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You searched for subject:(propeller). Showing records 1 – 30 of 164 total matches.

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Delft University of Technology

1. Sinnige, T. 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. “The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:.” 2013. Masters Thesis, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:a70b25ef-f780-41f7-afa0-9fb3f5e8e992.

MLA Handbook (7th Edition):

Sinnige, T. “The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:.” 2013. Web. 22 Nov 2019.

Vancouver:

Sinnige T. The Effects of Pylon Blowing on Pusher Propeller Performance and Noise Emissions:. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2019 Nov 22]. 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


University of Texas – Austin

2. -7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.

Degree: PhD, Civil Engineering, 2018, University of Texas – Austin

 The goal of this research is to reduce the computational cost of a fully unsteady RANS simulation for the multibody interaction problems in the ship… (more)

Subjects/Keywords: Propeller hydrodynamics; BEM/RANS; Hull propeller interaction

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APA (6th Edition):

-7364-0506. (2018). Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68081

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-7364-0506. “Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed November 22, 2019. http://hdl.handle.net/2152/68081.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-7364-0506. “Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.” 2018. Web. 22 Nov 2019.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/2152/68081.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/68081

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


University of Cincinnati

3. Nichols, Schuyler R. Experimental Approach to the Feasibility of an Axially-Stacked Propeller System.

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

 The aerospace industry is experiencing an ever increasing demand for cheaper, quieter, and more efficient propulsion systems. This demand has placed much pressure on engineers… (more)

Subjects/Keywords: Aerospace Materials; Propeller

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APA (6th Edition):

Nichols, S. R. (2014). Experimental Approach to the Feasibility of an Axially-Stacked Propeller System. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1415626159

Chicago Manual of Style (16th Edition):

Nichols, Schuyler R. “Experimental Approach to the Feasibility of an Axially-Stacked Propeller System.” 2014. Masters Thesis, University of Cincinnati. Accessed November 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1415626159.

MLA Handbook (7th Edition):

Nichols, Schuyler R. “Experimental Approach to the Feasibility of an Axially-Stacked Propeller System.” 2014. Web. 22 Nov 2019.

Vancouver:

Nichols SR. Experimental Approach to the Feasibility of an Axially-Stacked Propeller System. [Internet] [Masters thesis]. University of Cincinnati; 2014. [cited 2019 Nov 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1415626159.

Council of Science Editors:

Nichols SR. Experimental Approach to the Feasibility of an Axially-Stacked Propeller System. [Masters Thesis]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1415626159


Delft University of Technology

4. Channa, V.V. Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:.

Degree: 2015, Delft University of Technology

 Open rotors are considered to have the potential to improve the fuel economy of aircraft significantly by improving the propulsive efficiency compared to the current… (more)

Subjects/Keywords: propeller; performance; acoustics

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APA (6th Edition):

Channa, V. V. (2015). Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5

Chicago Manual of Style (16th Edition):

Channa, V V. “Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5.

MLA Handbook (7th Edition):

Channa, V V. “Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:.” 2015. Web. 22 Nov 2019.

Vancouver:

Channa VV. Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 22]. Available from: http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5.

Council of Science Editors:

Channa VV. Sensitivity of Pusher Propeller Performance and Noise Emissions to the UpstreamWake Characteristics: An Experimental and Numerical Study:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e32f84f1-21da-4a5a-a541-2f15b041ede5


Delft University of Technology

5. Zhou, T. Orthogonal Vortex-Propeller Interaction: Vortex Response and Impact on the Propeller Performance:.

Degree: 2015, Delft University of Technology

 In some situations, concentrated vorticity which forms a vortical flow is involved in the inflow of a propeller. The impingement of the vortex on the… (more)

Subjects/Keywords: vortex; propeller; interaction

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APA (6th Edition):

Zhou, T. (2015). Orthogonal Vortex-Propeller Interaction: Vortex Response and Impact on the Propeller Performance:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8c8b0678-519d-4480-825d-69d215ae48c3

Chicago Manual of Style (16th Edition):

Zhou, T. “Orthogonal Vortex-Propeller Interaction: Vortex Response and Impact on the Propeller Performance:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:8c8b0678-519d-4480-825d-69d215ae48c3.

MLA Handbook (7th Edition):

Zhou, T. “Orthogonal Vortex-Propeller Interaction: Vortex Response and Impact on the Propeller Performance:.” 2015. Web. 22 Nov 2019.

