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You searched for subject:(Aeroacoustic). Showing records 1 – 30 of 35 total matches.

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University of Toronto

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

Degree: 2016, University of Toronto

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Chow, Derrick. “Design and Characterization of the UTIAS Anechoic Wind Tunnel.” 2016. Masters Thesis, University of Toronto. Accessed August 14, 2020. http://hdl.handle.net/1807/71668.

MLA Handbook (7th Edition):

Chow, Derrick. “Design and Characterization of the UTIAS Anechoic Wind Tunnel.” 2016. Web. 14 Aug 2020.

Vancouver:

Chow D. Design and Characterization of the UTIAS Anechoic Wind Tunnel. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/1807/71668.

Council of Science Editors:

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


Delft University of Technology

2. Haddaoui, Mohammed (author). Development of a Propeller Source Noise Model.

Degree: 2019, Delft University of Technology

 Turboprop engines are known for their high fuel efficiency on short-range missions compared to turbofan engines. A disadvantage of turboprop engines is the noise they… (more)

Subjects/Keywords: Propeller noise; Aeroacoustic; Noise prediction

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APA (6th Edition):

Haddaoui, M. (. (2019). Development of a Propeller Source Noise Model. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f8e13c98-08b6-4280-ad2d-034fd8a6b63e

Chicago Manual of Style (16th Edition):

Haddaoui, Mohammed (author). “Development of a Propeller Source Noise Model.” 2019. Masters Thesis, Delft University of Technology. Accessed August 14, 2020. http://resolver.tudelft.nl/uuid:f8e13c98-08b6-4280-ad2d-034fd8a6b63e.

MLA Handbook (7th Edition):

Haddaoui, Mohammed (author). “Development of a Propeller Source Noise Model.” 2019. Web. 14 Aug 2020.

Vancouver:

Haddaoui M(. Development of a Propeller Source Noise Model. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Aug 14]. Available from: http://resolver.tudelft.nl/uuid:f8e13c98-08b6-4280-ad2d-034fd8a6b63e.

Council of Science Editors:

Haddaoui M(. Development of a Propeller Source Noise Model. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:f8e13c98-08b6-4280-ad2d-034fd8a6b63e


University of New South Wales

3. Karimi, Mahmoud. Periodic boundary element technique for acoustic and aeroacoustic applications.

Degree: Mechanical & Manufacturing Engineering, 2016, University of New South Wales

 Two major hurdles associated with simulation of exterior acoustic problems are the memory requirement and computation time. A vast amount of memory is required to… (more)

Subjects/Keywords: Boundary element method; Acoustic; Aeroacoustic; Periodic structures

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APA (6th Edition):

Karimi, M. (2016). Periodic boundary element technique for acoustic and aeroacoustic applications. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/57078 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42446/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Karimi, Mahmoud. “Periodic boundary element technique for acoustic and aeroacoustic applications.” 2016. Doctoral Dissertation, University of New South Wales. Accessed August 14, 2020. http://handle.unsw.edu.au/1959.4/57078 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42446/SOURCE02?view=true.

MLA Handbook (7th Edition):

Karimi, Mahmoud. “Periodic boundary element technique for acoustic and aeroacoustic applications.” 2016. Web. 14 Aug 2020.

Vancouver:

Karimi M. Periodic boundary element technique for acoustic and aeroacoustic applications. [Internet] [Doctoral dissertation]. University of New South Wales; 2016. [cited 2020 Aug 14]. Available from: http://handle.unsw.edu.au/1959.4/57078 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42446/SOURCE02?view=true.

Council of Science Editors:

Karimi M. Periodic boundary element technique for acoustic and aeroacoustic applications. [Doctoral Dissertation]. University of New South Wales; 2016. Available from: http://handle.unsw.edu.au/1959.4/57078 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:42446/SOURCE02?view=true


Queen Mary, University of London

4. Selfridge, R. Real-time sound synthesis of aeroacoustic sounds using physically derived models.

Degree: PhD, 2019, Queen Mary, University of London

 This thesis examines the use of a novel synthesis approach to reproduce aeroacoustic sound effects. This requires research into the fi eld of fluid dynamics… (more)

Subjects/Keywords: Aeroacoustic Sounds; fluid dynamics; replication; Audio Engineering

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APA (6th Edition):

Selfridge, R. (2019). Real-time sound synthesis of aeroacoustic sounds using physically derived models. (Doctoral Dissertation). Queen Mary, University of London. Retrieved from http://qmro.qmul.ac.uk/xmlui/handle/123456789/58445 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.781009

Chicago Manual of Style (16th Edition):

Selfridge, R. “Real-time sound synthesis of aeroacoustic sounds using physically derived models.” 2019. Doctoral Dissertation, Queen Mary, University of London. Accessed August 14, 2020. http://qmro.qmul.ac.uk/xmlui/handle/123456789/58445 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.781009.

MLA Handbook (7th Edition):

Selfridge, R. “Real-time sound synthesis of aeroacoustic sounds using physically derived models.” 2019. Web. 14 Aug 2020.

Vancouver:

Selfridge R. Real-time sound synthesis of aeroacoustic sounds using physically derived models. [Internet] [Doctoral dissertation]. Queen Mary, University of London; 2019. [cited 2020 Aug 14]. Available from: http://qmro.qmul.ac.uk/xmlui/handle/123456789/58445 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.781009.

Council of Science Editors:

Selfridge R. Real-time sound synthesis of aeroacoustic sounds using physically derived models. [Doctoral Dissertation]. Queen Mary, University of London; 2019. Available from: http://qmro.qmul.ac.uk/xmlui/handle/123456789/58445 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.781009


Iowa State University

5. Ning, Zhe. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers.

Degree: 2018, Iowa State University

 Unmanned aerial system (UAS) is a hot topic in both industry and academia fields. As a popular planform, the rotary-wing system gains more attentions. The… (more)

Subjects/Keywords: aeroacoustic; Aerodynamic; experiment; Icing; propeller; UAS; Engineering

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APA (6th Edition):

Ning, Z. (2018). Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/16427

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):

Ning, Zhe. “Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers.” 2018. Thesis, Iowa State University. Accessed August 14, 2020. https://lib.dr.iastate.edu/etd/16427.

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

MLA Handbook (7th Edition):

Ning, Zhe. “Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers.” 2018. Web. 14 Aug 2020.

