7th Edition):

Giri, Ritangshu. “Numerical Analysis of Non-Reacting Flow in a Multi-nozzle Swirl Stabilized Lean Direct Injection Combustor.” 2015. Web. 16 Sep 2019.

Vancouver:

Giri R. Numerical Analysis of Non-Reacting Flow in a Multi-nozzle Swirl Stabilized Lean Direct Injection Combustor. [Internet] [Masters thesis]. University of Cincinnati; 2015. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447690568.

Council of Science Editors:

Giri R. Numerical Analysis of Non-Reacting Flow in a Multi-nozzle Swirl Stabilized Lean Direct Injection Combustor. [Masters Thesis]. University of Cincinnati; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1447690568

17. Rask, Olaf Haller. The Reduction of Mixing Noise and Shock Associated Noise using Chevrons and other Mixing Enhancement Devices.

Degree: PhD, Engineering : Aerospace Engineering, 2009, University of Cincinnati

  This experimental research project varied nozzle discharge geometries in an effort to reduce jet noise. Chevrons and other mixing enhancement devices introduced streamwise vortices… (more)

Subjects/Keywords: Acoustics; Engineering; jet noise; shock noise; shock associated noise; chevrons; fluidic injection; mixing noise; vortex generators

…acquired using the coaxial flow test facility at the University of Cincinnati. The basic… 

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APA (6th Edition):

Rask, O. H. (2009). The Reduction of Mixing Noise and Shock Associated Noise using Chevrons and other Mixing Enhancement Devices. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1223056142

Chicago Manual of Style (16th Edition):

Rask, Olaf Haller. “The Reduction of Mixing Noise and Shock Associated Noise using Chevrons and other Mixing Enhancement Devices.” 2009. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1223056142.

MLA Handbook (7th Edition):

Rask, Olaf Haller. “The Reduction of Mixing Noise and Shock Associated Noise using Chevrons and other Mixing Enhancement Devices.” 2009. Web. 16 Sep 2019.

Vancouver:

Rask OH. The Reduction of Mixing Noise and Shock Associated Noise using Chevrons and other Mixing Enhancement Devices. [Internet] [Doctoral dissertation]. University of Cincinnati; 2009. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1223056142.

Council of Science Editors:

Rask OH. The Reduction of Mixing Noise and Shock Associated Noise using Chevrons and other Mixing Enhancement Devices. [Doctoral Dissertation]. University of Cincinnati; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1223056142

18. Guillou, Erwann. Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2011, University of Cincinnati

  Due to recent emission regulations, the use of turbochargers for force induction of internal combustion engines has increased. Actually, the trend in diesel engines… (more)

Subjects/Keywords: Aerospace Materials; Radial Compressor; Surge; Passive Control; Ported Shroud; Particle Image Velocimetry; PIV

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APA (6th Edition):

Guillou, E. (2011). Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1321371782

Chicago Manual of Style (16th Edition):

Guillou, Erwann. “Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control.” 2011. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1321371782.

MLA Handbook (7th Edition):

Guillou, Erwann. “Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control.” 2011. Web. 16 Sep 2019.

Vancouver:

Guillou E. Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control. [Internet] [Doctoral dissertation]. University of Cincinnati; 2011. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1321371782.

Council of Science Editors:

Guillou E. Flow Characterization and Dynamic Analysis of a Radial Compressor with Passive Method of Surge Control. [Doctoral Dissertation]. University of Cincinnati; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1321371782

19. Pappu, Suryanarayana. A Parametric Study to Quantify the Pressure Drop of Pulsating Flow through Blockages.

Degree: MS, Engineering and Applied Science: Mechanical Engineering, 2014, University of Cincinnati

 The current set up is an improvement of a previous set up designed and fabricated to study pulsating flow through blockages[1]. The ultimate objective of… (more)

Subjects/Keywords: Engineering; Coronary Artery Disease; Pressure Drop; Pulsating Flow; Fast Fourier Transform; Blockage; Experimental

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APA (6th Edition):

Pappu, S. (2014). A Parametric Study to Quantify the Pressure Drop of Pulsating Flow through Blockages. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881302

Chicago Manual of Style (16th Edition):

Pappu, Suryanarayana. “A Parametric Study to Quantify the Pressure Drop of Pulsating Flow through Blockages.” 2014. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881302.

