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You searched for subject:(Propeller noise). Showing records 1 – 18 of 18 total matches.

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Delft University of Technology

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

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 15, 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. 15 Aug 2020.

Vancouver:

Haddaoui M(. Development of a Propeller Source Noise Model. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Aug 15]. 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


Delft University of Technology

2. 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 August 15, 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. 15 Aug 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 Aug 15]. 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


Penn State University

3. Zolbayar, Bolor Erdene. Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers.

Degree: 2018, Penn State University

 This thesis focuses on propeller noise considerations that would be appropriate for a 6-9 passenger low-tip-speed, electric propeller-driven aircraft. A baseline aircraft and propeller are… (more)

Subjects/Keywords: propeller noise; low-tip-speed propeller noise; unsteady loading; electric low-tip-speed propeller noise

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APA (6th Edition):

Zolbayar, B. E. (2018). Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15741bzz5065

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):

Zolbayar, Bolor Erdene. “Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers.” 2018. Thesis, Penn State University. Accessed August 15, 2020. https://submit-etda.libraries.psu.edu/catalog/15741bzz5065.

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

MLA Handbook (7th Edition):

Zolbayar, Bolor Erdene. “Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers.” 2018. Web. 15 Aug 2020.

Vancouver:

Zolbayar BE. Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers. [Internet] [Thesis]. Penn State University; 2018. [cited 2020 Aug 15]. Available from: https://submit-etda.libraries.psu.edu/catalog/15741bzz5065.

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

Council of Science Editors:

Zolbayar BE. Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/15741bzz5065

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

4. Sjöberg, Jacob. Low-Noise Propeller Design for Future Electric Aircraft .

Degree: Chalmers tekniska högskola / Institutionen för mekanik och maritima vetenskaper, 2020, Chalmers University of Technology

 Right now electric aircraft are being developed as an alternative to make the aviation industry more sustainable. The electric airplanes available today are using propellers… (more)

Subjects/Keywords: low-noise propeller; electric aircraft; propeller design; acoustic studies

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APA (6th Edition):

Sjöberg, J. (2020). Low-Noise Propeller Design for Future Electric Aircraft . (Thesis). Chalmers University of Technology. Retrieved from http://hdl.handle.net/20.500.12380/300830

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):

Sjöberg, Jacob. “Low-Noise Propeller Design for Future Electric Aircraft .” 2020. Thesis, Chalmers University of Technology. Accessed August 15, 2020. http://hdl.handle.net/20.500.12380/300830.

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

MLA Handbook (7th Edition):

Sjöberg, Jacob. “Low-Noise Propeller Design for Future Electric Aircraft .” 2020. Web. 15 Aug 2020.

Vancouver:

Sjöberg J. Low-Noise Propeller Design for Future Electric Aircraft . [Internet] [Thesis]. Chalmers University of Technology; 2020. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/20.500.12380/300830.

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

Council of Science Editors:

Sjöberg J. Low-Noise Propeller Design for Future Electric Aircraft . [Thesis]. Chalmers University of Technology; 2020. Available from: http://hdl.handle.net/20.500.12380/300830

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

5. Barros, Alexandre Bernardes de. Análise de desempenho e ruído de hélices de mínima perda de energia.

Degree: Mestrado, Aeronaves, 2009, University of São Paulo

Revisa os métodos para cálculo de desempenho e ruído de hélices. Apresenta um método para determinação de desempenho de hélices com mínima perda de energia… (more)

Subjects/Keywords: Desempenho; Hélice; Noise; Performance; Propeller; Ruído

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APA (6th Edition):

Barros, A. B. d. (2009). Análise de desempenho e ruído de hélices de mínima perda de energia. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-130409/ ;

Chicago Manual of Style (16th Edition):

Barros, Alexandre Bernardes de. “Análise de desempenho e ruído de hélices de mínima perda de energia.” 2009. Masters Thesis, University of São Paulo. Accessed August 15, 2020. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-130409/ ;.

MLA Handbook (7th Edition):

Barros, Alexandre Bernardes de. “Análise de desempenho e ruído de hélices de mínima perda de energia.” 2009. Web. 15 Aug 2020.

