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You searched for subject:(aeroacoustics). Showing records 1 – 30 of 242 total matches.

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University of Adelaide

1. Porteous, Ric. The aeroacoustics of finite wall-mounted cylinders.

Degree: 2016, University of Adelaide

 Community noise is one of the most poorly controlled environmental pollutants. Controlling the noise generated by bluff-body flow can alleviate community noise generated by transportation… (more)

Subjects/Keywords: aeroacoustics; finite; cylinders

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APA (6th Edition):

Porteous, R. (2016). The aeroacoustics of finite wall-mounted cylinders. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/102379

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Porteous, Ric. “The aeroacoustics of finite wall-mounted cylinders.” 2016. Thesis, University of Adelaide. Accessed July 07, 2020. http://hdl.handle.net/2440/102379.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Porteous, Ric. “The aeroacoustics of finite wall-mounted cylinders.” 2016. Web. 07 Jul 2020.

Vancouver:

Porteous R. The aeroacoustics of finite wall-mounted cylinders. [Internet] [Thesis]. University of Adelaide; 2016. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/2440/102379.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Porteous R. The aeroacoustics of finite wall-mounted cylinders. [Thesis]. University of Adelaide; 2016. Available from: http://hdl.handle.net/2440/102379

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Cambridge

2. Ayton, Lorna Jane. Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows.

Degree: PhD, 2014, University of Cambridge

 This thesis considers the sound generated by unsteady perturbations interacting with solid aerofoils in background steady flows, in an attempt to further develop analytic models… (more)

Subjects/Keywords: Aeroacoustics; Fluid mechanics

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APA (6th Edition):

Ayton, L. J. (2014). Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/246549https://www.repository.cam.ac.uk/bitstream/1810/246549/4/ThesisC3.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/246549/5/ThesisC3.pdf.jpg

Chicago Manual of Style (16th Edition):

Ayton, Lorna Jane. “Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows.” 2014. Doctoral Dissertation, University of Cambridge. Accessed July 07, 2020. https://www.repository.cam.ac.uk/handle/1810/246549https://www.repository.cam.ac.uk/bitstream/1810/246549/4/ThesisC3.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/246549/5/ThesisC3.pdf.jpg.

MLA Handbook (7th Edition):

Ayton, Lorna Jane. “Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows.” 2014. Web. 07 Jul 2020.

Vancouver:

Ayton LJ. Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows. [Internet] [Doctoral dissertation]. University of Cambridge; 2014. [cited 2020 Jul 07]. Available from: https://www.repository.cam.ac.uk/handle/1810/246549https://www.repository.cam.ac.uk/bitstream/1810/246549/4/ThesisC3.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/246549/5/ThesisC3.pdf.jpg.

Council of Science Editors:

Ayton LJ. Asymptotic approximations for the sound generated by aerofoils in unsteady subsonic flows. [Doctoral Dissertation]. University of Cambridge; 2014. Available from: https://www.repository.cam.ac.uk/handle/1810/246549https://www.repository.cam.ac.uk/bitstream/1810/246549/4/ThesisC3.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/246549/5/ThesisC3.pdf.jpg


McMaster University

3. Finnerty, Donal. Self-excited oscillations of the impinging multi-slot planar jet.

Degree: 2019, McMaster University

Impinging high-speed planar jets are susceptible to self-excited aeroacoustic feedback mechanisms due to the coupling of the highly unstable shear layer and upstream travelling pressure… (more)

Subjects/Keywords: Aeroacoustics; Jets; Galvanizing

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APA (6th Edition):

Finnerty, D. (2019). Self-excited oscillations of the impinging multi-slot planar jet. (Thesis). McMaster University. Retrieved from http://hdl.handle.net/11375/25107

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Finnerty, Donal. “Self-excited oscillations of the impinging multi-slot planar jet.” 2019. Thesis, McMaster University. Accessed July 07, 2020. http://hdl.handle.net/11375/25107.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Finnerty, Donal. “Self-excited oscillations of the impinging multi-slot planar jet.” 2019. Web. 07 Jul 2020.

Vancouver:

Finnerty D. Self-excited oscillations of the impinging multi-slot planar jet. [Internet] [Thesis]. McMaster University; 2019. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/11375/25107.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Finnerty D. Self-excited oscillations of the impinging multi-slot planar jet. [Thesis]. McMaster University; 2019. Available from: http://hdl.handle.net/11375/25107

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Illinois – Urbana-Champaign

4. Buchta, David A. Crackle noise from high-speed free-shear-flow turbulence.

Degree: PhD, Theoretical & Applied Mechans, 2016, University of Illinois – Urbana-Champaign

 The sound from high-speed jets, such as on military aircraft, is distinctly different than that from lower-speed jets, such as on commercial airliners. Atop the… (more)

Subjects/Keywords: aeroacoustics; turbulence simulation

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APA (6th Edition):

Buchta, D. A. (2016). Crackle noise from high-speed free-shear-flow turbulence. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/95256

Chicago Manual of Style (16th Edition):

Buchta, David A. “Crackle noise from high-speed free-shear-flow turbulence.” 2016. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed July 07, 2020. http://hdl.handle.net/2142/95256.