Vancouver:

Zhou T. Orthogonal Vortex-Propeller Interaction: Vortex Response and Impact on the Propeller Performance:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 22]. Available from: http://resolver.tudelft.nl/uuid:8c8b0678-519d-4480-825d-69d215ae48c3.

Council of Science Editors:

Zhou T. Orthogonal Vortex-Propeller Interaction: Vortex Response and Impact on the Propeller Performance:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:8c8b0678-519d-4480-825d-69d215ae48c3


Penn State University

6. Zolbayar, Bolor. 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 a6-9 passenger low-tip-speed, electric propeller-driven aircraft. A baseline aircraft andpropeller are used for… (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. (2018). Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers. (Thesis). Penn State University. Retrieved from https://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. “Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers.” 2018. Thesis, Penn State University. Accessed November 22, 2019. https://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. “Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers.” 2018. Web. 22 Nov 2019.

Vancouver:

Zolbayar B. Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers. [Internet] [Thesis]. Penn State University; 2018. [cited 2019 Nov 22]. Available from: https://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 B. Investigation Noise from Electric, Low-Tip-Speed Aircraft Propellers. [Thesis]. Penn State University; 2018. Available from: https://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


Delft University of Technology

7. Pouw, C.P. Development of a multiobjective design optimization procedure for marine propellers:.

Degree: Mechanical Maritime and Materials Engineering, Marine and Transport Technology, 2008, Delft University of Technology

 The design of a marine propeller is characterized by its complexity rather then its shortcoming of knowledge how to asses its performance. There are several… (more)

Subjects/Keywords: marine; propeller; design; multiobjective; optimisation

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APA (6th Edition):

Pouw, C. P. (2008). Development of a multiobjective design optimization procedure for marine propellers:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:95d6e4fd-dd15-440f-8640-07dadd1aca48

Chicago Manual of Style (16th Edition):

Pouw, C P. “Development of a multiobjective design optimization procedure for marine propellers:.” 2008. Masters Thesis, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:95d6e4fd-dd15-440f-8640-07dadd1aca48.

MLA Handbook (7th Edition):

Pouw, C P. “Development of a multiobjective design optimization procedure for marine propellers:.” 2008. Web. 22 Nov 2019.

Vancouver:

Pouw CP. Development of a multiobjective design optimization procedure for marine propellers:. [Internet] [Masters thesis]. Delft University of Technology; 2008. [cited 2019 Nov 22]. Available from: http://resolver.tudelft.nl/uuid:95d6e4fd-dd15-440f-8640-07dadd1aca48.

Council of Science Editors:

Pouw CP. Development of a multiobjective design optimization procedure for marine propellers:. [Masters Thesis]. Delft University of Technology; 2008. Available from: http://resolver.tudelft.nl/uuid:95d6e4fd-dd15-440f-8640-07dadd1aca48


Delft University of Technology

8. Huisman, T.J. Optimization of Ice-Class Propellers:.

Degree: 2015, Delft University of Technology

 The main objective of this Master’s thesis is to develop an optimization routine to improve ice-class propeller design methodology using the design space within the… (more)

Subjects/Keywords: ice; propeller; optimization; genetic; class

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APA (6th Edition):

Huisman, T. J. (2015). Optimization of Ice-Class Propellers:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0607236e-c6d1-41a7-873b-c487065cea34

Chicago Manual of Style (16th Edition):

Huisman, T J. “Optimization of Ice-Class Propellers:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:0607236e-c6d1-41a7-873b-c487065cea34.

MLA Handbook (7th Edition):

Huisman, T J. “Optimization of Ice-Class Propellers:.” 2015. Web. 22 Nov 2019.

Vancouver:

Huisman TJ. Optimization of Ice-Class Propellers:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 22]. Available from: http://resolver.tudelft.nl/uuid:0607236e-c6d1-41a7-873b-c487065cea34.