Vancouver:

Barros ABd. Análise de desempenho e ruído de hélices de mínima perda de energia. [Internet] [Masters thesis]. University of São Paulo; 2009. [cited 2020 Aug 15]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-130409/ ;.

Council of Science Editors:

Barros ABd. Análise de desempenho e ruído de hélices de mínima perda de energia. [Masters Thesis]. University of São Paulo; 2009. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-130409/ ;


University of Adelaide

6. Blunt, David Mark. Optimisation and adaptive control of aircraft propeller synchrophase angles.

Degree: 2012, University of Adelaide

 This thesis provides a new and detailed examination of how the optimum propeller synchrophase angles for minimum cabin noise and vibration vary with different flight… (more)

Subjects/Keywords: aircraft; propeller; noise; vibration; active control; synchrophasing

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APA (6th Edition):

Blunt, D. M. (2012). Optimisation and adaptive control of aircraft propeller synchrophase angles. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/75757

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):

Blunt, David Mark. “Optimisation and adaptive control of aircraft propeller synchrophase angles.” 2012. Thesis, University of Adelaide. Accessed August 15, 2020. http://hdl.handle.net/2440/75757.

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

MLA Handbook (7th Edition):

Blunt, David Mark. “Optimisation and adaptive control of aircraft propeller synchrophase angles.” 2012. Web. 15 Aug 2020.

Vancouver:

Blunt DM. Optimisation and adaptive control of aircraft propeller synchrophase angles. [Internet] [Thesis]. University of Adelaide; 2012. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/2440/75757.

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

Council of Science Editors:

Blunt DM. Optimisation and adaptive control of aircraft propeller synchrophase angles. [Thesis]. University of Adelaide; 2012. Available from: http://hdl.handle.net/2440/75757

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


University of Manchester

7. Nigro, David. Prediction of broadband aero and hydrodynamic noise: derivation of analytical models for low frequency.

Degree: 2017, University of Manchester

 In this thesis we explore several topics with applications to both aero and hydroacoustics. Due to the much larger speed of sound in water compared… (more)

Subjects/Keywords: aeroacoustics; hydroacoustics; wave scattering; propeller noise; trailing edge noise; ingested noise

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APA (6th Edition):

Nigro, D. (2017). Prediction of broadband aero and hydrodynamic noise: derivation of analytical models for low frequency. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307176

Chicago Manual of Style (16th Edition):

Nigro, David. “Prediction of broadband aero and hydrodynamic noise: derivation of analytical models for low frequency.” 2017. Doctoral Dissertation, University of Manchester. Accessed August 15, 2020. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307176.

MLA Handbook (7th Edition):

Nigro, David. “Prediction of broadband aero and hydrodynamic noise: derivation of analytical models for low frequency.” 2017. Web. 15 Aug 2020.

Vancouver:

Nigro D. Prediction of broadband aero and hydrodynamic noise: derivation of analytical models for low frequency. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2020 Aug 15]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307176.

Council of Science Editors:

Nigro D. Prediction of broadband aero and hydrodynamic noise: derivation of analytical models for low frequency. [Doctoral Dissertation]. University of Manchester; 2017. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:307176


University of Manchester

8. Nigro, David. Prediction of broadband aero and hydrodynamic noise : derivation of analytical models for low frequency.

Degree: PhD, 2017, University of Manchester

 In this thesis we explore several topics with applications to both aero and hydroacoustics. Due to the much larger speed of sound in water compared… (more)

Subjects/Keywords: 534; aeroacoustics; wave scattering; propeller noise; trailing edge noise; ingested noise; hydroacoustics

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APA (6th Edition):

Nigro, D. (2017). Prediction of broadband aero and hydrodynamic noise : derivation of analytical models for low frequency. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/prediction-of-broadband-aero-and-hydrodynamic-noise-derivation-of-analytical-models-for-low-frequency(25bb8835-9cf8-488a-acc0-677a53122801).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727963

Chicago Manual of Style (16th Edition):

Nigro, David. “Prediction of broadband aero and hydrodynamic noise : derivation of analytical models for low frequency.” 2017. Doctoral Dissertation, University of Manchester. Accessed August 15, 2020. https://www.research.manchester.ac.uk/portal/en/theses/prediction-of-broadband-aero-and-hydrodynamic-noise-derivation-of-analytical-models-for-low-frequency(25bb8835-9cf8-488a-acc0-677a53122801).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727963.