MLA Handbook (7th Edition):

Pappu, Suryanarayana. “A Parametric Study to Quantify the Pressure Drop of Pulsating Flow through Blockages.” 2014. Web. 16 Sep 2019.

Vancouver:

Pappu S. A Parametric Study to Quantify the Pressure Drop of Pulsating Flow through Blockages. [Internet] [Masters thesis]. University of Cincinnati; 2014. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881302.

Council of Science Editors:

Pappu S. A Parametric Study to Quantify the Pressure Drop of Pulsating Flow through Blockages. [Masters Thesis]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881302

20. Mylavarapu, Goutham. Computational Flow Modeling of Human Upper Airway Breathing.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 Computational modeling of biological systems have gained a lot of interest in biomedical research, in the recent past. This thesis focuses on the application of… (more)

Subjects/Keywords: Aerospace Materials; Bio Fluid Mechanics; CFD Applications; Upper Airway; Sleep Apnea; Virtual Surgery; FSI

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APA (6th Edition):

Mylavarapu, G. (2013). Computational Flow Modeling of Human Upper Airway Breathing. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377871159

Chicago Manual of Style (16th Edition):

Mylavarapu, Goutham. “Computational Flow Modeling of Human Upper Airway Breathing.” 2013. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377871159.

MLA Handbook (7th Edition):

Mylavarapu, Goutham. “Computational Flow Modeling of Human Upper Airway Breathing.” 2013. Web. 16 Sep 2019.

Vancouver:

Mylavarapu G. Computational Flow Modeling of Human Upper Airway Breathing. [Internet] [Doctoral dissertation]. University of Cincinnati; 2013. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377871159.

Council of Science Editors:

Mylavarapu G. Computational Flow Modeling of Human Upper Airway Breathing. [Doctoral Dissertation]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1377871159

21. Munday, David. Flow and Acoustics of Jets from Practical Nozzles for High-Performance Military Aircraft.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2010, University of Cincinnati

  This research project examines supersonic jets from nozzles representative of the practical variable-geometry convergent-divergent nozzles used on high-performance military aircraft. The nozzles employed have… (more)

Subjects/Keywords: Aerospace Materials; jet noise; chevrons; microjets; fluidics; Prantdl-Pack; supersonic jets

…Shaaban Abdallah and Paul Orkwis of the University of Cincinnati; James Bridges of the NASA… …SERDP sponsored two concurrent projects; one with University of Cincinnati and one with Penn… …avoid duplication of effort imposed on University of Cincinnati an explicit de-emphasis on far… 

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APA (6th Edition):

Munday, D. (2010). Flow and Acoustics of Jets from Practical Nozzles for High-Performance Military Aircraft. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1289842789

Chicago Manual of Style (16th Edition):

Munday, David. “Flow and Acoustics of Jets from Practical Nozzles for High-Performance Military Aircraft.” 2010. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1289842789.

MLA Handbook (7th Edition):

Munday, David. “Flow and Acoustics of Jets from Practical Nozzles for High-Performance Military Aircraft.” 2010. Web. 16 Sep 2019.

Vancouver:

Munday D. Flow and Acoustics of Jets from Practical Nozzles for High-Performance Military Aircraft. [Internet] [Doctoral dissertation]. University of Cincinnati; 2010. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1289842789.