MLA Handbook (7th Edition):

Buchta, David A. “Crackle noise from high-speed free-shear-flow turbulence.” 2016. Web. 07 Jul 2020.

Vancouver:

Buchta DA. Crackle noise from high-speed free-shear-flow turbulence. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2016. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/2142/95256.

Council of Science Editors:

Buchta DA. Crackle noise from high-speed free-shear-flow turbulence. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2016. Available from: http://hdl.handle.net/2142/95256


Virginia Tech

5. Daniel, Kyle Andreas. Space-time Description of Supersonic Jets with Thermal Non-uniformity.

Degree: PhD, Aerospace Engineering, 2019, Virginia Tech

 A more complete understanding of the intense noise sources present in supersonic jet plumes is of value to both government and industry, and is a… (more)

Subjects/Keywords: Jet Noise; Aeroacoustics; Fluid Dynamics

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APA (6th Edition):

Daniel, K. A. (2019). Space-time Description of Supersonic Jets with Thermal Non-uniformity. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/95942

Chicago Manual of Style (16th Edition):

Daniel, Kyle Andreas. “Space-time Description of Supersonic Jets with Thermal Non-uniformity.” 2019. Doctoral Dissertation, Virginia Tech. Accessed July 07, 2020. http://hdl.handle.net/10919/95942.

MLA Handbook (7th Edition):

Daniel, Kyle Andreas. “Space-time Description of Supersonic Jets with Thermal Non-uniformity.” 2019. Web. 07 Jul 2020.

Vancouver:

Daniel KA. Space-time Description of Supersonic Jets with Thermal Non-uniformity. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/10919/95942.

Council of Science Editors:

Daniel KA. Space-time Description of Supersonic Jets with Thermal Non-uniformity. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/95942

6. Baddoo, Peter Jonathan. Analytic Solutions for Flows Through Cascades.

Degree: PhD, 2020, University of Cambridge

 Noise reduction is a principal aim of the aviation industry. Particular attention is devoted to reducing turbomachinery noise, which is an important component of overall… (more)

Subjects/Keywords: fluid dynamics; complex variables; aeroacoustics

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

APA (6th Edition):

Baddoo, P. J. (2020). Analytic Solutions for Flows Through Cascades. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/299624

Chicago Manual of Style (16th Edition):

Baddoo, Peter Jonathan. “Analytic Solutions for Flows Through Cascades.” 2020. Doctoral Dissertation, University of Cambridge. Accessed July 07, 2020. https://www.repository.cam.ac.uk/handle/1810/299624.

MLA Handbook (7th Edition):

Baddoo, Peter Jonathan. “Analytic Solutions for Flows Through Cascades.” 2020. Web. 07 Jul 2020.

Vancouver:

Baddoo PJ. Analytic Solutions for Flows Through Cascades. [Internet] [Doctoral dissertation]. University of Cambridge; 2020. [cited 2020 Jul 07]. Available from: https://www.repository.cam.ac.uk/handle/1810/299624.

Council of Science Editors:

Baddoo PJ. Analytic Solutions for Flows Through Cascades. [Doctoral Dissertation]. University of Cambridge; 2020. Available from: https://www.repository.cam.ac.uk/handle/1810/299624


University of Notre Dame

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

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

  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 (6th Edition):

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

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Tufts, Anne L. “Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>.” 2018. Thesis, University of Notre Dame. Accessed July 07, 2020. https://curate.nd.edu/show/d217qn62j1g.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Tufts, Anne L. “Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>.” 2018. Web. 07 Jul 2020.

Vancouver:

Tufts AL. Numerical Investigation of Sound Generation by Airfoil Interaction with a Turbulent Shear Layer</h1>. [Internet] [Thesis]. University of Notre Dame; 2018. [cited 2020 Jul 07]. Available from: https://curate.nd.edu/show/d217qn62j1g.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

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

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Delft University of Technology

8. Tamaro, Simone (author). Numerical and Experimental Study of Airfoils with Porous Trailing Edge.

Degree: 2019, Delft University of Technology

The addition of porous material to the trailing edge of airfoils was studied numerically and experimentally. The purpose of this work is to inspect whether… (more)

Subjects/Keywords: Porous Media; Aeroacoustics; CFD

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APA (6th Edition):

Tamaro, S. (. (2019). Numerical and Experimental Study of Airfoils with Porous Trailing Edge. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:21c1e156-c8df-4ab6-8630-25c6170d3bc6

Chicago Manual of Style (16th Edition):

Tamaro, Simone (author). “Numerical and Experimental Study of Airfoils with Porous Trailing Edge.” 2019. Masters Thesis, Delft University of Technology. Accessed July 07, 2020. http://resolver.tudelft.nl/uuid:21c1e156-c8df-4ab6-8630-25c6170d3bc6.