Vancouver:

Ning Z. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. [Internet] [Thesis]. Iowa State University; 2018. [cited 2020 Aug 14]. Available from: https://lib.dr.iastate.edu/etd/16427.

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

Council of Science Editors:

Ning Z. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. [Thesis]. Iowa State University; 2018. Available from: https://lib.dr.iastate.edu/etd/16427

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


Delft University of Technology

6. Brandetti, Livia (author). Beamforming applied to Small Wind Turbines.

Degree: 2018, Delft University of Technology

 The increase of energy consumption as well as the need to reduce green-house emissions trigger the shift from a fossil-fuel based society towards a sustainable… (more)

Subjects/Keywords: Beamforming; Small wind turbine; Aeroacoustic; Noise

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APA (6th Edition):

Brandetti, L. (. (2018). Beamforming applied to Small Wind Turbines. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:bbee225f-a3bc-4730-b5f7-1d6f549decc7

Chicago Manual of Style (16th Edition):

Brandetti, Livia (author). “Beamforming applied to Small Wind Turbines.” 2018. Masters Thesis, Delft University of Technology. Accessed August 14, 2020. http://resolver.tudelft.nl/uuid:bbee225f-a3bc-4730-b5f7-1d6f549decc7.

MLA Handbook (7th Edition):

Brandetti, Livia (author). “Beamforming applied to Small Wind Turbines.” 2018. Web. 14 Aug 2020.

Vancouver:

Brandetti L(. Beamforming applied to Small Wind Turbines. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2020 Aug 14]. Available from: http://resolver.tudelft.nl/uuid:bbee225f-a3bc-4730-b5f7-1d6f549decc7.

Council of Science Editors:

Brandetti L(. Beamforming applied to Small Wind Turbines. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:bbee225f-a3bc-4730-b5f7-1d6f549decc7


Georgia Tech

7. Schatzman, Natasha Lydia. Aerodynamics and aeroacoustic sources of a coaxial rotor.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Vehicles with coaxial, contra-rotating rotor systems (CACR) are being considered for a range of applications, including those requiring high speed and operations in urban environments.… (more)

Subjects/Keywords: Rotorcraft; Helicopter; Coaxial; Noise; Aerodynamics; Aeroacoustic; Rotor; CFD

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APA (6th Edition):

Schatzman, N. L. (2018). Aerodynamics and aeroacoustic sources of a coaxial rotor. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59922

Chicago Manual of Style (16th Edition):

Schatzman, Natasha Lydia. “Aerodynamics and aeroacoustic sources of a coaxial rotor.” 2018. Doctoral Dissertation, Georgia Tech. Accessed August 14, 2020. http://hdl.handle.net/1853/59922.

MLA Handbook (7th Edition):

Schatzman, Natasha Lydia. “Aerodynamics and aeroacoustic sources of a coaxial rotor.” 2018. Web. 14 Aug 2020.

Vancouver:

Schatzman NL. Aerodynamics and aeroacoustic sources of a coaxial rotor. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/1853/59922.

Council of Science Editors:

Schatzman NL. Aerodynamics and aeroacoustic sources of a coaxial rotor. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59922

8. Shaaban, Ayman. Sound Generation By Flow Over Multiple Shallow Cavities.

Degree: PhD, 2018, McMaster University

 Corrugated pipes are widely used in offshore gas and oil fields for their flexibility while offering local rigidity. However, self-sustained pressure pulsations associated with the… (more)

Subjects/Keywords: multiple cavities; corrugated pipes; aeroacoustic source; fluid-structure interaction; flow-sound interaction; PIV

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APA (6th Edition):

Shaaban, A. (2018). Sound Generation By Flow Over Multiple Shallow Cavities. (Doctoral Dissertation). McMaster University. Retrieved from http://hdl.handle.net/11375/23390

Chicago Manual of Style (16th Edition):

Shaaban, Ayman. “Sound Generation By Flow Over Multiple Shallow Cavities.” 2018. Doctoral Dissertation, McMaster University. Accessed August 14, 2020. http://hdl.handle.net/11375/23390.

MLA Handbook (7th Edition):

Shaaban, Ayman. “Sound Generation By Flow Over Multiple Shallow Cavities.” 2018. Web. 14 Aug 2020.

Vancouver:

Shaaban A. Sound Generation By Flow Over Multiple Shallow Cavities. [Internet] [Doctoral dissertation]. McMaster University; 2018. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/11375/23390.

Council of Science Editors:

Shaaban A. Sound Generation By Flow Over Multiple Shallow Cavities. [Doctoral Dissertation]. McMaster University; 2018. Available from: http://hdl.handle.net/11375/23390


Virginia Tech

9. Leitch, Thomas A. Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing.

Degree: MS, Mechanical Engineering, 1997, Virginia Tech

 An aeroacoustic investigation was performed to assess the effects of adding mass flow at the trailing edges of four stators upstream of an aircraft engine… (more)

Subjects/Keywords: Trailing Edge Blowing; Aeroacoustic; Noise; Turbomachinery

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APA (6th Edition):

Leitch, T. A. (1997). Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30527

Chicago Manual of Style (16th Edition):

Leitch, Thomas A. “Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing.” 1997. Masters Thesis, Virginia Tech. Accessed August 14, 2020. http://hdl.handle.net/10919/30527.

MLA Handbook (7th Edition):

Leitch, Thomas A. “Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing.” 1997. Web. 14 Aug 2020.

Vancouver:

Leitch TA. Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing. [Internet] [Masters thesis]. Virginia Tech; 1997. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/10919/30527.

Council of Science Editors:

Leitch TA. Reduction of Unsteady Rotor-Stator Interaction Using Trailing Edge Blowing. [Masters Thesis]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/30527


University of Alberta

10. Brougham, Michael V. Theoretical Framework for Modeling Ingressive Phonation.

Degree: MS, Department of Mechanical Engineering, 2012, University of Alberta

 Researchers in vocal acoustics have used computer simulations of single and multi-mass models of the human vocal folds to study human phonation for over 40… (more)

Subjects/Keywords: Aerodynamic state feedback; Modal analysis; Vocal tract and subglottal resonators; Ingressive phonation using a multi-mass model; Aeroacoustic coupling; Mucosal wave

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APA (6th Edition):

Brougham, M. V. (2012). Theoretical Framework for Modeling Ingressive Phonation. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/sn009z00f

Chicago Manual of Style (16th Edition):

Brougham, Michael V. “Theoretical Framework for Modeling Ingressive Phonation.” 2012. Masters Thesis, University of Alberta. Accessed August 14, 2020. https://era.library.ualberta.ca/files/sn009z00f.