Council of Science Editors:

Huisman TJ. Optimization of Ice-Class Propellers:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:0607236e-c6d1-41a7-873b-c487065cea34


Oklahoma State University

9. Bettinger, Ben Thomas. Manufacturing, Analysis, and Experimental Testing of Multi-bladed Propellers for SUAS.

Degree: Mechanical & Aerospace Engineering, 2012, Oklahoma State University

 The emergence of small UAS with infinite applications has increased the demand for improved small aircraft components. For custom built UAS, optimized propellers are rarely… (more)

Subjects/Keywords: composites; manufacturing; propeller; uas

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APA (6th Edition):

Bettinger, B. T. (2012). Manufacturing, Analysis, and Experimental Testing of Multi-bladed Propellers for SUAS. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/9895

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):

Bettinger, Ben Thomas. “Manufacturing, Analysis, and Experimental Testing of Multi-bladed Propellers for SUAS.” 2012. Thesis, Oklahoma State University. Accessed November 22, 2019. http://hdl.handle.net/11244/9895.

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

MLA Handbook (7th Edition):

Bettinger, Ben Thomas. “Manufacturing, Analysis, and Experimental Testing of Multi-bladed Propellers for SUAS.” 2012. Web. 22 Nov 2019.

Vancouver:

Bettinger BT. Manufacturing, Analysis, and Experimental Testing of Multi-bladed Propellers for SUAS. [Internet] [Thesis]. Oklahoma State University; 2012. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/11244/9895.

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

Council of Science Editors:

Bettinger BT. Manufacturing, Analysis, and Experimental Testing of Multi-bladed Propellers for SUAS. [Thesis]. Oklahoma State University; 2012. Available from: http://hdl.handle.net/11244/9895

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

10. Duvall, Brian Edward. Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design.

Degree: MS, Aerospace Engineering, 2016, Old Dominion University

  Interest in small unmanned aerial vehicles has increased dramatically in recent years. Hybrid vehicles which allow forward flight as a fixed wing aircraft and… (more)

Subjects/Keywords: Acoustic; Performance; Propeller; Aerospace Engineering

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APA (6th Edition):

Duvall, B. E. (2016). Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design. (Thesis). Old Dominion University. Retrieved from 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12

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):

Duvall, Brian Edward. “Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12.

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

MLA Handbook (7th Edition):

Duvall, Brian Edward. “Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design.” 2016. Web. 22 Nov 2019.

Vancouver:

Duvall BE. Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12.

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

Council of Science Editors:

Duvall BE. Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design. [Thesis]. Old Dominion University; 2016. Available from: 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12

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


Utah State University

11. Goates, Joshua Taylor. Development of an Improved Low-Order Model for Propeller-Wing Interactions.

Degree: MS, Mechanical and Aerospace Engineering, 2018, Utah State University

  For aircraft that have propellers mounted in front of the wings or tail, the prop wash produced by the propellers can have a strong… (more)

Subjects/Keywords: Propeller; Wing; Aerodynamics; Mechanical Engineering

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APA (6th Edition):

Goates, J. T. (2018). Development of an Improved Low-Order Model for Propeller-Wing Interactions. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7394

Chicago Manual of Style (16th Edition):

Goates, Joshua Taylor. “Development of an Improved Low-Order Model for Propeller-Wing Interactions.” 2018. Masters Thesis, Utah State University. Accessed November 22, 2019. https://digitalcommons.usu.edu/etd/7394.

MLA Handbook (7th Edition):

Goates, Joshua Taylor. “Development of an Improved Low-Order Model for Propeller-Wing Interactions.” 2018. Web. 22 Nov 2019.

Vancouver:

Goates JT. Development of an Improved Low-Order Model for Propeller-Wing Interactions. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2019 Nov 22]. Available from: https://digitalcommons.usu.edu/etd/7394.

Council of Science Editors:

Goates JT. Development of an Improved Low-Order Model for Propeller-Wing Interactions. [Masters Thesis]. Utah State University; 2018. Available from: https://digitalcommons.usu.edu/etd/7394

12. Deters, Robert. Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers.

Degree: PhD, 4048, 2014, University of Illinois – Urbana-Champaign

 The low Reynolds number effects of small-scale propellers were investigated. At the Reynolds numbers of interest (below 100,000), a decrease in lift and an increase… (more)

Subjects/Keywords: propeller; slipstream; propeller performance; propeller efficiency; wind tunnel testing; 3D printing; Unmanned Aerial Vehicle (UAV); Micro air vehicle (MAV); low Reynolds number; 7-hole probe; pressure probe measurements; propeller testing; static tests; advancing flow tests; propeller wake; propeller thrust; propeller power; axial velocity; swirl; propeller wing interaction

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APA (6th Edition):

Deters, R. (2014). Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/49607

Chicago Manual of Style (16th Edition):

Deters, Robert. “Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed November 22, 2019. http://hdl.handle.net/2142/49607.