MLA Handbook (7th Edition):

Nigro, David. “Prediction of broadband aero and hydrodynamic noise : derivation of analytical models for low frequency.” 2017. Web. 15 Aug 2020.

Vancouver:

Nigro D. Prediction of broadband aero and hydrodynamic noise : derivation of analytical models for low frequency. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2020 Aug 15]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/prediction-of-broadband-aero-and-hydrodynamic-noise-derivation-of-analytical-models-for-low-frequency(25bb8835-9cf8-488a-acc0-677a53122801).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727963.

Council of Science Editors:

Nigro D. Prediction of broadband aero and hydrodynamic noise : derivation of analytical models for low frequency. [Doctoral Dissertation]. University of Manchester; 2017. Available from: https://www.research.manchester.ac.uk/portal/en/theses/prediction-of-broadband-aero-and-hydrodynamic-noise-derivation-of-analytical-models-for-low-frequency(25bb8835-9cf8-488a-acc0-677a53122801).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727963


Delft University of Technology

9. van Mourik Broekman, Jeremy (author). Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model.

Degree: 2017, Delft University of Technology

The high efficiency of open rotor propulsion has led to a comeback of propeller propulsion systems in recent years. The main issue preventing wide application… (more)

Subjects/Keywords: vortex-surface interaction; experimental; Conceptual modelling; m-tunnel; aerodynamics; propeller noise

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APA (6th Edition):

van Mourik Broekman, J. (. (2017). Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03

Chicago Manual of Style (16th Edition):

van Mourik Broekman, Jeremy (author). “Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model.” 2017. Masters Thesis, Delft University of Technology. Accessed August 15, 2020. http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03.

MLA Handbook (7th Edition):

van Mourik Broekman, Jeremy (author). “Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model.” 2017. Web. 15 Aug 2020.

Vancouver:

van Mourik Broekman J(. Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Aug 15]. Available from: http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03.

Council of Science Editors:

van Mourik Broekman J(. Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03


KTH

10. Sjöö, Filip. Development of concept for silent UAV propulsion.

Degree: Machine Design (Dept.), 2018, KTH

Eftersom användningen av små UAV:s (Unmanned Aerial Vehicles) fortsätter att öka, harbullret från deras framdrivningssystem blivit ett ökande problem. Denna rapport är resultatetav ett… (more)

Subjects/Keywords: UAV; circulation control; propeller; boundary layer separation; noise reduction; multirotor; gränsskikt; avlösning; ljudreduktion; propeller; Mechanical Engineering; Maskinteknik

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APA (6th Edition):

Sjöö, F. (2018). Development of concept for silent UAV propulsion. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232450

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):

Sjöö, Filip. “Development of concept for silent UAV propulsion.” 2018. Thesis, KTH. Accessed August 15, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232450.

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

MLA Handbook (7th Edition):

Sjöö, Filip. “Development of concept for silent UAV propulsion.” 2018. Web. 15 Aug 2020.

Vancouver:

Sjöö F. Development of concept for silent UAV propulsion. [Internet] [Thesis]. KTH; 2018. [cited 2020 Aug 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232450.

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

Council of Science Editors:

Sjöö F. Development of concept for silent UAV propulsion. [Thesis]. KTH; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232450

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

11. Andersson, Magnus. Analysis of noise levels, audio frequency and fuel consumption with propellers of type McCauley and MT on BAe Jetstream 32.

Degree: Design and Engineering, 2012, Mälardalen University

This report describes a thesis project conducted at Direktflyg in Borlänge, in early 2012, where the aim was to analyse the difference in noise(more)

Subjects/Keywords: aeronautical; aerospace; engineering; propeller; jetstream; direktflyg; british aerospace; MT; McCauley; frequency; noise levels; noise; fuel consumption; flyg; flygteknik; propeller; McCauley; MT; jetstream; Direktflyg; ljudnivå; frekvens; ljudfrekvens; bränsleförbrukning; BAe; british aerospace

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

APA (6th Edition):

Andersson, M. (2012). Analysis of noise levels, audio frequency and fuel consumption with propellers of type McCauley and MT on BAe Jetstream 32. (Thesis). Mälardalen University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-14446

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):

Andersson, Magnus. “Analysis of noise levels, audio frequency and fuel consumption with propellers of type McCauley and MT on BAe Jetstream 32.” 2012. Thesis, Mälardalen University. Accessed August 15, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-14446.