MLA Handbook (7th Edition):

Brougham, Michael V. “Theoretical Framework for Modeling Ingressive Phonation.” 2012. Web. 14 Aug 2020.

Vancouver:

Brougham MV. Theoretical Framework for Modeling Ingressive Phonation. [Internet] [Masters thesis]. University of Alberta; 2012. [cited 2020 Aug 14]. Available from: https://era.library.ualberta.ca/files/sn009z00f.

Council of Science Editors:

Brougham MV. Theoretical Framework for Modeling Ingressive Phonation. [Masters Thesis]. University of Alberta; 2012. Available from: https://era.library.ualberta.ca/files/sn009z00f

11. Lacombe, Romain. Sifflement de diaphragmes en conduit soumis à un écoulement subsonique turbulent : Whistling of orifices in duct under turbulent subsonic flow.

Degree: Docteur es, Acoustique, 2011, Le Mans

Les diaphragmes utilisés comme organes de perte de charge à l'intérieur des tuyauteries de centrales électriques ont été mis en cause dans la création de… (more)

Subjects/Keywords: Sifflements; Aéroacoustique; Instabilité aérodynamique; Oscillations auto-entretenues; Méthode à deux sources; Simulations RANS / LES; Whistling; Aeroacoustic; Aerodynamic instability

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APA (6th Edition):

Lacombe, R. (2011). Sifflement de diaphragmes en conduit soumis à un écoulement subsonique turbulent : Whistling of orifices in duct under turbulent subsonic flow. (Doctoral Dissertation). Le Mans. Retrieved from http://www.theses.fr/2011LEMA1003

Chicago Manual of Style (16th Edition):

Lacombe, Romain. “Sifflement de diaphragmes en conduit soumis à un écoulement subsonique turbulent : Whistling of orifices in duct under turbulent subsonic flow.” 2011. Doctoral Dissertation, Le Mans. Accessed August 14, 2020. http://www.theses.fr/2011LEMA1003.

MLA Handbook (7th Edition):

Lacombe, Romain. “Sifflement de diaphragmes en conduit soumis à un écoulement subsonique turbulent : Whistling of orifices in duct under turbulent subsonic flow.” 2011. Web. 14 Aug 2020.

Vancouver:

Lacombe R. Sifflement de diaphragmes en conduit soumis à un écoulement subsonique turbulent : Whistling of orifices in duct under turbulent subsonic flow. [Internet] [Doctoral dissertation]. Le Mans; 2011. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2011LEMA1003.

Council of Science Editors:

Lacombe R. Sifflement de diaphragmes en conduit soumis à un écoulement subsonique turbulent : Whistling of orifices in duct under turbulent subsonic flow. [Doctoral Dissertation]. Le Mans; 2011. Available from: http://www.theses.fr/2011LEMA1003


The Ohio State University

12. Malone, James Michael. An Analysis of the Nonlinear Interaction of Peak Frequencies in Resonant Cavity Flows.

Degree: MS, Mechanical Engineering, 2008, The Ohio State University

 Shallow cavity flows, commonly found on aircraft, are currently an area of significant research. Active flow control is desirable to improve aircraft performance and efficiency… (more)

Subjects/Keywords: Acoustics; Engineering; Fluid Dynamics; Mechanical Engineering; Technology; Rossiter modes; rectangular; cavity; resonance; amplitude modulation; fundamental aeroacoustic loop

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APA (6th Edition):

Malone, J. M. (2008). An Analysis of the Nonlinear Interaction of Peak Frequencies in Resonant Cavity Flows. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1204037947

Chicago Manual of Style (16th Edition):

Malone, James Michael. “An Analysis of the Nonlinear Interaction of Peak Frequencies in Resonant Cavity Flows.” 2008. Masters Thesis, The Ohio State University. Accessed August 14, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1204037947.

MLA Handbook (7th Edition):

Malone, James Michael. “An Analysis of the Nonlinear Interaction of Peak Frequencies in Resonant Cavity Flows.” 2008. Web. 14 Aug 2020.

Vancouver:

Malone JM. An Analysis of the Nonlinear Interaction of Peak Frequencies in Resonant Cavity Flows. [Internet] [Masters thesis]. The Ohio State University; 2008. [cited 2020 Aug 14]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1204037947.

Council of Science Editors:

Malone JM. An Analysis of the Nonlinear Interaction of Peak Frequencies in Resonant Cavity Flows. [Masters Thesis]. The Ohio State University; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1204037947

13. Pene, Yves. Antennerie numérique pour la caractérisation de sources aéroacoustiques en milieu complexe : CAA-based beamforming for aeroacoustic noise source identification in complex media.

Degree: Docteur es, Acoustique, 2015, Université Pierre et Marie Curie – Paris VI

L’antennerie acoustique, aussi appelée formation de voies, est une technique d’identification acoustique basée sur un modèle de propagation analytique entre les sources de bruit et… (more)

Subjects/Keywords: Aéroacoustique; Imagerie; Formation de voies; Milieu de propagation complexe; Simulation numérique; Fonction de Green; Green function; Aeroacoustic; 534

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APA (6th Edition):

Pene, Y. (2015). Antennerie numérique pour la caractérisation de sources aéroacoustiques en milieu complexe : CAA-based beamforming for aeroacoustic noise source identification in complex media. (Doctoral Dissertation). Université Pierre et Marie Curie – Paris VI. Retrieved from http://www.theses.fr/2015PA066167

Chicago Manual of Style (16th Edition):

Pene, Yves. “Antennerie numérique pour la caractérisation de sources aéroacoustiques en milieu complexe : CAA-based beamforming for aeroacoustic noise source identification in complex media.” 2015. Doctoral Dissertation, Université Pierre et Marie Curie – Paris VI. Accessed August 14, 2020. http://www.theses.fr/2015PA066167.

MLA Handbook (7th Edition):

Pene, Yves. “Antennerie numérique pour la caractérisation de sources aéroacoustiques en milieu complexe : CAA-based beamforming for aeroacoustic noise source identification in complex media.” 2015. Web. 14 Aug 2020.

