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You searched for subject:(tip vortex). Showing records 1 – 30 of 44 total matches.

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Delft University of Technology

1. Varadharajan, Prasath Krishnaswamy (author). The effect of upstream turbulence on a tip-vortex.

Degree: 2019, Delft University of Technology

A tip-vortex in the wake of a finite length lift generating surface has a low pressure region near the axis of the tip-vortex. This low… (more)

Subjects/Keywords: Tip-vortex; Turbulence; PIV

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

APA (6th Edition):

Varadharajan, P. K. (. (2019). The effect of upstream turbulence on a tip-vortex. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8cf2b5a2-b090-453f-8c87-61ec8172448e

Chicago Manual of Style (16th Edition):

Varadharajan, Prasath Krishnaswamy (author). “The effect of upstream turbulence on a tip-vortex.” 2019. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:8cf2b5a2-b090-453f-8c87-61ec8172448e.

MLA Handbook (7th Edition):

Varadharajan, Prasath Krishnaswamy (author). “The effect of upstream turbulence on a tip-vortex.” 2019. Web. 30 Sep 2020.

Vancouver:

Varadharajan PK(. The effect of upstream turbulence on a tip-vortex. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:8cf2b5a2-b090-453f-8c87-61ec8172448e.

Council of Science Editors:

Varadharajan PK(. The effect of upstream turbulence on a tip-vortex. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:8cf2b5a2-b090-453f-8c87-61ec8172448e


Penn State University

2. Andichamy, Veerandra Chakkarava. STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER.

Degree: 2017, Penn State University

 The gap between the turbine rotor blade tip and turbine casing surface is essential to prevent rubbing of these two components. Due to presence of… (more)

Subjects/Keywords: Turbine blade tip; Tip leakage flows; leakage vortex; Leakage vortex mitigation; turbine blade tip design; blade tip modification

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APA (6th Edition):

Andichamy, V. C. (2017). STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14469vka5038

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):

Andichamy, Veerandra Chakkarava. “STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER.” 2017. Thesis, Penn State University. Accessed September 30, 2020. https://submit-etda.libraries.psu.edu/catalog/14469vka5038.

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

MLA Handbook (7th Edition):

Andichamy, Veerandra Chakkarava. “STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER.” 2017. Web. 30 Sep 2020.

Vancouver:

Andichamy VC. STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER. [Internet] [Thesis]. Penn State University; 2017. [cited 2020 Sep 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/14469vka5038.

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

Council of Science Editors:

Andichamy VC. STUDY OF MITIGATION OF TURBINE BLADE TIP LEAKAGE FLOWS USING TIP LEAKAGE INTERRUPTER. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/14469vka5038

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


Delft University of Technology

3. Timmer, M.A. (author). The resonance frequency of tip-vortex cavitation.

Degree: 2015, Delft University of Technology

 Over time much research has been performed on the subject of cavitation. A recent development in this field is the investigation into the behaviour of… (more)

Subjects/Keywords: tip vortex cavitation; center frequency; numerical simulation

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APA (6th Edition):

Timmer, M. A. (. (2015). The resonance frequency of tip-vortex cavitation. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f150f227-645f-444d-bfcf-5430344018b0

Chicago Manual of Style (16th Edition):

Timmer, M A (author). “The resonance frequency of tip-vortex cavitation.” 2015. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:f150f227-645f-444d-bfcf-5430344018b0.

MLA Handbook (7th Edition):

Timmer, M A (author). “The resonance frequency of tip-vortex cavitation.” 2015. Web. 30 Sep 2020.

Vancouver:

Timmer MA(. The resonance frequency of tip-vortex cavitation. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:f150f227-645f-444d-bfcf-5430344018b0.

Council of Science Editors:

Timmer MA(. The resonance frequency of tip-vortex cavitation. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:f150f227-645f-444d-bfcf-5430344018b0


University of Adelaide

4. Whitehead, Edward J. The stability of multiple wing-tip vortices.

Degree: 2010, University of Adelaide

 Over the last forty or so years interest in the study of wing-tip vortices has increased, primarily due to the introduction of larger passenger aircraft… (more)

Subjects/Keywords: stability; vortices; batchelor vortex, inviscid stability; viscous stability; wing-tip vortex

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APA (6th Edition):

Whitehead, E. J. (2010). The stability of multiple wing-tip vortices. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/57899

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):

Whitehead, Edward J. “The stability of multiple wing-tip vortices.” 2010. Thesis, University of Adelaide. Accessed September 30, 2020. http://hdl.handle.net/2440/57899.