Council of Science Editors:

Munday D. Flow and Acoustics of Jets from Practical Nozzles for High-Performance Military Aircraft. [Doctoral Dissertation]. University of Cincinnati; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1289842789

22. Guillou, Erwann. Flame Characteristics and Application of Flameless Combustion.

Degree: MS, Engineering : Aerospace Engineering, 2008, University of Cincinnati

 Flameless combustion is a technique obtained by operating at high level of turbulence and temperature of oxidizer higher than the autoignition temperature of the air… (more)

Subjects/Keywords: Engineering; Aerospace

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APA (6th Edition):

Guillou, E. (2008). Flame Characteristics and Application of Flameless Combustion. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205191185

Chicago Manual of Style (16th Edition):

Guillou, Erwann. “Flame Characteristics and Application of Flameless Combustion.” 2008. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205191185.

MLA Handbook (7th Edition):

Guillou, Erwann. “Flame Characteristics and Application of Flameless Combustion.” 2008. Web. 16 Sep 2019.

Vancouver:

Guillou E. Flame Characteristics and Application of Flameless Combustion. [Internet] [Masters thesis]. University of Cincinnati; 2008. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205191185.

Council of Science Editors:

Guillou E. Flame Characteristics and Application of Flameless Combustion. [Masters Thesis]. University of Cincinnati; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205191185

23. Oren, Liran. Fluid dynamics of pulsating jets and voice.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2012, University of Cincinnati

Vortical structure plays a significant role in flow mechanisms that impact our everyday life. Advisors/Committee Members: Gutmark, Ephraim (Committee Chair).

Subjects/Keywords: Aerospace Materials; fluid dynamics; synthetic jet; voice

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APA (6th Edition):

Oren, L. (2012). Fluid dynamics of pulsating jets and voice. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1353155395

Chicago Manual of Style (16th Edition):

Oren, Liran. “Fluid dynamics of pulsating jets and voice.” 2012. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1353155395.

MLA Handbook (7th Edition):

Oren, Liran. “Fluid dynamics of pulsating jets and voice.” 2012. Web. 16 Sep 2019.

Vancouver:

Oren L. Fluid dynamics of pulsating jets and voice. [Internet] [Doctoral dissertation]. University of Cincinnati; 2012. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1353155395.

Council of Science Editors:

Oren L. Fluid dynamics of pulsating jets and voice. [Doctoral Dissertation]. University of Cincinnati; 2012. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1353155395

24. Driscoll, Robert B. EXPERIMENTAL INVESTIGATION OF SHOCK TRANSFER AND SHOCK INITIATED DETONATION IN A DUAL PULSE DETONATION ENGINE CROSSOVER SYSTEM.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2013, University of Cincinnati

 An experimental investigation was carried out to study the travel of a shockwave through a crossover tube and analyze the ability to cause shock initiated… (more)

Subjects/Keywords: Aerospace Materials; Pulse Detonation Engine; Detonation; Crossover

…29 CHAPTER 2: UNIVERSITY OF CINCINNATI PULSE DETONATION FACILITY ............ 32 2.1… 

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APA (6th Edition):

Driscoll, R. B. (2013). EXPERIMENTAL INVESTIGATION OF SHOCK TRANSFER AND SHOCK INITIATED DETONATION IN A DUAL PULSE DETONATION ENGINE CROSSOVER SYSTEM. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378113995

Chicago Manual of Style (16th Edition):

Driscoll, Robert B. “EXPERIMENTAL INVESTIGATION OF SHOCK TRANSFER AND SHOCK INITIATED DETONATION IN A DUAL PULSE DETONATION ENGINE CROSSOVER SYSTEM.” 2013. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378113995.

MLA Handbook (7th Edition):

Driscoll, Robert B. “EXPERIMENTAL INVESTIGATION OF SHOCK TRANSFER AND SHOCK INITIATED DETONATION IN A DUAL PULSE DETONATION ENGINE CROSSOVER SYSTEM.” 2013. Web. 16 Sep 2019.

Vancouver:

Driscoll RB. EXPERIMENTAL INVESTIGATION OF SHOCK TRANSFER AND SHOCK INITIATED DETONATION IN A DUAL PULSE DETONATION ENGINE CROSSOVER SYSTEM. [Internet] [Masters thesis]. University of Cincinnati; 2013. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378113995.