MLA Handbook (7th Edition):

Deters, Robert. “Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers.” 2014. Web. 22 Nov 2019.

Vancouver:

Deters R. Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/2142/49607.

Council of Science Editors:

Deters R. Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/49607


University of New South Wales

13. Mulcahy, Norman Lex. Structural design of shape-adaptive composite marine propellers.

Degree: Mechanical & Manufacturing Engineering, 2010, University of New South Wales

 Nickel-Aluminium-Bronze alloy is the most common material for ship propellers but, more recently, composite materials have been used in propeller construction. One of the advantages… (more)

Subjects/Keywords: Ship propeller design; Ship propeller construction; Shape-adaptive marine propellers

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APA (6th Edition):

Mulcahy, N. L. (2010). Structural design of shape-adaptive composite marine propellers. (Masters Thesis). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/44629 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7926/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Mulcahy, Norman Lex. “Structural design of shape-adaptive composite marine propellers.” 2010. Masters Thesis, University of New South Wales. Accessed November 22, 2019. http://handle.unsw.edu.au/1959.4/44629 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7926/SOURCE01?view=true.

MLA Handbook (7th Edition):

Mulcahy, Norman Lex. “Structural design of shape-adaptive composite marine propellers.” 2010. Web. 22 Nov 2019.

Vancouver:

Mulcahy NL. Structural design of shape-adaptive composite marine propellers. [Internet] [Masters thesis]. University of New South Wales; 2010. [cited 2019 Nov 22]. Available from: http://handle.unsw.edu.au/1959.4/44629 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7926/SOURCE01?view=true.

Council of Science Editors:

Mulcahy NL. Structural design of shape-adaptive composite marine propellers. [Masters Thesis]. University of New South Wales; 2010. Available from: http://handle.unsw.edu.au/1959.4/44629 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:7926/SOURCE01?view=true

14. 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 November 22, 2019. 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. 22 Nov 2019.

Vancouver:

Barros ABd. Análise de desempenho e ruído de hélices de mínima perda de energia. [Internet] [Masters thesis]. University of São Paulo; 2009. [cited 2019 Nov 22]. 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 Canterbury

15. Fernandez, Rajan. Oscillating Hydrofoil Propulsion for Human-Powered Watercraft Applications.

Degree: Mechanical Engineering, 2013, University of Canterbury

 Unlike conventional propellers, flapping wings may generate large amplitude oscillating forces, which can make them difficult to incorporate into a craft design. This is particularly… (more)

Subjects/Keywords: hydrofoil; oscillating; flapping; human-powered; propulsion; propeller

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APA (6th Edition):

Fernandez, R. (2013). Oscillating Hydrofoil Propulsion for Human-Powered Watercraft Applications. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/8206

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):

Fernandez, Rajan. “Oscillating Hydrofoil Propulsion for Human-Powered Watercraft Applications.” 2013. Thesis, University of Canterbury. Accessed November 22, 2019. http://hdl.handle.net/10092/8206.

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

MLA Handbook (7th Edition):

Fernandez, Rajan. “Oscillating Hydrofoil Propulsion for Human-Powered Watercraft Applications.” 2013. Web. 22 Nov 2019.

Vancouver:

Fernandez R. Oscillating Hydrofoil Propulsion for Human-Powered Watercraft Applications. [Internet] [Thesis]. University of Canterbury; 2013. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/10092/8206.

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

Council of Science Editors:

Fernandez R. Oscillating Hydrofoil Propulsion for Human-Powered Watercraft Applications. [Thesis]. University of Canterbury; 2013. Available from: http://hdl.handle.net/10092/8206

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


NSYSU

16. Du, Jiun-Hua. Development of an Underwater Vehicle Simulation Platform.

Degree: Master, IAMPUT, 2011, NSYSU

 In the development of underwater vehicles, it is necessary to conduct performance test in the water tank. However, different factors need to be considered depending… (more)

Subjects/Keywords: Underwater vehicle; altitude control; propeller; PD controller

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APA (6th Edition):

Du, J. (2011). Development of an Underwater Vehicle Simulation Platform. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-1115111-153323

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):

Du, Jiun-Hua. “Development of an Underwater Vehicle Simulation Platform.” 2011. Thesis, NSYSU. Accessed November 22, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-1115111-153323.