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

MLA Handbook (7th Edition):

Andersson, Magnus. “Analysis of noise levels, audio frequency and fuel consumption with propellers of type McCauley and MT on BAe Jetstream 32.” 2012. Web. 15 Aug 2020.

Vancouver:

Andersson M. Analysis of noise levels, audio frequency and fuel consumption with propellers of type McCauley and MT on BAe Jetstream 32. [Internet] [Thesis]. Mälardalen University; 2012. [cited 2020 Aug 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-14446.

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

Council of Science Editors:

Andersson M. Analysis of noise levels, audio frequency and fuel consumption with propellers of type McCauley and MT on BAe Jetstream 32. [Thesis]. Mälardalen University; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-14446

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


Delft University of Technology

12. Klein, Peter (author). Parametric Modeling and Optimization of Advanced Propellers for Next-Generation Aircraft.

Degree: 2017, Delft University of Technology

As traditional fossil fuels become scarcer and more attention is given to environmental impact of the combustion of fossil fuels, for next-generation aircraft, the focus… (more)

Subjects/Keywords: Propeller; CFD; Installed pusher configuration; Optimization; Parametric design tool; Noise; Pylon wake

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APA (6th Edition):

Klein, P. (. (2017). Parametric Modeling and Optimization of Advanced Propellers for Next-Generation Aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4e54cfb3-3024-420a-8205-48c7eb767ce9

Chicago Manual of Style (16th Edition):

Klein, Peter (author). “Parametric Modeling and Optimization of Advanced Propellers for Next-Generation Aircraft.” 2017. Masters Thesis, Delft University of Technology. Accessed August 15, 2020. http://resolver.tudelft.nl/uuid:4e54cfb3-3024-420a-8205-48c7eb767ce9.

MLA Handbook (7th Edition):

Klein, Peter (author). “Parametric Modeling and Optimization of Advanced Propellers for Next-Generation Aircraft.” 2017. Web. 15 Aug 2020.

Vancouver:

Klein P(. Parametric Modeling and Optimization of Advanced Propellers for Next-Generation Aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Aug 15]. Available from: http://resolver.tudelft.nl/uuid:4e54cfb3-3024-420a-8205-48c7eb767ce9.

Council of Science Editors:

Klein P(. Parametric Modeling and Optimization of Advanced Propellers for Next-Generation Aircraft. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:4e54cfb3-3024-420a-8205-48c7eb767ce9


Georgia Tech

13. Turkdogru, Nurkan. Validity of the point source assumption of a rotor for farfield acoustic measurements with and without shielding.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 Measuring the farfield noise levels of full-scale rotor systems is not trivial and can be costly. Researchers prefer to perform small-scale experiments in the laboratory… (more)

Subjects/Keywords: Propeller noise; Shielding; Geometric far field; Aeroacoustics; Ducted rotor noise; Noise Measurement; Noise control

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APA (6th Edition):

Turkdogru, N. (2010). Validity of the point source assumption of a rotor for farfield acoustic measurements with and without shielding. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/37226

Chicago Manual of Style (16th Edition):

Turkdogru, Nurkan. “Validity of the point source assumption of a rotor for farfield acoustic measurements with and without shielding.” 2010. Doctoral Dissertation, Georgia Tech. Accessed August 15, 2020. http://hdl.handle.net/1853/37226.

MLA Handbook (7th Edition):

Turkdogru, Nurkan. “Validity of the point source assumption of a rotor for farfield acoustic measurements with and without shielding.” 2010. Web. 15 Aug 2020.

Vancouver:

Turkdogru N. Validity of the point source assumption of a rotor for farfield acoustic measurements with and without shielding. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/1853/37226.

Council of Science Editors:

Turkdogru N. Validity of the point source assumption of a rotor for farfield acoustic measurements with and without shielding. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/37226

14. Liller, William R. The design of small propellers operating at low Reynolds numbers and associated experimental evaluation.