MLA Handbook (7th Edition):

Tamaro, Simone (author). “Numerical and Experimental Study of Airfoils with Porous Trailing Edge.” 2019. Web. 07 Jul 2020.

Vancouver:

Tamaro S(. Numerical and Experimental Study of Airfoils with Porous Trailing Edge. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Jul 07]. Available from: http://resolver.tudelft.nl/uuid:21c1e156-c8df-4ab6-8630-25c6170d3bc6.

Council of Science Editors:

Tamaro S(. Numerical and Experimental Study of Airfoils with Porous Trailing Edge. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:21c1e156-c8df-4ab6-8630-25c6170d3bc6


University of Florida

9. Nickels, Adam S. Experimental-Based Velocity, Hydrodynamic Pressure, and Acoustic Estimation in a Three-Dimensional Turbulent Wall Jet.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2018, University of Florida

 The nature of turbulence generated acoustics has been researched for much of the last century due to its prevalence in practical flow scenarios. The derivation… (more)

Subjects/Keywords: acoustics  – aeroacoustics  – estimation  – pod  – turbulence

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APA (6th Edition):

Nickels, A. S. (2018). Experimental-Based Velocity, Hydrodynamic Pressure, and Acoustic Estimation in a Three-Dimensional Turbulent Wall Jet. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0051784

Chicago Manual of Style (16th Edition):

Nickels, Adam S. “Experimental-Based Velocity, Hydrodynamic Pressure, and Acoustic Estimation in a Three-Dimensional Turbulent Wall Jet.” 2018. Doctoral Dissertation, University of Florida. Accessed July 07, 2020. https://ufdc.ufl.edu/UFE0051784.

MLA Handbook (7th Edition):

Nickels, Adam S. “Experimental-Based Velocity, Hydrodynamic Pressure, and Acoustic Estimation in a Three-Dimensional Turbulent Wall Jet.” 2018. Web. 07 Jul 2020.

Vancouver:

Nickels AS. Experimental-Based Velocity, Hydrodynamic Pressure, and Acoustic Estimation in a Three-Dimensional Turbulent Wall Jet. [Internet] [Doctoral dissertation]. University of Florida; 2018. [cited 2020 Jul 07]. Available from: https://ufdc.ufl.edu/UFE0051784.

Council of Science Editors:

Nickels AS. Experimental-Based Velocity, Hydrodynamic Pressure, and Acoustic Estimation in a Three-Dimensional Turbulent Wall Jet. [Doctoral Dissertation]. University of Florida; 2018. Available from: https://ufdc.ufl.edu/UFE0051784


University of Cambridge

10. Baddoo, Peter Jonathan. Analytic solutions for flows through cascades.

Degree: PhD, 2020, University of Cambridge

 Noise reduction is a principal aim of the aviation industry. Particular attention is devoted to reducing turbomachinery noise, which is an important component of overall… (more)

Subjects/Keywords: fluid dynamics; complex variables; aeroacoustics

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

APA (6th Edition):

Baddoo, P. J. (2020). Analytic solutions for flows through cascades. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/299624 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793102

Chicago Manual of Style (16th Edition):

Baddoo, Peter Jonathan. “Analytic solutions for flows through cascades.” 2020. Doctoral Dissertation, University of Cambridge. Accessed July 07, 2020. https://www.repository.cam.ac.uk/handle/1810/299624 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793102.

MLA Handbook (7th Edition):

Baddoo, Peter Jonathan. “Analytic solutions for flows through cascades.” 2020. Web. 07 Jul 2020.

Vancouver:

Baddoo PJ. Analytic solutions for flows through cascades. [Internet] [Doctoral dissertation]. University of Cambridge; 2020. [cited 2020 Jul 07]. Available from: https://www.repository.cam.ac.uk/handle/1810/299624 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793102.

Council of Science Editors:

Baddoo PJ. Analytic solutions for flows through cascades. [Doctoral Dissertation]. University of Cambridge; 2020. Available from: https://www.repository.cam.ac.uk/handle/1810/299624 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.793102


Penn State University

11. Villafana, Willca. Rotorcraft Noise Abatement Procedures Development.

Degree: MS, Aerospace Engineering, 2016, Penn State University

 A rotorcraft noise prediction system has recently been developed as part of a project to develop and evaluate helicopter noise abatement procedures for a range… (more)

Subjects/Keywords: aeroacoustics; helicopter; rotor noise; simulation; modeling

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APA (6th Edition):

Villafana, W. (2016). Rotorcraft Noise Abatement Procedures Development. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13106wrv105

Chicago Manual of Style (16th Edition):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Masters Thesis, Penn State University. Accessed July 07, 2020. https://etda.libraries.psu.edu/catalog/13106wrv105.

MLA Handbook (7th Edition):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Web. 07 Jul 2020.

Vancouver:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2020 Jul 07]. Available from: https://etda.libraries.psu.edu/catalog/13106wrv105.