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

MLA Handbook (7th Edition):

Du, Jiun-Hua. “Development of an Underwater Vehicle Simulation Platform.” 2011. Web. 22 Nov 2019.

Vancouver:

Du J. Development of an Underwater Vehicle Simulation Platform. [Internet] [Thesis]. NSYSU; 2011. [cited 2019 Nov 22]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-1115111-153323.

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

Council of Science Editors:

Du J. Development of an Underwater Vehicle Simulation Platform. [Thesis]. NSYSU; 2011. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-1115111-153323

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


Iowa State University

17. 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 November 22, 2019. 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. 22 Nov 2019.

Vancouver:

Ning Z. Experimental investigations on the aerodynamic and aeroacoustic characteristics of small UAS propellers. [Internet] [Thesis]. Iowa State University; 2018. [cited 2019 Nov 22]. 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


Virginia Tech

18. Duelley, Richard Skyler. Autonomous Underwater Vehicle Propulsion Design.

Degree: MS, Aerospace and Ocean Engineering, 2010, Virginia Tech

 The goal of this design process was to achieve the most efficient propulsive system for the candidate autonomous underwater vehicle (AUV) as possible. A mathematical… (more)

Subjects/Keywords: AUV; OpenProp; Efficiency; Propulsion; Propeller; NeuMotor

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APA (6th Edition):

Duelley, R. S. (2010). Autonomous Underwater Vehicle Propulsion Design. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34789

Chicago Manual of Style (16th Edition):

Duelley, Richard Skyler. “Autonomous Underwater Vehicle Propulsion Design.” 2010. Masters Thesis, Virginia Tech. Accessed November 22, 2019. http://hdl.handle.net/10919/34789.

MLA Handbook (7th Edition):

Duelley, Richard Skyler. “Autonomous Underwater Vehicle Propulsion Design.” 2010. Web. 22 Nov 2019.

Vancouver:

Duelley RS. Autonomous Underwater Vehicle Propulsion Design. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/10919/34789.

Council of Science Editors:

Duelley RS. Autonomous Underwater Vehicle Propulsion Design. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/34789


University of Adelaide

19. 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 November 22, 2019. 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. 22 Nov 2019.

Vancouver:

Blunt DM. Optimisation and adaptive control of aircraft propeller synchrophase angles. [Internet] [Thesis]. University of Adelaide; 2012. [cited 2019 Nov 22]. 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


Delft University of Technology

20. Candade, A.A. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:.

Degree: 2015, Delft University of Technology

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Candade, A A. “Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135.

MLA Handbook (7th Edition):

Candade, A A. “Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:.” 2015. Web. 22 Nov 2019.

Vancouver:

Candade AA. Horizontal Tailplane-Tip Mounted Tractor Propeller Interaction Effects:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 22]. Available from: http://resolver.tudelft.nl/uuid:e7e16208-8b9a-457e-9bdc-87e65e4c9135.

Council of Science Editors:

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


Oklahoma State University

21. Morris, Mason Wade. Mobile Propeller Dynamometer Validation.

Degree: Mechanical Engineering, 2013, Oklahoma State University

 With growing interest in UAVs and OSU's interest in propeller performance and manufacturing, evaluating UAV propeller and propulsion system performance has become essential. In attempts… (more)

Subjects/Keywords: aerodynamics; dynamometer; dyno; mobile; propeller; vehicle

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APA (6th Edition):

Morris, M. W. (2013). Mobile Propeller Dynamometer Validation. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/15027

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):

Morris, Mason Wade. “Mobile Propeller Dynamometer Validation.” 2013. Thesis, Oklahoma State University. Accessed November 22, 2019. http://hdl.handle.net/11244/15027.

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

MLA Handbook (7th Edition):

Morris, Mason Wade. “Mobile Propeller Dynamometer Validation.” 2013. Web. 22 Nov 2019.

Vancouver:

Morris MW. Mobile Propeller Dynamometer Validation. [Internet] [Thesis]. Oklahoma State University; 2013. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/11244/15027.