Degree: M.S.M.E., Baylor University. School of Engineering., 2015, Baylor University

 Small-scale Unmanned Aerial Systems (UASs) are becoming increasingly important in the field of intelligence, surveillance, and reconnaissance. As the desire for higher payloads and longer… (more)

Subjects/Keywords: Small propellers. Low Reynolds numbers. UAS propulsion. UAV propulsion. Small propeller design. Small propeller testing. Small propeller noise.

…173 Figure 5.95: APC 9x6/TPXa/TPXc In-Tunnel Propeller Noise Comparison, T = 0.5 lbf, V = 44… …173 Figure 5.96: APC 9x6/TPXa/TPXc Tunnel Inlet Propeller Noise Comparison, T = 0.5 lbf, V… …propeller efficiency and reducing noise signature. 7 Increasing Efficiency and Reducing Noise… …6 Figure 2.1: NACA 16 Series Propeller Efficiencies vs. Reynolds Number [9]… …Surface Oil Flow Features [13] ......................14 Figure 2.8: UIUC Propeller… 

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

APA (6th Edition):

Liller, W. R. (2015). The design of small propellers operating at low Reynolds numbers and associated experimental evaluation. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9502

Chicago Manual of Style (16th Edition):

Liller, William R. “The design of small propellers operating at low Reynolds numbers and associated experimental evaluation.” 2015. Masters Thesis, Baylor University. Accessed August 15, 2020. http://hdl.handle.net/2104/9502.

MLA Handbook (7th Edition):

Liller, William R. “The design of small propellers operating at low Reynolds numbers and associated experimental evaluation.” 2015. Web. 15 Aug 2020.

Vancouver:

Liller WR. The design of small propellers operating at low Reynolds numbers and associated experimental evaluation. [Internet] [Masters thesis]. Baylor University; 2015. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/2104/9502.

Council of Science Editors:

Liller WR. The design of small propellers operating at low Reynolds numbers and associated experimental evaluation. [Masters Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9502


Brno University of Technology

15. Dofek, Ivan. Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization.

Degree: 2019, Brno University of Technology

 The work deals with the use of geometric parameterization for shape description of some parts of the airplane. Geometric parametrization is used for creating a… (more)

Subjects/Keywords: parametrizace; evoluční algoritmus; geometrická parametrizace; optimalizace; hluk vrtule; letecký profil; Ffowcs Williams–Hawkings; polynomická paremtetrizace; řízená distribuce paremetrů; aerodynamická optimalizace vrtule; evolutionary algorithm; parametrization; geometric parametrization; optimization; propeller noise; airfoil; Ffowcs Williams–Hawkings; direct parameters distribution; propeller aerodynamics optimization

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

APA (6th Edition):

Dofek, I. (2019). Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/36292

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):

Dofek, Ivan. “Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization.” 2019. Thesis, Brno University of Technology. Accessed August 15, 2020. http://hdl.handle.net/11012/36292.

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

MLA Handbook (7th Edition):

Dofek, Ivan. “Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization.” 2019. Web. 15 Aug 2020.

Vancouver:

Dofek I. Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/11012/36292.

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

Council of Science Editors:

Dofek I. Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/36292

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


Virginia Tech

16. Murray IV, Henry Hall. Turbulence and Sound Generated by a Rotor Operating Near a Wall.

Degree: MS, Aerospace and Ocean Engineering, 2016, Virginia Tech

 Acoustic and aerodynamic measurements have been carried out on a rotor operating in a planar turbulent boundary layer near a wall for a variety of… (more)

Subjects/Keywords: Rotor; Acoustics; Boundary Layer; Tip Gap; Turbulence Ingestion Noise; Particle Image Velocimetry; Phase Averaged; Experimental; Wind Tunnel; Microphone; Wall Pressure; Blade Vortex Interaction; Propeller-Hull Vortex; Pirouette Vortex

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

APA (6th Edition):

Murray IV, H. H. (2016). Turbulence and Sound Generated by a Rotor Operating Near a Wall. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71332

Chicago Manual of Style (16th Edition):

Murray IV, Henry Hall. “Turbulence and Sound Generated by a Rotor Operating Near a Wall.” 2016. Masters Thesis, Virginia Tech. Accessed August 15, 2020. http://hdl.handle.net/10919/71332.