Council of Science Editors:

Driscoll RB. EXPERIMENTAL INVESTIGATION OF SHOCK TRANSFER AND SHOCK INITIATED DETONATION IN A DUAL PULSE DETONATION ENGINE CROSSOVER SYSTEM. [Masters Thesis]. University of Cincinnati; 2013. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1378113995

25. Nieberding, Zachary J. An Investigation of Acoustic Wave Propagation in Mach 2 Flow.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2014, University of Cincinnati

 Hypersonic technology is the next advancement to enter the aerospace community; it is defined as the study of flight at speeds Mach 5 and higher… (more)

Subjects/Keywords: Aerospace Materials; hypersonics; supersonic; scramjet; experimental; signal propagation; inlet unstart

…Tucker-Davis Technologies TS# Test Series # UC University of Cincinnati ue Time averaged… …pressure. In the experiment, H-S tubes from both AFRL and the University of Cincinnati (UC… 

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APA (6th Edition):

Nieberding, Z. J. (2014). An Investigation of Acoustic Wave Propagation in Mach 2 Flow. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881591

Chicago Manual of Style (16th Edition):

Nieberding, Zachary J. “An Investigation of Acoustic Wave Propagation in Mach 2 Flow.” 2014. Masters Thesis, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881591.

MLA Handbook (7th Edition):

Nieberding, Zachary J. “An Investigation of Acoustic Wave Propagation in Mach 2 Flow.” 2014. Web. 16 Sep 2019.

Vancouver:

Nieberding ZJ. An Investigation of Acoustic Wave Propagation in Mach 2 Flow. [Internet] [Masters thesis]. University of Cincinnati; 2014. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881591.

Council of Science Editors:

Nieberding ZJ. An Investigation of Acoustic Wave Propagation in Mach 2 Flow. [Masters Thesis]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406881591

26. St. George, Andrew. Development and Testing of Pulsed and Rotating Detonation Combustors.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 Detonation is a self-sustaining, supersonic, shock-driven, exothermic reaction. Detonation combustion can theoretically provide significant improvements in thermodynamic efficiency over constant pressure combustion when incorporated into… (more)

Subjects/Keywords: Aerospace Materials; detonation; rotating detonation combustor; pulse detonation combustor; turbine; initiation; cell width

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APA (6th Edition):

St. George, A. (2016). Development and Testing of Pulsed and Rotating Detonation Combustors. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893231

Chicago Manual of Style (16th Edition):

St. George, Andrew. “Development and Testing of Pulsed and Rotating Detonation Combustors.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893231.

MLA Handbook (7th Edition):

St. George, Andrew. “Development and Testing of Pulsed and Rotating Detonation Combustors.” 2016. Web. 16 Sep 2019.

Vancouver:

St. George A. Development and Testing of Pulsed and Rotating Detonation Combustors. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893231.

Council of Science Editors:

St. George A. Development and Testing of Pulsed and Rotating Detonation Combustors. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1458893231

27. Cornwell, Michael. Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2011, University of Cincinnati

 Combustion at high pressure in applications such as rocket engines and gas turbine engines commonly experience destructive combustion instabilities. These instabilities results from interactions between… (more)

Subjects/Keywords: Aerospace Materials; Combustion Instability; Thermoacoustic Instability; Active Combustion Control; Flameless Combustion; Swirl Stabilized Combustion; Vortex Breakdown

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APA (6th Edition):

Cornwell, M. (2011). Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323433

Chicago Manual of Style (16th Edition):

Cornwell, Michael. “Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines.” 2011. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323433.

MLA Handbook (7th Edition):

Cornwell, Michael. “Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines.” 2011. Web. 16 Sep 2019.

Vancouver:

Cornwell M. Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines. [Internet] [Doctoral dissertation]. University of Cincinnati; 2011. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323433.