Vancouver:

Pene Y. Antennerie numérique pour la caractérisation de sources aéroacoustiques en milieu complexe : CAA-based beamforming for aeroacoustic noise source identification in complex media. [Internet] [Doctoral dissertation]. Université Pierre et Marie Curie – Paris VI; 2015. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2015PA066167.

Council of Science Editors:

Pene Y. Antennerie numérique pour la caractérisation de sources aéroacoustiques en milieu complexe : CAA-based beamforming for aeroacoustic noise source identification in complex media. [Doctoral Dissertation]. Université Pierre et Marie Curie – Paris VI; 2015. Available from: http://www.theses.fr/2015PA066167

14. Parisot-Dupuis, Hélène. Application de l'holographie acoustique en soufflerie par mesures LDV : Application of acoustic holography in wind tunnel by means of LDV measurements.

Degree: Docteur es, Dynamique des fluides, 2012, Toulouse, ISAE

L’ Holographie acoustique de champ proche (NAH) est une méthode d’imagerie acoustique robuste, mais son application en écoulement peut être limitée par l’utilisation de mesures… (more)

Subjects/Keywords: Holographie acoustique de champ proche; Aéroacoustique; Soufflerie; Vélocimétrie laser Doppler; Nearfield acoustic holography; Aeroacoustic; Wind tunnel; Laser Doppler velocimetry; 532

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APA (6th Edition):

Parisot-Dupuis, H. (2012). Application de l'holographie acoustique en soufflerie par mesures LDV : Application of acoustic holography in wind tunnel by means of LDV measurements. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2012ESAE0035

Chicago Manual of Style (16th Edition):

Parisot-Dupuis, Hélène. “Application de l'holographie acoustique en soufflerie par mesures LDV : Application of acoustic holography in wind tunnel by means of LDV measurements.” 2012. Doctoral Dissertation, Toulouse, ISAE. Accessed August 14, 2020. http://www.theses.fr/2012ESAE0035.

MLA Handbook (7th Edition):

Parisot-Dupuis, Hélène. “Application de l'holographie acoustique en soufflerie par mesures LDV : Application of acoustic holography in wind tunnel by means of LDV measurements.” 2012. Web. 14 Aug 2020.

Vancouver:

Parisot-Dupuis H. Application de l'holographie acoustique en soufflerie par mesures LDV : Application of acoustic holography in wind tunnel by means of LDV measurements. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2012. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2012ESAE0035.

Council of Science Editors:

Parisot-Dupuis H. Application de l'holographie acoustique en soufflerie par mesures LDV : Application of acoustic holography in wind tunnel by means of LDV measurements. [Doctoral Dissertation]. Toulouse, ISAE; 2012. Available from: http://www.theses.fr/2012ESAE0035

15. Gojon, Romain. Etude de jets supersoniques impactant une paroi par simulation numérique : Analyse aérodynamique et acoustique des mécanismes de rétroaction : Transport de particules solides dans une couche limite turbulente en présence de collines gaussiennes.

Degree: Docteur es, Mécanique des fluides, 2015, Ecully, Ecole centrale de Lyon

Cette thèse est consacrée à l'étude des propriétés aéroacoustiques de jets supersoniques impactant une paroi par simulation des grandes échelles. Ces simulations sont réalisées à… (more)

Subjects/Keywords: Jets supersoniques; Simulation des grandes échelles; Rétroaction; Paroi; Supersonic impinging jets; Large-eddy simulation; Aeroacoustic feedback

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APA (6th Edition):

Gojon, R. (2015). Etude de jets supersoniques impactant une paroi par simulation numérique : Analyse aérodynamique et acoustique des mécanismes de rétroaction : Transport de particules solides dans une couche limite turbulente en présence de collines gaussiennes. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon. Retrieved from http://www.theses.fr/2015ECDL0039

Chicago Manual of Style (16th Edition):

Gojon, Romain. “Etude de jets supersoniques impactant une paroi par simulation numérique : Analyse aérodynamique et acoustique des mécanismes de rétroaction : Transport de particules solides dans une couche limite turbulente en présence de collines gaussiennes.” 2015. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed August 14, 2020. http://www.theses.fr/2015ECDL0039.

MLA Handbook (7th Edition):

Gojon, Romain. “Etude de jets supersoniques impactant une paroi par simulation numérique : Analyse aérodynamique et acoustique des mécanismes de rétroaction : Transport de particules solides dans une couche limite turbulente en présence de collines gaussiennes.” 2015. Web. 14 Aug 2020.

Vancouver:

Gojon R. Etude de jets supersoniques impactant une paroi par simulation numérique : Analyse aérodynamique et acoustique des mécanismes de rétroaction : Transport de particules solides dans une couche limite turbulente en présence de collines gaussiennes. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2015. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2015ECDL0039.

Council of Science Editors:

Gojon R. Etude de jets supersoniques impactant une paroi par simulation numérique : Analyse aérodynamique et acoustique des mécanismes de rétroaction : Transport de particules solides dans une couche limite turbulente en présence de collines gaussiennes. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; 2015. Available from: http://www.theses.fr/2015ECDL0039


Delft University of Technology

16. Vlemmix, Christian (author). Acoustic Array Design: The design of a reconfigurable phased microphone array for aeroacoustic wind tunnel measurements.

Degree: 2017, Delft University of Technology

Since both the aircraft and wind energy sectors are experiencing rapid growth, improvements must be made in terms of noise reduction as to enable growth… (more)

Subjects/Keywords: acoustic; noise; array; microphone; phased; wind; tunnel; experiment; aeroacoustic; sound; beamforming; CLEAN-PSF; CLEAN-SC; calibration

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APA (6th Edition):

Vlemmix, C. (. (2017). Acoustic Array Design: The design of a reconfigurable phased microphone array for aeroacoustic wind tunnel measurements. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:db51ea64-71b1-446d-9022-61842f2e794a

Chicago Manual of Style (16th Edition):

Vlemmix, Christian (author). “Acoustic Array Design: The design of a reconfigurable phased microphone array for aeroacoustic wind tunnel measurements.” 2017. Masters Thesis, Delft University of Technology. Accessed August 14, 2020. http://resolver.tudelft.nl/uuid:db51ea64-71b1-446d-9022-61842f2e794a.

MLA Handbook (7th Edition):

Vlemmix, Christian (author). “Acoustic Array Design: The design of a reconfigurable phased microphone array for aeroacoustic wind tunnel measurements.” 2017. Web. 14 Aug 2020.