MLA Handbook (7th Edition):

Murray IV, Henry Hall. “Turbulence and Sound Generated by a Rotor Operating Near a Wall.” 2016. Web. 15 Aug 2020.

Vancouver:

Murray IV HH. Turbulence and Sound Generated by a Rotor Operating Near a Wall. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/10919/71332.

Council of Science Editors:

Murray IV HH. Turbulence and Sound Generated by a Rotor Operating Near a Wall. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/71332


Delft University of Technology

17. De Vries, R. (author). Unsteady Pylon Loading for Pylon-Mounted Tractor Propellers.

Degree: 2016, Delft University of Technology

Aerospace Engineering

Flight Performance and Propulsion

Advisors/Committee Members: Sinnige, T. (mentor).

Subjects/Keywords: Propeller; Pylon; Structure-Borne Noise; Wind Tunnel; Experimental; Aerodynamics; Aeroacoustics; Interaction; Unsteady Pressure; Unsteady Loading

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

APA (6th Edition):

De Vries, R. (. (2016). Unsteady Pylon Loading for Pylon-Mounted Tractor Propellers. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c0f10961-0ac5-4f58-869b-fe04b7cd22a5

Chicago Manual of Style (16th Edition):

De Vries, R (author). “Unsteady Pylon Loading for Pylon-Mounted Tractor Propellers.” 2016. Masters Thesis, Delft University of Technology. Accessed August 15, 2020. http://resolver.tudelft.nl/uuid:c0f10961-0ac5-4f58-869b-fe04b7cd22a5.

MLA Handbook (7th Edition):

De Vries, R (author). “Unsteady Pylon Loading for Pylon-Mounted Tractor Propellers.” 2016. Web. 15 Aug 2020.

Vancouver:

De Vries R(. Unsteady Pylon Loading for Pylon-Mounted Tractor Propellers. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Aug 15]. Available from: http://resolver.tudelft.nl/uuid:c0f10961-0ac5-4f58-869b-fe04b7cd22a5.

Council of Science Editors:

De Vries R(. Unsteady Pylon Loading for Pylon-Mounted Tractor Propellers. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:c0f10961-0ac5-4f58-869b-fe04b7cd22a5

18. Rao, Arjun. Measurement of aerodynamic characteristics of MAVs using motion tracking.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 Aerodynamic characteristics of Micro Air Vehicles (MAVs) is not well addressed in aeronautics literature, and more experimental data are required to help better understand the… (more)

Subjects/Keywords: Micro air vehicle (MAV); Reynolds number; remote controlled (RC); aircraft; airplane; model; Lift; drag; thrust; moment; stability; control; pitch; roll; yaw; weathercock; weathervane; motion tracking; motion capture; VICON; camera; wand; Re; lift curve; drag polar; propeller; Advanced Precision Composites (APC); sport; E-flite; sideslip; static margin (SM); axis; axes; PropellerScanner; airfoil; wing; lifting line theory; theory; experimental; Aerodynamics; calibration; noise; markers; camera; Euler angles; longitudinal; lateral; advance ratio; density; data points; Extra 260; Extra 300 3D; glider; frequency; revolutions per minute (RPM); body-fixed; Earth-fixed; transformation; rotation; matrix; filter; low-pass; finite difference; robust; lineqar; least-squares; parabolic; Uhlig; Selig; Rao

…The Vicon markers built into separate objects with the propeller, the aircraft, and the two… …propeller. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Geometric characteristics… …of APC 9×5 propeller… …Experimentally determined thrust characteristics of the APC 9×5 propeller… …Experimentally measured propeller speed for various flights… 

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

APA (6th Edition):

Rao, A. (2012). Measurement of aerodynamic characteristics of MAVs using motion tracking. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/30943

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):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed August 15, 2020. http://hdl.handle.net/2142/30943.

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

MLA Handbook (7th Edition):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Web. 15 Aug 2020.

Vancouver:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2020 Aug 15]. Available from: http://hdl.handle.net/2142/30943.

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

Council of Science Editors:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/30943

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

.