Council of Science Editors:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Masters Thesis]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/13106wrv105


Penn State University

12. Powers, Russell. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.

Degree: PhD, Aerospace Engineering, 2015, Penn State University

 The noise produced by the supersonic, high temperature jets that exhaust from military aircraft is becoming a hazard to naval personnel and a disturbance to… (more)

Subjects/Keywords: Jet Noise; Supersonic; Aeroacoustics; Noise Reduction

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APA (6th Edition):

Powers, R. (2015). Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26397

Chicago Manual of Style (16th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Doctoral Dissertation, Penn State University. Accessed July 07, 2020. https://etda.libraries.psu.edu/catalog/26397.

MLA Handbook (7th Edition):

Powers, Russell. “Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts.” 2015. Web. 07 Jul 2020.

Vancouver:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Internet] [Doctoral dissertation]. Penn State University; 2015. [cited 2020 Jul 07]. Available from: https://etda.libraries.psu.edu/catalog/26397.

Council of Science Editors:

Powers R. Experimental Investigation of the Noise Reduction of Supersonic Exhaust Jets with Fluidic Inserts. [Doctoral Dissertation]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/26397


University of Cambridge

13. Wilsby, Oscar. Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number.

Degree: PhD, 2019, University of Cambridge

 This thesis is an investigation into the production and prediction of broadband noise in axial compressors operating at low Reynolds number. The low Reynolds number… (more)

Subjects/Keywords: Large eddy simulation; low reynolds number; aeroacoustics

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APA (6th Edition):

Wilsby, O. (2019). Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/294622

Chicago Manual of Style (16th Edition):

Wilsby, Oscar. “Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number.” 2019. Doctoral Dissertation, University of Cambridge. Accessed July 07, 2020. https://www.repository.cam.ac.uk/handle/1810/294622.

MLA Handbook (7th Edition):

Wilsby, Oscar. “Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number.” 2019. Web. 07 Jul 2020.

Vancouver:

Wilsby O. Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2020 Jul 07]. Available from: https://www.repository.cam.ac.uk/handle/1810/294622.

Council of Science Editors:

Wilsby O. Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/294622


University of Cambridge

14. Pearson, Charlie. Vertical axis wind turbine acoustics.

Degree: PhD, 2014, University of Cambridge

 Increasing awareness of the issues of climate change and sustainable energy use has led to growing levels of interest in small-scale, decentralised power generation. Small-scale… (more)

Subjects/Keywords: Aeroacoustics; VAWT; Noise; Wind turbines; Acoustic array

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APA (6th Edition):

Pearson, C. (2014). Vertical axis wind turbine acoustics. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/245256https://www.repository.cam.ac.uk/bitstream/1810/245256/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/3/license_rdf ; https://www.repository.cam.ac.uk/bitstream/1810/245256/4/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/5/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.jpg

Chicago Manual of Style (16th Edition):

Pearson, Charlie. “Vertical axis wind turbine acoustics.” 2014. Doctoral Dissertation, University of Cambridge. Accessed July 07, 2020. https://www.repository.cam.ac.uk/handle/1810/245256https://www.repository.cam.ac.uk/bitstream/1810/245256/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/3/license_rdf ; https://www.repository.cam.ac.uk/bitstream/1810/245256/4/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/5/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.jpg.

MLA Handbook (7th Edition):

Pearson, Charlie. “Vertical axis wind turbine acoustics.” 2014. Web. 07 Jul 2020.

Vancouver:

Pearson C. Vertical axis wind turbine acoustics. [Internet] [Doctoral dissertation]. University of Cambridge; 2014. [cited 2020 Jul 07]. Available from: https://www.repository.cam.ac.uk/handle/1810/245256https://www.repository.cam.ac.uk/bitstream/1810/245256/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/3/license_rdf ; https://www.repository.cam.ac.uk/bitstream/1810/245256/4/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/5/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.jpg.

Council of Science Editors:

Pearson C. Vertical axis wind turbine acoustics. [Doctoral Dissertation]. University of Cambridge; 2014. Available from: https://www.repository.cam.ac.uk/handle/1810/245256https://www.repository.cam.ac.uk/bitstream/1810/245256/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/3/license_rdf ; https://www.repository.cam.ac.uk/bitstream/1810/245256/4/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/245256/5/Thesis%20-%20VAWT%20Noise%20-%20Charlie%20Pearson.pdf.jpg


University of Toronto

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

Degree: 2014, University of Toronto

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

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

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Chekiri, Rafik. “Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller.” 2014. Masters Thesis, University of Toronto. Accessed July 07, 2020. http://hdl.handle.net/1807/67867.

MLA Handbook (7th Edition):

Chekiri, Rafik. “Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller.” 2014. Web. 07 Jul 2020.

Vancouver:

Chekiri R. Experimental Aeroacoustic Study of a Landing Gear in the Unsteady Flow Induced by a Propeller. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/1807/67867.

Council of Science Editors:

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


University of Toronto

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

Degree: 2018, University of Toronto

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Lane, Creighton. “Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations.” 2018. Masters Thesis, University of Toronto. Accessed July 07, 2020. http://hdl.handle.net/1807/89620.