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

Council of Science Editors:

Morris MW. Mobile Propeller Dynamometer Validation. [Thesis]. Oklahoma State University; 2013. Available from: http://hdl.handle.net/11244/15027

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


University of Illinois – Urbana-Champaign

22. Shetty, Omkar R. Measurements of Small-Scale Propellers Operating in the Vortex Ring State.

Degree: MS, 4048, 2011, University of Illinois – Urbana-Champaign

 The behavior of small-scale propellers operating in vertical descent and through the vortex ring state (VRS) was measured. In particular, a total of 26 propellers… (more)

Subjects/Keywords: vortex ring state (VRS); propeller tests

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APA (6th Edition):

Shetty, O. R. (2011). Measurements of Small-Scale Propellers Operating in the Vortex Ring State. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/18400

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):

Shetty, Omkar R. “Measurements of Small-Scale Propellers Operating in the Vortex Ring State.” 2011. Thesis, University of Illinois – Urbana-Champaign. Accessed November 22, 2019. http://hdl.handle.net/2142/18400.

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

MLA Handbook (7th Edition):

Shetty, Omkar R. “Measurements of Small-Scale Propellers Operating in the Vortex Ring State.” 2011. Web. 22 Nov 2019.

Vancouver:

Shetty OR. Measurements of Small-Scale Propellers Operating in the Vortex Ring State. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2011. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/2142/18400.

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

Council of Science Editors:

Shetty OR. Measurements of Small-Scale Propellers Operating in the Vortex Ring State. [Thesis]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/18400

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


RMIT University

23. Xu, Chao. CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system.

Degree: 2015, RMIT University

 In recent years Unmanned Air Vehicles (UAVs) have been extensively used for both military operation and academic research. UAV designs are classified by the size,… (more)

Subjects/Keywords: Fields of Research; CFD; UAV; Design; Counter Rotating Propeller; Propeller Spacing; Pitch Angle

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

APA (6th Edition):

Xu, C. (2015). CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161574

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):

Xu, Chao. “CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system.” 2015. Thesis, RMIT University. Accessed November 22, 2019. http://researchbank.rmit.edu.au/view/rmit:161574.

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

MLA Handbook (7th Edition):

Xu, Chao. “CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system.” 2015. Web. 22 Nov 2019.

Vancouver:

Xu C. CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system. [Internet] [Thesis]. RMIT University; 2015. [cited 2019 Nov 22]. Available from: http://researchbank.rmit.edu.au/view/rmit:161574.

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

Council of Science Editors:

Xu C. CFD investigation into propeller spacing and pitch angle for a ducted twin counter rotating propeller system. [Thesis]. RMIT University; 2015. Available from: http://researchbank.rmit.edu.au/view/rmit:161574

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


University of Vienna

24. Konecsni, Tuende. Role of the β-propeller domain of low-density lipoprotein receptor in human rhinovirus infection.

Degree: 2010, University of Vienna

Drei Vertreter der low-density Lipoprotein Rezeptor Familie, LDLR selbst, very-LDLR, und LDLR related protein (LRP) werden von minor group Rhinoviren des Menschen (HRVs) als Rezeptoren… (more)

Subjects/Keywords: 42.32 Virologie; LDL-Rezeptor / β-Propeller / Human Rhinovirus; LDL-receptor / β-propeller / human rhinovirus

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APA (6th Edition):

Konecsni, T. (2010). Role of the β-propeller domain of low-density lipoprotein receptor in human rhinovirus infection. (Thesis). University of Vienna. Retrieved from http://othes.univie.ac.at/9192/

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):

Konecsni, Tuende. “Role of the β-propeller domain of low-density lipoprotein receptor in human rhinovirus infection.” 2010. Thesis, University of Vienna. Accessed November 22, 2019. http://othes.univie.ac.at/9192/.

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

MLA Handbook (7th Edition):

Konecsni, Tuende. “Role of the β-propeller domain of low-density lipoprotein receptor in human rhinovirus infection.” 2010. Web. 22 Nov 2019.

Vancouver:

Konecsni T. Role of the β-propeller domain of low-density lipoprotein receptor in human rhinovirus infection. [Internet] [Thesis]. University of Vienna; 2010. [cited 2019 Nov 22]. Available from: http://othes.univie.ac.at/9192/.

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

Council of Science Editors:

Konecsni T. Role of the β-propeller domain of low-density lipoprotein receptor in human rhinovirus infection. [Thesis]. University of Vienna; 2010. Available from: http://othes.univie.ac.at/9192/

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


University of Texas – Austin

25. -8821-362X. An improved full wake alignment scheme for the prediction of open/ducted propeller performance in steady and unsteady flow.