Vancouver:

Vlemmix C(. Acoustic Array Design: The design of a reconfigurable phased microphone array for aeroacoustic wind tunnel measurements. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Aug 14]. Available from: http://resolver.tudelft.nl/uuid:db51ea64-71b1-446d-9022-61842f2e794a.

Council of Science Editors:

Vlemmix C(. Acoustic Array Design: The design of a reconfigurable phased microphone array for aeroacoustic wind tunnel measurements. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:db51ea64-71b1-446d-9022-61842f2e794a


Delft University of Technology

17. Mayer, Jonathan (author). Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications.

Degree: 2019, Delft University of Technology

For many aerospace applications, the dominant airfoil self-noise source is Turbulent Boundary Layer Trailing Edge (TBL-TE) noise. The replacement of solid airfoil trailing edges with… (more)

Subjects/Keywords: porous material; trailing edge noise; polymeric coating; airfoil self-noise; trailing edge heating; aeroacoustic; permeable material

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APA (6th Edition):

Mayer, J. (. (2019). Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10

Chicago Manual of Style (16th Edition):

Mayer, Jonathan (author). “Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications.” 2019. Masters Thesis, Delft University of Technology. Accessed August 14, 2020. http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10.

MLA Handbook (7th Edition):

Mayer, Jonathan (author). “Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications.” 2019. Web. 14 Aug 2020.

Vancouver:

Mayer J(. Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Aug 14]. Available from: http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10.

Council of Science Editors:

Mayer J(. Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10


Indian Institute of Science

18. Shivakanth Chary, P. Linear Stability Models for Reacting Mixing Layers.

Degree: MSc Engg, Faculty of Engineering, 2018, Indian Institute of Science

 We develop a physics-based reduced-order model of the aero-acoustic sound sources in reacting mixing layers as a method for fast and accurate predictions of the… (more)

Subjects/Keywords: Aeroacoustic Theory; Supersonic Mixing Layers; Aeroacoustic Sound Sources - Model; Compressible Reacting Mixing Layers; Coherent Structures; Supersonic Reacting Mixing Layers; Linear Stability Equations; Linear Parabolized Stability Equations; PSE Equations; Linear Stability Models; Aerospace Engineering

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APA (6th Edition):

Shivakanth Chary, P. (2018). Linear Stability Models for Reacting Mixing Layers. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/3267

Chicago Manual of Style (16th Edition):

Shivakanth Chary, P. “Linear Stability Models for Reacting Mixing Layers.” 2018. Masters Thesis, Indian Institute of Science. Accessed August 14, 2020. http://etd.iisc.ac.in/handle/2005/3267.

MLA Handbook (7th Edition):

Shivakanth Chary, P. “Linear Stability Models for Reacting Mixing Layers.” 2018. Web. 14 Aug 2020.

Vancouver:

Shivakanth Chary P. Linear Stability Models for Reacting Mixing Layers. [Internet] [Masters thesis]. Indian Institute of Science; 2018. [cited 2020 Aug 14]. Available from: http://etd.iisc.ac.in/handle/2005/3267.

Council of Science Editors:

Shivakanth Chary P. Linear Stability Models for Reacting Mixing Layers. [Masters Thesis]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/3267

19. Pagani Júnior, Carlos do Carmo. Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS.

Degree: PhD, Aeronaves, 2014, University of São Paulo

 A redução do ruído externo gerado por aeronaves operando nas proximidades de grandes centros urbanos é apontada como uma questão vital para a manutenção e… (more)

Subjects/Keywords: Beam-forming acústico; Acoustic beam-forming; Aeroacoustic measurements; Aerofólio hiper-sustentador; Deconvolução DAMAS; Deconvolution DAMAS.; High-lift airfoil; Medições aeroacústicas; Ruído de eslate; Slat noise

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APA (6th Edition):

Pagani Júnior, C. d. C. (2014). Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;

Chicago Manual of Style (16th Edition):

Pagani Júnior, Carlos do Carmo. “Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS.” 2014. Doctoral Dissertation, University of São Paulo. Accessed August 14, 2020. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;.

MLA Handbook (7th Edition):

Pagani Júnior, Carlos do Carmo. “Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS.” 2014. Web. 14 Aug 2020.

Vancouver:

Pagani Júnior CdC. Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS. [Internet] [Doctoral dissertation]. University of São Paulo; 2014. [cited 2020 Aug 14]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;.

Council of Science Editors:

Pagani Júnior CdC. Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS. [Doctoral Dissertation]. University of São Paulo; 2014. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;


Penn State University

20. Veltin, Jeremy. On the Characterization of Noise Sources in Supersonic Shock Containing Jets.

Degree: 2008, Penn State University

 Research on the noise produced by military aircraft has seen a renewed interest due to the increasing concerns of communities around airbases and airports. Radiated… (more)

Subjects/Keywords: jet noise; aeroacoustic; supersonic pitot; schlieren; optical deflectometry; mach wave; correlation

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APA (6th Edition):

Veltin, J. (2008). On the Characterization of Noise Sources in Supersonic Shock Containing Jets. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/9068

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):

Veltin, Jeremy. “On the Characterization of Noise Sources in Supersonic Shock Containing Jets.” 2008. Thesis, Penn State University. Accessed August 14, 2020. https://submit-etda.libraries.psu.edu/catalog/9068.

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

MLA Handbook (7th Edition):

Veltin, Jeremy. “On the Characterization of Noise Sources in Supersonic Shock Containing Jets.” 2008. Web. 14 Aug 2020.

Vancouver:

Veltin J. On the Characterization of Noise Sources in Supersonic Shock Containing Jets. [Internet] [Thesis]. Penn State University; 2008. [cited 2020 Aug 14]. Available from: https://submit-etda.libraries.psu.edu/catalog/9068.

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

Council of Science Editors:

Veltin J. On the Characterization of Noise Sources in Supersonic Shock Containing Jets. [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/9068

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

21. David, Antoine. Étude des vibrations des réseaux de transport de gaz dans l'industrie de l'aluminium : Vibration study of gas transport ductwork in the aluminium industry.