MLA Handbook (7th Edition):

Lane, Creighton. “Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations.” 2018. Web. 07 Jul 2020.

Vancouver:

Lane C. Measurement of Turbulent Boundary Layer Induced Surface Pressure Fluctuations. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/1807/89620.

Council of Science Editors:

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


University of Waterloo

17. Bale, Adam Edward. The Application of MEMS Microphone Arrays to Aeroacoustic Measurements.

Degree: 2011, University of Waterloo

 Aeroacoustic emissions were identified as a primary concern in the public acceptance of wind turbines. A review of literature involving sound localization was undertaken and… (more)

Subjects/Keywords: Aeroacoustics; Microphone arrays; Wind turbines; MEMS

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APA (6th Edition):

Bale, A. E. (2011). The Application of MEMS Microphone Arrays to Aeroacoustic Measurements. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/5880

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bale, Adam Edward. “The Application of MEMS Microphone Arrays to Aeroacoustic Measurements.” 2011. Thesis, University of Waterloo. Accessed July 07, 2020. http://hdl.handle.net/10012/5880.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bale, Adam Edward. “The Application of MEMS Microphone Arrays to Aeroacoustic Measurements.” 2011. Web. 07 Jul 2020.

Vancouver:

Bale AE. The Application of MEMS Microphone Arrays to Aeroacoustic Measurements. [Internet] [Thesis]. University of Waterloo; 2011. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/10012/5880.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bale AE. The Application of MEMS Microphone Arrays to Aeroacoustic Measurements. [Thesis]. University of Waterloo; 2011. Available from: http://hdl.handle.net/10012/5880

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Delft University of Technology

18. Sinnige, T. (author). The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions.

Degree: 2013, Delft University of Technology

 Growing concerns about the environmental impact of aircraft operations and increasing fuel prices have led to the demand for more fuel-efficient aircraft. One of the… (more)

Subjects/Keywords: propeller; propeller noise; pylon blowing; aeroacoustics

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APA (6th Edition):

Sinnige, T. (. (2013). The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992

Chicago Manual of Style (16th Edition):

Sinnige, T (author). “The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions.” 2013. Masters Thesis, Delft University of Technology. Accessed July 07, 2020. http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992.

MLA Handbook (7th Edition):

Sinnige, T (author). “The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions.” 2013. Web. 07 Jul 2020.

Vancouver:

Sinnige T(. The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2020 Jul 07]. Available from: http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992.

Council of Science Editors:

Sinnige T(. The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992


Delft University of Technology

19. Candade, A.A. (author). Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects.

Degree: 2015, Delft University of Technology

 Advanced propeller propulsion systems potentially provide a significant reduction in fuel burn compared to traditional turbofans. An alternative to the conventional aft-fuselage mounted pusher layout… (more)

Subjects/Keywords: propeller; propulsion integration; vortex interactions; aeroacoustics

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APA (6th Edition):

Candade, A. A. (. (2015). Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135

Chicago Manual of Style (16th Edition):

Candade, A A (author). “Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects.” 2015. Masters Thesis, Delft University of Technology. Accessed July 07, 2020. http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135.

MLA Handbook (7th Edition):

Candade, A A (author). “Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects.” 2015. Web. 07 Jul 2020.

Vancouver:

Candade AA(. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Jul 07]. Available from: http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135.

Council of Science Editors:

Candade AA(. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135


University of Windsor

20. Patel, Krishna Rajendra. A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise.

Degree: MA, Mechanical, Automotive, and Materials Engineering, 2016, University of Windsor

 As turbofan engine designs move towards bypass ratios >12 and corresponding low pressure ratios, fan rotor blade tip Mach numbers are reduced, leading to rotor-stator… (more)

Subjects/Keywords: Aeroacoustics; Interaction; Noise; Non-uniform; Rotor; Stator

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

APA (6th Edition):

Patel, K. R. (2016). A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise. (Masters Thesis). University of Windsor. Retrieved from https://scholar.uwindsor.ca/etd/5860

Chicago Manual of Style (16th Edition):

Patel, Krishna Rajendra. “A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise.” 2016. Masters Thesis, University of Windsor. Accessed July 07, 2020. https://scholar.uwindsor.ca/etd/5860.

MLA Handbook (7th Edition):

Patel, Krishna Rajendra. “A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise.” 2016. Web. 07 Jul 2020.

Vancouver:

Patel KR. A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise. [Internet] [Masters thesis]. University of Windsor; 2016. [cited 2020 Jul 07]. Available from: https://scholar.uwindsor.ca/etd/5860.