Degree: MSin Engineering, Civil Engineering, 2017, University of Texas – Austin

 For a long time, ducted propellers have been a viable alternative of propulsion; due to their higher efficiency at high thrust coefficients, less sensitivity to… (more)

Subjects/Keywords: Wake alignment scheme; Open propeller; Ducted propeller; Panel method; BEM; Steady flow; Unsteady flow

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APA (6th Edition):

-8821-362X. (2017). An improved full wake alignment scheme for the prediction of open/ducted propeller performance in steady and unsteady flow. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/61658

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

-8821-362X. “An improved full wake alignment scheme for the prediction of open/ducted propeller performance in steady and unsteady flow.” 2017. Masters Thesis, University of Texas – Austin. Accessed November 22, 2019. http://hdl.handle.net/2152/61658.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

-8821-362X. “An improved full wake alignment scheme for the prediction of open/ducted propeller performance in steady and unsteady flow.” 2017. Web. 22 Nov 2019.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-8821-362X. An improved full wake alignment scheme for the prediction of open/ducted propeller performance in steady and unsteady flow. [Internet] [Masters thesis]. University of Texas – Austin; 2017. [cited 2019 Nov 22]. Available from: http://hdl.handle.net/2152/61658.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

-8821-362X. An improved full wake alignment scheme for the prediction of open/ducted propeller performance in steady and unsteady flow. [Masters Thesis]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/61658

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete


Delft University of Technology

26. Li, Q. Towards optimum swirl recovery for propeller propulsion systems.

Degree: 2019, Delft University of Technology

 In a propeller propulsion system, due to the torque working on the propeller, a rotational motion of the fluid is generated. This rotational motion, expressed… (more)

Subjects/Keywords: propeller; swirl recovery vane; propeller integration

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APA (6th Edition):

Li, Q. (2019). Towards optimum swirl recovery for propeller propulsion systems. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c

Chicago Manual of Style (16th Edition):

Li, Q. “Towards optimum swirl recovery for propeller propulsion systems.” 2019. Doctoral Dissertation, Delft University of Technology. Accessed November 22, 2019. http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c.

MLA Handbook (7th Edition):

Li, Q. “Towards optimum swirl recovery for propeller propulsion systems.” 2019. Web. 22 Nov 2019.

Vancouver:

Li Q. Towards optimum swirl recovery for propeller propulsion systems. [Internet] [Doctoral dissertation]. Delft University of Technology; 2019. [cited 2019 Nov 22]. Available from: http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c.

Council of Science Editors:

Li Q. Towards optimum swirl recovery for propeller propulsion systems. [Doctoral Dissertation]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; ef966464-6b76-434d-b147-81ec247b023c ; 10.4233/uuid:ef966464-6b76-434d-b147-81ec247b023c ; urn:isbn:978-94-6323-805-2 ; urn:NBN:nl:ui:24-uuid:ef966464-6b76-434d-b147-81ec247b023c ; http://resolver.tudelft.nl/uuid:ef966464-6b76-434d-b147-81ec247b023c


University of Tasmania

27. Niyomka, P. Performance and control of a collective and cyclic pitch propeller for an underwater vehicle.

Degree: 2014, University of Tasmania

 Most of the underwater vehicles have control surfaces to enable manoeuvring. The problem with an underwater vehicle with control surfaces is operating it at low… (more)

Subjects/Keywords: underwater vehicle; marine propulsion; collective and cyclic pitch propeller; marine control; simulation; unconventional propulsion; propeller performance

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APA (6th Edition):

Niyomka, P. (2014). Performance and control of a collective and cyclic pitch propeller for an underwater vehicle. (Thesis). University of Tasmania. Retrieved from https://eprints.utas.edu.au/18251/1/Whole-Niyomka-thesis.pdf

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):

Niyomka, P. “Performance and control of a collective and cyclic pitch propeller for an underwater vehicle.” 2014. Thesis, University of Tasmania. Accessed November 22, 2019. https://eprints.utas.edu.au/18251/1/Whole-Niyomka-thesis.pdf.

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

MLA Handbook (7th Edition):

Niyomka, P. “Performance and control of a collective and cyclic pitch propeller for an underwater vehicle.” 2014. Web. 22 Nov 2019.