Degree: Docteur es, Mécanique Avancée, 2016, Compiègne

Les gaines rectangulaires utilisées dans les réseaux de transport de gaz, notamment dans l'industrie de l'aluminium, sont soumises à des excitations provenant du flux s'écoulant… (more)

Subjects/Keywords: Gaine rectangulaire; Écoulement turbulent; Sources aéroacoustiques; Couche limite turbulente; Modélisation semi-analytique; Rectangular duct; Turbulent flow; Aeroacoustic sources; Turbulent boundary layer; Fluid mechanics

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APA (6th Edition):

David, A. (2016). Étude des vibrations des réseaux de transport de gaz dans l'industrie de l'aluminium : Vibration study of gas transport ductwork in the aluminium industry. (Doctoral Dissertation). Compiègne. Retrieved from http://www.theses.fr/2016COMP2277

Chicago Manual of Style (16th Edition):

David, Antoine. “Étude des vibrations des réseaux de transport de gaz dans l'industrie de l'aluminium : Vibration study of gas transport ductwork in the aluminium industry.” 2016. Doctoral Dissertation, Compiègne. Accessed August 14, 2020. http://www.theses.fr/2016COMP2277.

MLA Handbook (7th Edition):

David, Antoine. “Étude des vibrations des réseaux de transport de gaz dans l'industrie de l'aluminium : Vibration study of gas transport ductwork in the aluminium industry.” 2016. Web. 14 Aug 2020.

Vancouver:

David A. Étude des vibrations des réseaux de transport de gaz dans l'industrie de l'aluminium : Vibration study of gas transport ductwork in the aluminium industry. [Internet] [Doctoral dissertation]. Compiègne; 2016. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2016COMP2277.

Council of Science Editors:

David A. Étude des vibrations des réseaux de transport de gaz dans l'industrie de l'aluminium : Vibration study of gas transport ductwork in the aluminium industry. [Doctoral Dissertation]. Compiègne; 2016. Available from: http://www.theses.fr/2016COMP2277


Virginia Tech

22. Miller, Kevin C. Comparison of the aeroacoustics of two small-scale supersonic inlets.

Degree: MS, Mechanical Engineering, 1996, Virginia Tech

Subjects/Keywords: supersonic inlet; aeroacoustic; P inlet; bifurcated 2D inlet; LD5655.V855 1996.M555

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APA (6th Edition):

Miller, K. C. (1996). Comparison of the aeroacoustics of two small-scale supersonic inlets. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/45385

Chicago Manual of Style (16th Edition):

Miller, Kevin C. “Comparison of the aeroacoustics of two small-scale supersonic inlets.” 1996. Masters Thesis, Virginia Tech. Accessed August 14, 2020. http://hdl.handle.net/10919/45385.

MLA Handbook (7th Edition):

Miller, Kevin C. “Comparison of the aeroacoustics of two small-scale supersonic inlets.” 1996. Web. 14 Aug 2020.

Vancouver:

Miller KC. Comparison of the aeroacoustics of two small-scale supersonic inlets. [Internet] [Masters thesis]. Virginia Tech; 1996. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/10919/45385.

Council of Science Editors:

Miller KC. Comparison of the aeroacoustics of two small-scale supersonic inlets. [Masters Thesis]. Virginia Tech; 1996. Available from: http://hdl.handle.net/10919/45385


Virginia Tech

23. Mish, Patrick Francis. An Experimental Investigation of Unsteady Surface Pressure on Single and Multiple Airfoils.

Degree: PhD, Aerospace and Ocean Engineering, 2003, Virginia Tech

 This dissertation presents measurements of unsteady surface pressure on airfoils encountering flow disturbances. Analysis of measurements made on an airfoil immersed in turbulence and comparisons… (more)

Subjects/Keywords: aeroacoustic; unsteady loading; cascade response; airfoil in turbulence; inviscid response; unsteady surface pressure

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APA (6th Edition):

Mish, P. F. (2003). An Experimental Investigation of Unsteady Surface Pressure on Single and Multiple Airfoils. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26567

Chicago Manual of Style (16th Edition):

Mish, Patrick Francis. “An Experimental Investigation of Unsteady Surface Pressure on Single and Multiple Airfoils.” 2003. Doctoral Dissertation, Virginia Tech. Accessed August 14, 2020. http://hdl.handle.net/10919/26567.

MLA Handbook (7th Edition):

Mish, Patrick Francis. “An Experimental Investigation of Unsteady Surface Pressure on Single and Multiple Airfoils.” 2003. Web. 14 Aug 2020.

Vancouver:

Mish PF. An Experimental Investigation of Unsteady Surface Pressure on Single and Multiple Airfoils. [Internet] [Doctoral dissertation]. Virginia Tech; 2003. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/10919/26567.

Council of Science Editors:

Mish PF. An Experimental Investigation of Unsteady Surface Pressure on Single and Multiple Airfoils. [Doctoral Dissertation]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/26567


INP Toulouse

24. Ansaldi, Tobias. Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics : Stabilité d'un jet double flux et analyse de sensibilité sur la base d'un modèle adjoint en relation avec l'aeroacoustic.

Degree: Docteur es, Dynamique des fluides, 2016, INP Toulouse

La thèse est relative à la compréhension de la physique et au contrôle des émissions acoustiques dans les jets turbulents simples et double-flux. La génération… (more)

Subjects/Keywords: Analyse de sensibilité; Analyse de la stabilité; Analogy aéroacoustique; Bruit de jet; Quantification de l'incertitude; Sensitivity analysis; Stability analysis; Aeroacoustic analogy; Jet noise; Uncertainty Quantification

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APA (6th Edition):

Ansaldi, T. (2016). Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics : Stabilité d'un jet double flux et analyse de sensibilité sur la base d'un modèle adjoint en relation avec l'aeroacoustic. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2016INPT0081

Chicago Manual of Style (16th Edition):

Ansaldi, Tobias. “Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics : Stabilité d'un jet double flux et analyse de sensibilité sur la base d'un modèle adjoint en relation avec l'aeroacoustic.” 2016. Doctoral Dissertation, INP Toulouse. Accessed August 14, 2020. http://www.theses.fr/2016INPT0081.

MLA Handbook (7th Edition):

Ansaldi, Tobias. “Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics : Stabilité d'un jet double flux et analyse de sensibilité sur la base d'un modèle adjoint en relation avec l'aeroacoustic.” 2016. Web. 14 Aug 2020.

Vancouver:

Ansaldi T. Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics : Stabilité d'un jet double flux et analyse de sensibilité sur la base d'un modèle adjoint en relation avec l'aeroacoustic. [Internet] [Doctoral dissertation]. INP Toulouse; 2016. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2016INPT0081.