Council of Science Editors:

Patel KR. A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise. [Masters Thesis]. University of Windsor; 2016. Available from: https://scholar.uwindsor.ca/etd/5860


Loughborough University

21. Rife, M. E. Large eddy simulations of high Reynolds number jets with microjet injection.

Degree: PhD, 2014, Loughborough University

 Continued growth of the aviation industry and increasingly strict noise requirements set by international bodies and airport authorities alike means that novel methods of reducing… (more)

Subjects/Keywords: 629.132; Jet noise; Aeroacoustics; Computational fluid dynamics; Computational aeroacoustics; Microjets; CFD; CAA

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

APA (6th Edition):

Rife, M. E. (2014). Large eddy simulations of high Reynolds number jets with microjet injection. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/14686

Chicago Manual of Style (16th Edition):

Rife, M E. “Large eddy simulations of high Reynolds number jets with microjet injection.” 2014. Doctoral Dissertation, Loughborough University. Accessed July 07, 2020. http://hdl.handle.net/2134/14686.

MLA Handbook (7th Edition):

Rife, M E. “Large eddy simulations of high Reynolds number jets with microjet injection.” 2014. Web. 07 Jul 2020.

Vancouver:

Rife ME. Large eddy simulations of high Reynolds number jets with microjet injection. [Internet] [Doctoral dissertation]. Loughborough University; 2014. [cited 2020 Jul 07]. Available from: http://hdl.handle.net/2134/14686.

Council of Science Editors:

Rife ME. Large eddy simulations of high Reynolds number jets with microjet injection. [Doctoral Dissertation]. Loughborough University; 2014. Available from: http://hdl.handle.net/2134/14686

22. Silva, Carlos Roberto Ilário da. Desenvolvimento de um novo método RANS-based para a aeroacústica computacional de jatos de alta velocidade.

Degree: PhD, Engenharia Mecânica de Energia de Fluidos, 2011, University of São Paulo

Uma nova ferramenta de aeroacústica computacional baseada em simulações RANS (Reynolds Averaged Navier-Stokes) foi desenvolvida para a predição do ruído gerado pelo escoamento tri-dimensional de… (more)

Subjects/Keywords: Aeroacoustics; Aeroacoustics analogy; Aeroacústica; Analogia acústica; Interação fluidoacústica; Jatos; Jets; Noise prediction; Predição de ruído; Sound-flow interaction

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

APA (6th Edition):

Silva, C. R. I. d. (2011). Desenvolvimento de um novo método RANS-based para a aeroacústica computacional de jatos de alta velocidade. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/3/3150/tde-02072012-163931/ ;

Chicago Manual of Style (16th Edition):

Silva, Carlos Roberto Ilário da. “Desenvolvimento de um novo método RANS-based para a aeroacústica computacional de jatos de alta velocidade.” 2011. Doctoral Dissertation, University of São Paulo. Accessed July 07, 2020. http://www.teses.usp.br/teses/disponiveis/3/3150/tde-02072012-163931/ ;.

MLA Handbook (7th Edition):

Silva, Carlos Roberto Ilário da. “Desenvolvimento de um novo método RANS-based para a aeroacústica computacional de jatos de alta velocidade.” 2011. Web. 07 Jul 2020.

Vancouver:

Silva CRId. Desenvolvimento de um novo método RANS-based para a aeroacústica computacional de jatos de alta velocidade. [Internet] [Doctoral dissertation]. University of São Paulo; 2011. [cited 2020 Jul 07]. Available from: http://www.teses.usp.br/teses/disponiveis/3/3150/tde-02072012-163931/ ;.

Council of Science Editors:

Silva CRId. Desenvolvimento de um novo método RANS-based para a aeroacústica computacional de jatos de alta velocidade. [Doctoral Dissertation]. University of São Paulo; 2011. Available from: http://www.teses.usp.br/teses/disponiveis/3/3150/tde-02072012-163931/ ;


University of Notre Dame

23. Michaela Marie Logue. Sound Generation and Scattering in Turbofan Engines</h1>.

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

  The reduction of fan noise contributions to the engine noise spectrum is an important area in overall engine design as noise restrictions on commercial… (more)

Subjects/Keywords: broadband noise; computational aeroacoustics; tonal noise; aeroacoustics

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APA (6th Edition):

Logue, M. M. (2010). Sound Generation and Scattering in Turbofan Engines</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/ft848p60w3j

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Logue, Michaela Marie. “Sound Generation and Scattering in Turbofan Engines</h1>.” 2010. Thesis, University of Notre Dame. Accessed July 07, 2020. https://curate.nd.edu/show/ft848p60w3j.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Logue, Michaela Marie. “Sound Generation and Scattering in Turbofan Engines</h1>.” 2010. Web. 07 Jul 2020.