Vancouver:

Niyomka P. Performance and control of a collective and cyclic pitch propeller for an underwater vehicle. [Internet] [Thesis]. University of Tasmania; 2014. [cited 2019 Nov 22]. Available from: https://eprints.utas.edu.au/18251/1/Whole-Niyomka-thesis.pdf.

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

Council of Science Editors:

Niyomka P. Performance and control of a collective and cyclic pitch propeller for an underwater vehicle. [Thesis]. University of Tasmania; 2014. Available from: https://eprints.utas.edu.au/18251/1/Whole-Niyomka-thesis.pdf

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


KTH

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

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 November 22, 2019. 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. 22 Nov 2019.

Vancouver:

Sjöö F. Development of concept for silent UAV propulsion. [Internet] [Thesis]. KTH; 2018. [cited 2019 Nov 22]. 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


Penn State University

29. Koncoski, Jeremy J. A REDUCED ORDER MODEL OF PROPELLER UNSTEADY FORCES FOR COMPUTATIONAL FLUID DYNAMICS SIMULATIONS.

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

 Propellers generate unsteady forces and moments when operating in flowfields containing spatial and temporal variation. Time-accurate simulation of propeller unsteady forces using a viscous flow… (more)

Subjects/Keywords: propeller; unsteady force; model; CFD; computational fluid dynamics

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

APA (6th Edition):

Koncoski, J. J. (2010). A REDUCED ORDER MODEL OF PROPELLER UNSTEADY FORCES FOR COMPUTATIONAL FLUID DYNAMICS SIMULATIONS. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10369

Chicago Manual of Style (16th Edition):

Koncoski, Jeremy J. “A REDUCED ORDER MODEL OF PROPELLER UNSTEADY FORCES FOR COMPUTATIONAL FLUID DYNAMICS SIMULATIONS.” 2010. Masters Thesis, Penn State University. Accessed November 22, 2019. https://etda.libraries.psu.edu/catalog/10369.

MLA Handbook (7th Edition):

Koncoski, Jeremy J. “A REDUCED ORDER MODEL OF PROPELLER UNSTEADY FORCES FOR COMPUTATIONAL FLUID DYNAMICS SIMULATIONS.” 2010. Web. 22 Nov 2019.

Vancouver:

Koncoski JJ. A REDUCED ORDER MODEL OF PROPELLER UNSTEADY FORCES FOR COMPUTATIONAL FLUID DYNAMICS SIMULATIONS. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2019 Nov 22]. Available from: https://etda.libraries.psu.edu/catalog/10369.

Council of Science Editors:

Koncoski JJ. A REDUCED ORDER MODEL OF PROPELLER UNSTEADY FORCES FOR COMPUTATIONAL FLUID DYNAMICS SIMULATIONS. [Masters Thesis]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/10369


Penn State University

30. Cole, Julia A. A Higher-Order Free-Wake Method for Aerodynamic Performance Prediction of Propeller-Wing Systems.

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

 A new higher-order free-wake (HOFW) method has been developed to enable conceptual design space explorations of propeller-wing systems. The method uses higher order vorticity elements… (more)

Subjects/Keywords: Aerodynamic analysis; free-wake method; propeller-wing interaction

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

APA (6th Edition):

Cole, J. A. (2016). A Higher-Order Free-Wake Method for Aerodynamic Performance Prediction of Propeller-Wing Systems. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13435jac582

Chicago Manual of Style (16th Edition):

Cole, Julia A. “A Higher-Order Free-Wake Method for Aerodynamic Performance Prediction of Propeller-Wing Systems.” 2016. Doctoral Dissertation, Penn State University. Accessed November 22, 2019. https://etda.libraries.psu.edu/catalog/13435jac582.

MLA Handbook (7th Edition):

Cole, Julia A. “A Higher-Order Free-Wake Method for Aerodynamic Performance Prediction of Propeller-Wing Systems.” 2016. Web. 22 Nov 2019.

Vancouver:

Cole JA. A Higher-Order Free-Wake Method for Aerodynamic Performance Prediction of Propeller-Wing Systems. [Internet] [Doctoral dissertation]. Penn State University; 2016. [cited 2019 Nov 22]. Available from: https://etda.libraries.psu.edu/catalog/13435jac582.

Council of Science Editors:

Cole JA. A Higher-Order Free-Wake Method for Aerodynamic Performance Prediction of Propeller-Wing Systems. [Doctoral Dissertation]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/13435jac582

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