Council of Science Editors:

Ansaldi T. Compressible single and dual stream jet stability and adjoint-based sensitivity analysis in relationship with aeroacoustics : Stabilité d'un jet double flux et analyse de sensibilité sur la base d'un modèle adjoint en relation avec l'aeroacoustic. [Doctoral Dissertation]. INP Toulouse; 2016. Available from: http://www.theses.fr/2016INPT0081


University of Florida

25. WILLIAMS,MATTHEW D. Development of a MEMS Piezoelectric Microphone for Aeroacoustic Applications.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2011, University of Florida

 Passenger expectations for a quiet flight experience coupled with concern about long-term noise exposure of flight crews drive aircraft manufacturers to reduce cabin noise in… (more)

Subjects/Keywords: Aeroacoustics; Boundary conditions; Capacitance; Diaphragm; Electric potential; Frequency response; Microelectromechanical systems; Microphones; Modeling; Sensors; AEROACOUSTIC  – AIRCRAFT  – ALUMINUM  – MEMS  – MIC  – MICROFABRICATED  – MICROPHONE  – MICROSYSTEM  – PIEZOELECTRIC

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APA (6th Edition):

D, W. (2011). Development of a MEMS Piezoelectric Microphone for Aeroacoustic Applications. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0041968

Chicago Manual of Style (16th Edition):

D, WILLIAMS,MATTHEW. “Development of a MEMS Piezoelectric Microphone for Aeroacoustic Applications.” 2011. Doctoral Dissertation, University of Florida. Accessed August 14, 2020. https://ufdc.ufl.edu/UFE0041968.

MLA Handbook (7th Edition):

D, WILLIAMS,MATTHEW. “Development of a MEMS Piezoelectric Microphone for Aeroacoustic Applications.” 2011. Web. 14 Aug 2020.

Vancouver:

D W. Development of a MEMS Piezoelectric Microphone for Aeroacoustic Applications. [Internet] [Doctoral dissertation]. University of Florida; 2011. [cited 2020 Aug 14]. Available from: https://ufdc.ufl.edu/UFE0041968.

Council of Science Editors:

D W. Development of a MEMS Piezoelectric Microphone for Aeroacoustic Applications. [Doctoral Dissertation]. University of Florida; 2011. Available from: https://ufdc.ufl.edu/UFE0041968


University of Florida

26. Reagan, Tiffany N. MEMS on a Plane: A Flush-Mount MEMS Piezoelectric Microphone for Aircraft Fuselage Arrays.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2017, University of Florida

Subjects/Keywords: aeroacoustic; aln; flush-mount; mems; microphone; piezoelectric; through-silicon-vias

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APA (6th Edition):

Reagan, T. N. (2017). MEMS on a Plane: A Flush-Mount MEMS Piezoelectric Microphone for Aircraft Fuselage Arrays. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0050603

Chicago Manual of Style (16th Edition):

Reagan, Tiffany N. “MEMS on a Plane: A Flush-Mount MEMS Piezoelectric Microphone for Aircraft Fuselage Arrays.” 2017. Doctoral Dissertation, University of Florida. Accessed August 14, 2020. https://ufdc.ufl.edu/UFE0050603.

MLA Handbook (7th Edition):

Reagan, Tiffany N. “MEMS on a Plane: A Flush-Mount MEMS Piezoelectric Microphone for Aircraft Fuselage Arrays.” 2017. Web. 14 Aug 2020.

Vancouver:

Reagan TN. MEMS on a Plane: A Flush-Mount MEMS Piezoelectric Microphone for Aircraft Fuselage Arrays. [Internet] [Doctoral dissertation]. University of Florida; 2017. [cited 2020 Aug 14]. Available from: https://ufdc.ufl.edu/UFE0050603.

Council of Science Editors:

Reagan TN. MEMS on a Plane: A Flush-Mount MEMS Piezoelectric Microphone for Aircraft Fuselage Arrays. [Doctoral Dissertation]. University of Florida; 2017. Available from: https://ufdc.ufl.edu/UFE0050603

27. Bennaceur, Iannis. Etude numérique de la diffusion d'une onde acoustique par une couche de cisaillement turbulente à l'aide d'une simulation aux grandes échelles : Study of the scattering of an acoustic wave by a turbulent shear layer using large-eddy simulation.

Degree: Docteur es, Sciences de l'ingénieur. Mécanique et physique des fluides, 2017, Aix Marseille Université

Lors des mesures acoustiques dans les souffleries à veine ouverte, les ondes acoustiques émises par une maquette ou une source située dans la veine se… (more)

Subjects/Keywords: Aéro-Acoustique; Diffusion acoustique; Couche de cisaillement turbulente; Simulation numérique aux grandes échelles; Mesure en soufflerie à veine ouverte; Aeroacoustic; Acoustic scattering; Turbulent shear layer; Large-Eddy simulation; Open jet wind tunnel measurements

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APA (6th Edition):

Bennaceur, I. (2017). Etude numérique de la diffusion d'une onde acoustique par une couche de cisaillement turbulente à l'aide d'une simulation aux grandes échelles : Study of the scattering of an acoustic wave by a turbulent shear layer using large-eddy simulation. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2017AIXM0187

Chicago Manual of Style (16th Edition):

Bennaceur, Iannis. “Etude numérique de la diffusion d'une onde acoustique par une couche de cisaillement turbulente à l'aide d'une simulation aux grandes échelles : Study of the scattering of an acoustic wave by a turbulent shear layer using large-eddy simulation.” 2017. Doctoral Dissertation, Aix Marseille Université. Accessed August 14, 2020. http://www.theses.fr/2017AIXM0187.

MLA Handbook (7th Edition):

Bennaceur, Iannis. “Etude numérique de la diffusion d'une onde acoustique par une couche de cisaillement turbulente à l'aide d'une simulation aux grandes échelles : Study of the scattering of an acoustic wave by a turbulent shear layer using large-eddy simulation.” 2017. Web. 14 Aug 2020.

Vancouver:

Bennaceur I. Etude numérique de la diffusion d'une onde acoustique par une couche de cisaillement turbulente à l'aide d'une simulation aux grandes échelles : Study of the scattering of an acoustic wave by a turbulent shear layer using large-eddy simulation. [Internet] [Doctoral dissertation]. Aix Marseille Université 2017. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2017AIXM0187.