Council of Science Editors:

Cornwell M. Causes of Combustion Instabilities with Passive and Active Methods of Control for practical application to Gas Turbine Engines. [Doctoral Dissertation]. University of Cincinnati; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1307323433

28. Lakhamraju, Raghava Raju. Characterization of the jet emanating from a self-exciting flexible membrane nozzle.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2012, University of Cincinnati

 The present research investigates the development and characterization ofa novel self-exciting flexible membrane nozzle. Upon excitation (oscillations that areproduced by exerting tension at the nozzle… (more)

Subjects/Keywords: Aerospace Materials; flow control; flexible nozzle; self-excitation; pulsatile jet; noncircular jet; starting and entrainment vortices

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APA (6th Edition):

Lakhamraju, R. R. (2012). Characterization of the jet emanating from a self-exciting flexible membrane nozzle. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1337887322

Chicago Manual of Style (16th Edition):

Lakhamraju, Raghava Raju. “Characterization of the jet emanating from a self-exciting flexible membrane nozzle.” 2012. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1337887322.

MLA Handbook (7th Edition):

Lakhamraju, Raghava Raju. “Characterization of the jet emanating from a self-exciting flexible membrane nozzle.” 2012. Web. 16 Sep 2019.

Vancouver:

Lakhamraju RR. Characterization of the jet emanating from a self-exciting flexible membrane nozzle. [Internet] [Doctoral dissertation]. University of Cincinnati; 2012. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1337887322.

Council of Science Editors:

Lakhamraju RR. Characterization of the jet emanating from a self-exciting flexible membrane nozzle. [Doctoral Dissertation]. University of Cincinnati; 2012. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1337887322

29. Perrino, Michael. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2014, University of Cincinnati

 A pylon bottom bifurcation and a wing with variable flaps were designed and builtto attach to a scaled model of a coaxial exhaust nozzle system.… (more)

Subjects/Keywords: Aerospace Materials; Aeroacoustics; Aircraft Engine; Pylon; Noise; Nozzle

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APA (6th Edition):

Perrino, M. (2014). An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764

Chicago Manual of Style (16th Edition):

Perrino, Michael. “An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft.” 2014. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764.

MLA Handbook (7th Edition):

Perrino, Michael. “An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft.” 2014. Web. 16 Sep 2019.

Vancouver:

Perrino M. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. [Internet] [Doctoral dissertation]. University of Cincinnati; 2014. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764.

Council of Science Editors:

Perrino M. An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft. [Doctoral Dissertation]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1406819764

30. Gancedo, Matthieu. Effect of Self Recirculation Casing Treatment on the Performance of a TurbochargerCentrifugal Compressor.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2015, University of Cincinnati

 Increase in emission regulations in the transport industry brings the need to have more efficient engines. A path followed by the automobile industry is to… (more)

Subjects/Keywords: Aerospace Materials; Turbocharger; Surge; Centrifugal compressor; PIV; Pressure measurements; Experimental

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APA (6th Edition):

Gancedo, M. (2015). Effect of Self Recirculation Casing Treatment on the Performance of a TurbochargerCentrifugal Compressor. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439305804

Chicago Manual of Style (16th Edition):

Gancedo, Matthieu. “Effect of Self Recirculation Casing Treatment on the Performance of a TurbochargerCentrifugal Compressor.” 2015. Doctoral Dissertation, University of Cincinnati. Accessed September 16, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439305804.

MLA Handbook (7th Edition):

Gancedo, Matthieu. “Effect of Self Recirculation Casing Treatment on the Performance of a TurbochargerCentrifugal Compressor.” 2015. Web. 16 Sep 2019.

Vancouver:

Gancedo M. Effect of Self Recirculation Casing Treatment on the Performance of a TurbochargerCentrifugal Compressor. [Internet] [Doctoral dissertation]. University of Cincinnati; 2015. [cited 2019 Sep 16]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439305804.

Council of Science Editors:

Gancedo M. Effect of Self Recirculation Casing Treatment on the Performance of a TurbochargerCentrifugal Compressor. [Doctoral Dissertation]. University of Cincinnati; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1439305804

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