Vancouver:

Logue MM. Sound Generation and Scattering in Turbofan Engines</h1>. [Internet] [Thesis]. University of Notre Dame; 2010. [cited 2020 Jul 07]. Available from: https://curate.nd.edu/show/ft848p60w3j.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Logue MM. Sound Generation and Scattering in Turbofan Engines</h1>. [Thesis]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/ft848p60w3j

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Delft University of Technology

24. Shubham, Shubham (author). Computational Aeroacoustic Investigation of Co-rotating rotors for Urban Air Mobility.

Degree: 2020, Delft University of Technology

Noise is a major issue in Urban Air Mobility vehicles, especially due to its operation in the urban environment. One of the major sources of… (more)

Subjects/Keywords: Aerodynamics; Aeroacoustics; Urban Air Mobility; Drone; Propeller; Rotor; Co-rotating rotor; PowerFLOW; Computational Fluid Dynamics (CFD); Computational Aeroacoustics

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

APA (6th Edition):

Shubham, S. (. (2020). Computational Aeroacoustic Investigation of Co-rotating rotors for Urban Air Mobility. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:72330591-d337-4467-9f89-b4693816f334

Chicago Manual of Style (16th Edition):

Shubham, Shubham (author). “Computational Aeroacoustic Investigation of Co-rotating rotors for Urban Air Mobility.” 2020. Masters Thesis, Delft University of Technology. Accessed July 07, 2020. http://resolver.tudelft.nl/uuid:72330591-d337-4467-9f89-b4693816f334.

MLA Handbook (7th Edition):

Shubham, Shubham (author). “Computational Aeroacoustic Investigation of Co-rotating rotors for Urban Air Mobility.” 2020. Web. 07 Jul 2020.

Vancouver:

Shubham S(. Computational Aeroacoustic Investigation of Co-rotating rotors for Urban Air Mobility. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2020 Jul 07]. Available from: http://resolver.tudelft.nl/uuid:72330591-d337-4467-9f89-b4693816f334.

Council of Science Editors:

Shubham S(. Computational Aeroacoustic Investigation of Co-rotating rotors for Urban Air Mobility. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:72330591-d337-4467-9f89-b4693816f334


Penn State University

25. Petitjean, Benoit Philippe. On the Nonlinearities in the Noise Radiated from High-Speed Model Jets.

Degree: PhD, Aerospace Engineering, 2006, Penn State University

 The role of nonlinearity in the generation and propagation of the noise radiated from high-performance jet aircraft is not a well understood phenomenon. To address… (more)

Subjects/Keywords: aeroacoustics; jet noise; nonlinear acoustics

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APA (6th Edition):

Petitjean, B. P. (2006). On the Nonlinearities in the Noise Radiated from High-Speed Model Jets. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/7371

Chicago Manual of Style (16th Edition):

Petitjean, Benoit Philippe. “On the Nonlinearities in the Noise Radiated from High-Speed Model Jets.” 2006. Doctoral Dissertation, Penn State University. Accessed July 07, 2020. https://etda.libraries.psu.edu/catalog/7371.

MLA Handbook (7th Edition):

Petitjean, Benoit Philippe. “On the Nonlinearities in the Noise Radiated from High-Speed Model Jets.” 2006. Web. 07 Jul 2020.

Vancouver:

Petitjean BP. On the Nonlinearities in the Noise Radiated from High-Speed Model Jets. [Internet] [Doctoral dissertation]. Penn State University; 2006. [cited 2020 Jul 07]. Available from: https://etda.libraries.psu.edu/catalog/7371.

Council of Science Editors:

Petitjean BP. On the Nonlinearities in the Noise Radiated from High-Speed Model Jets. [Doctoral Dissertation]. Penn State University; 2006. Available from: https://etda.libraries.psu.edu/catalog/7371


Penn State University

26. Lampenfield, Jacob John. Simulations of the flow generated by fluidic inserts in a converging diverging nozzle.

Degree: MS, Aerospace Engineering, 2016, Penn State University

 This investigation of military jet noise prediction and reduction is a continuation from previous projects and is still ongoing. Numerical simulations have been performed on… (more)

Subjects/Keywords: CFD; computational fluid dynamics; converging; diverging; nozzle; aeroacoustics; noise reduction

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

APA (6th Edition):

Lampenfield, J. J. (2016). Simulations of the flow generated by fluidic inserts in a converging diverging nozzle. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/29170

Chicago Manual of Style (16th Edition):

Lampenfield, Jacob John. “Simulations of the flow generated by fluidic inserts in a converging diverging nozzle.” 2016. Masters Thesis, Penn State University. Accessed July 07, 2020. https://etda.libraries.psu.edu/catalog/29170.

MLA Handbook (7th Edition):

Lampenfield, Jacob John. “Simulations of the flow generated by fluidic inserts in a converging diverging nozzle.” 2016. Web. 07 Jul 2020.

Vancouver:

Lampenfield JJ. Simulations of the flow generated by fluidic inserts in a converging diverging nozzle. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2020 Jul 07]. Available from: https://etda.libraries.psu.edu/catalog/29170.

Council of Science Editors:

Lampenfield JJ. Simulations of the flow generated by fluidic inserts in a converging diverging nozzle. [Masters Thesis]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/29170


Penn State University

27. Leonard, Daniel Joseph. AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS.

Degree: MS, Aerospace Engineering, 2010, Penn State University

 This thesis addresses the sound radiated from a turbulent jet-wall interaction in a duct which was measured for several jet-wall interaction geometries. This sound production… (more)

Subjects/Keywords: unvoiced; turbulent jet; vortex; speech; acoustics; aeroacoustics; sound; source spectrum

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APA (6th Edition):

Leonard, D. J. (2010). AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9633

Chicago Manual of Style (16th Edition):

Leonard, Daniel Joseph. “AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS.” 2010. Masters Thesis, Penn State University. Accessed July 07, 2020. https://etda.libraries.psu.edu/catalog/9633.