Council of Science Editors:

Bennaceur I. Etude numérique de la diffusion d'une onde acoustique par une couche de cisaillement turbulente à l'aide d'une simulation aux grandes échelles : Study of the scattering of an acoustic wave by a turbulent shear layer using large-eddy simulation. [Doctoral Dissertation]. Aix Marseille Université 2017. Available from: http://www.theses.fr/2017AIXM0187

28. Tachos, Nikolaos. Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα.

Degree: 2013, University of Patras; Πανεπιστήμιο Πατρών

The aim of this study is to represent the aerodynamic and aeroacoustic analysis of horizontal axis wind turbine (ΗAWT) rotors. The calculation of the flow… (more)

Subjects/Keywords: Αεροδυναμική ανάλυση ανεμοκινητήρων; Αεροακουστική ανάλυση ανεμοκινητήρων; Μέθοδος επιφανειακών στοιχείων; Υπολογιστική ρευστοδυναμική; Ανεμοκινητήρες οριζοντίου άξονα; Aerodynamic analysis of wind turbine; Aeroacoustic analysis of wind turbine; Panel method; CFD; Horizontal axis wind turbine

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

APA (6th Edition):

Tachos, N. (2013). Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα. (Thesis). University of Patras; Πανεπιστήμιο Πατρών. Retrieved from http://hdl.handle.net/10442/hedi/36309

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):

Tachos, Nikolaos. “Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα.” 2013. Thesis, University of Patras; Πανεπιστήμιο Πατρών. Accessed August 14, 2020. http://hdl.handle.net/10442/hedi/36309.

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

MLA Handbook (7th Edition):

Tachos, Nikolaos. “Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα.” 2013. Web. 14 Aug 2020.

Vancouver:

Tachos N. Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα. [Internet] [Thesis]. University of Patras; Πανεπιστήμιο Πατρών; 2013. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/10442/hedi/36309.

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

Council of Science Editors:

Tachos N. Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα. [Thesis]. University of Patras; Πανεπιστήμιο Πατρών; 2013. Available from: http://hdl.handle.net/10442/hedi/36309

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

29. Τάχος, Νικόλαος. Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα.

Degree: 2014, University of Patras

Αντικείμενο της εργασίας είναι η αεροδυναμική και αεροακουστική ανάλυση στροφείων ανεμοκινητήρων οριζοντίου άξονα (α-ο-α). Ο υπολογισμός του πεδίου ροής και των αεροδυναμικών συντελεστών του στροφείου… (more)

Subjects/Keywords: Αεροδυναμική ανάλυση ανεμοκινητήρων; Αεροακουστική ανάλυση ανεμοκινητήρων; Μέθοδος επιφανειακών στοιχείων; Υπολογιστική ρευστοδυναμική; Ανεμοκινητήρες οριζοντίου άξονα; 621.45; Aerodynamic analysis of wind turbine; Aeroacoustic analysis of wind turbine; Panel method; Computational fluid dynamics (CFD); Horizontal axis wind turbine

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

APA (6th Edition):

Τάχος, . (2014). Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα. (Doctoral Dissertation). University of Patras. Retrieved from http://hdl.handle.net/10889/7966

Chicago Manual of Style (16th Edition):

Τάχος, Νικόλαος. “Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα.” 2014. Doctoral Dissertation, University of Patras. Accessed August 14, 2020. http://hdl.handle.net/10889/7966.

MLA Handbook (7th Edition):

Τάχος, Νικόλαος. “Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα.” 2014. Web. 14 Aug 2020.

Vancouver:

Τάχος . Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα. [Internet] [Doctoral dissertation]. University of Patras; 2014. [cited 2020 Aug 14]. Available from: http://hdl.handle.net/10889/7966.

Council of Science Editors:

Τάχος . Αεροδυναμική και αεροακουστική ανάλυση ανεμοκινητήρων οριζοντίου άξονα. [Doctoral Dissertation]. University of Patras; 2014. Available from: http://hdl.handle.net/10889/7966

30. Chronopoulos, Dimitrios. Prediction of the vibroacoustic response of aerospace composite structures in a broadband frequency range : Dynamic behavior of rotating turboshaft engines : Control of effects of rubbing devices.

Degree: Docteur es, Dynamique des structures, 2012, Ecully, Ecole centrale de Lyon

 Pendant sa mission, un lanceur est soumis à des excitations large bande, sévères, aérodynamiques, de provenances diverses, qui peuvent mettre en danger la survivabilité de… (more)

Subjects/Keywords: Excitations large bande; Réponse vibroacoustique; Méthode des éléments finis ondulatoires (WFEM); Analyse statistique énergétique (SEA); Approche de SOAR; Launch vehicle; Aeroacoustic excitations; Wave Finite Element Method (WFEM); Statistical Energy Analysis (SEA); Second Order ARnoldi reduction approach (SOAR)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chronopoulos, D. (2012). Prediction of the vibroacoustic response of aerospace composite structures in a broadband frequency range : Dynamic behavior of rotating turboshaft engines : Control of effects of rubbing devices. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon. Retrieved from http://www.theses.fr/2012ECDL0052

Chicago Manual of Style (16th Edition):

Chronopoulos, Dimitrios. “Prediction of the vibroacoustic response of aerospace composite structures in a broadband frequency range : Dynamic behavior of rotating turboshaft engines : Control of effects of rubbing devices.” 2012. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed August 14, 2020. http://www.theses.fr/2012ECDL0052.

MLA Handbook (7th Edition):

Chronopoulos, Dimitrios. “Prediction of the vibroacoustic response of aerospace composite structures in a broadband frequency range : Dynamic behavior of rotating turboshaft engines : Control of effects of rubbing devices.” 2012. Web. 14 Aug 2020.

Vancouver:

Chronopoulos D. Prediction of the vibroacoustic response of aerospace composite structures in a broadband frequency range : Dynamic behavior of rotating turboshaft engines : Control of effects of rubbing devices. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2012. [cited 2020 Aug 14]. Available from: http://www.theses.fr/2012ECDL0052.

Council of Science Editors:

Chronopoulos D. Prediction of the vibroacoustic response of aerospace composite structures in a broadband frequency range : Dynamic behavior of rotating turboshaft engines : Control of effects of rubbing devices. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; 2012. Available from: http://www.theses.fr/2012ECDL0052

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