MLA Handbook (7th Edition):

Leonard, Daniel Joseph. “AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS.” 2010. Web. 07 Jul 2020.

Vancouver:

Leonard DJ. AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2020 Jul 07]. Available from: https://etda.libraries.psu.edu/catalog/9633.

Council of Science Editors:

Leonard DJ. AEROACOUSTICS OF CONFINED JET-WALL INTERACTIONS WITH APPLICATION TO UNVOICED SPEECH SOUNDS. [Masters Thesis]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/9633


Penn State University

28. Lee, Seongkyu. Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise.

Degree: PhD, Aerospace Engineering, 2009, Penn State University

 This work aims at the development of a numerical method for the analysis of acoustic scattering in the time domain and its applications to rotorcraft… (more)

Subjects/Keywords: acoustic scattering; helicopter noise; equivalent source method; pressure gradient; aeroacoustics

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APA (6th Edition):

Lee, S. (2009). Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9323

Chicago Manual of Style (16th Edition):

Lee, Seongkyu. “Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise.” 2009. Doctoral Dissertation, Penn State University. Accessed July 07, 2020. https://etda.libraries.psu.edu/catalog/9323.

MLA Handbook (7th Edition):

Lee, Seongkyu. “Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise.” 2009. Web. 07 Jul 2020.

Vancouver:

Lee S. Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise. [Internet] [Doctoral dissertation]. Penn State University; 2009. [cited 2020 Jul 07]. Available from: https://etda.libraries.psu.edu/catalog/9323.

Council of Science Editors:

Lee S. Prediction of Acoustic Scattering in the Time Domain and its Applications to Rotorcraft Noise. [Doctoral Dissertation]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9323


The Ohio State University

29. Kastner, Jeffrey F. Far-field radiated noise mechanisms in high reynolds number and high-speed jets.

Degree: PhD, Mechanical Engineering, 2007, The Ohio State University

 The present research examines the relationship between the large-scale structure dynamics of a jet and the far-field sound. This was achieved by exploring the flowfield… (more)

Subjects/Keywords: Engineering, Mechanical; Fluid Dynamics; Gas Dynamics; Aeroacoustics; Optical Diagnostics

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

APA (6th Edition):

Kastner, J. F. (2007). Far-field radiated noise mechanisms in high reynolds number and high-speed jets. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1181753004

Chicago Manual of Style (16th Edition):

Kastner, Jeffrey F. “Far-field radiated noise mechanisms in high reynolds number and high-speed jets.” 2007. Doctoral Dissertation, The Ohio State University. Accessed July 07, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1181753004.

MLA Handbook (7th Edition):

Kastner, Jeffrey F. “Far-field radiated noise mechanisms in high reynolds number and high-speed jets.” 2007. Web. 07 Jul 2020.

Vancouver:

Kastner JF. Far-field radiated noise mechanisms in high reynolds number and high-speed jets. [Internet] [Doctoral dissertation]. The Ohio State University; 2007. [cited 2020 Jul 07]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1181753004.

Council of Science Editors:

Kastner JF. Far-field radiated noise mechanisms in high reynolds number and high-speed jets. [Doctoral Dissertation]. The Ohio State University; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1181753004


RMIT University

30. Wasko, M. The numerical and experimental study of the aeroacoustic noise of motor vehicle alternators.

Degree: 2009, RMIT University

 The aeroacoustics of a simplified alternator are analysed within the framework of this thesis, with the objective being the development of a tool capable of… (more)

Subjects/Keywords: Fields of Research; aeroacoustics; noise; sound; alternator; vehicle; Lowson

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

APA (6th Edition):

Wasko, M. (2009). The numerical and experimental study of the aeroacoustic noise of motor vehicle alternators. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:9284

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Wasko, M. “The numerical and experimental study of the aeroacoustic noise of motor vehicle alternators.” 2009. Thesis, RMIT University. Accessed July 07, 2020. http://researchbank.rmit.edu.au/view/rmit:9284.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Wasko, M. “The numerical and experimental study of the aeroacoustic noise of motor vehicle alternators.” 2009. Web. 07 Jul 2020.

Vancouver:

Wasko M. The numerical and experimental study of the aeroacoustic noise of motor vehicle alternators. [Internet] [Thesis]. RMIT University; 2009. [cited 2020 Jul 07]. Available from: http://researchbank.rmit.edu.au/view/rmit:9284.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Wasko M. The numerical and experimental study of the aeroacoustic noise of motor vehicle alternators. [Thesis]. RMIT University; 2009. Available from: http://researchbank.rmit.edu.au/view/rmit:9284

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

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