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

MLA Handbook (7th Edition):

Whitehead, Edward J. “The stability of multiple wing-tip vortices.” 2010. Web. 30 Sep 2020.

Vancouver:

Whitehead EJ. The stability of multiple wing-tip vortices. [Internet] [Thesis]. University of Adelaide; 2010. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/2440/57899.

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

Council of Science Editors:

Whitehead EJ. The stability of multiple wing-tip vortices. [Thesis]. University of Adelaide; 2010. Available from: http://hdl.handle.net/2440/57899

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


Penn State University

5. Hanson, David Royal. Cavitation Inception for Non-elliptically Loaded Fins.

Degree: 2012, Penn State University

 Cavitation on lift-producing fins often occurs at higher cavitation numbers in the tip vortex than elsewhere in the flow. Tip vortex cavitation inception is known… (more)

Subjects/Keywords: Cavitation; Vortex Lattice Theory; Tip Vortex Cavitation; Particle Image Velocimetry; Acoustic Measurements

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APA (6th Edition):

Hanson, D. R. (2012). Cavitation Inception for Non-elliptically Loaded Fins. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/16305

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):

Hanson, David Royal. “Cavitation Inception for Non-elliptically Loaded Fins.” 2012. Thesis, Penn State University. Accessed September 30, 2020. https://submit-etda.libraries.psu.edu/catalog/16305.

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

MLA Handbook (7th Edition):

Hanson, David Royal. “Cavitation Inception for Non-elliptically Loaded Fins.” 2012. Web. 30 Sep 2020.

Vancouver:

Hanson DR. Cavitation Inception for Non-elliptically Loaded Fins. [Internet] [Thesis]. Penn State University; 2012. [cited 2020 Sep 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/16305.

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

Council of Science Editors:

Hanson DR. Cavitation Inception for Non-elliptically Loaded Fins. [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/16305

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

6. Mula, Swathi Mahalaxmi. Stability and turbulence characteristics of a spiraling vortex filament using proper orthogonal decomposition.

Degree: PhD, Aerospace Engineering, 2015, University of Texas – Austin

 The stability and turbulence characteristics of a vortex filament emanating from a single-bladed rotor in hover are investigated using proper orthogonal decomposition. The rotor is… (more)

Subjects/Keywords: Instability; Turbulence; Tip vortex; Rotor; Vortex wander; Proper orthogonal decomposition; Particle image velocimetry

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APA (6th Edition):

Mula, S. M. (2015). Stability and turbulence characteristics of a spiraling vortex filament using proper orthogonal decomposition. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/30268

Chicago Manual of Style (16th Edition):

Mula, Swathi Mahalaxmi. “Stability and turbulence characteristics of a spiraling vortex filament using proper orthogonal decomposition.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed September 30, 2020. http://hdl.handle.net/2152/30268.

MLA Handbook (7th Edition):

Mula, Swathi Mahalaxmi. “Stability and turbulence characteristics of a spiraling vortex filament using proper orthogonal decomposition.” 2015. Web. 30 Sep 2020.

Vancouver:

Mula SM. Stability and turbulence characteristics of a spiraling vortex filament using proper orthogonal decomposition. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/2152/30268.

Council of Science Editors:

Mula SM. Stability and turbulence characteristics of a spiraling vortex filament using proper orthogonal decomposition. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/30268


Delft University of Technology

7. Liebrand, Rens (author). Tip vortex modelling for cavitation noise applications: A verification and validation study in ReFRESCO.

Degree: 2019, Delft University of Technology

Cavitating tip vortices of marine propellers are the main contributors to underwater radiated ship noise due to their dynamic behavior and broadband sound spectrum. Experimentally,… (more)

Subjects/Keywords: Cavitating tip vortex noise; Elliptical wing; ReFRESCO; Verification and validation

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APA (6th Edition):

Liebrand, R. (. (2019). Tip vortex modelling for cavitation noise applications: A verification and validation study in ReFRESCO. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:38888cc9-a116-42fa-bb2d-bdc7f407a78f

Chicago Manual of Style (16th Edition):

Liebrand, Rens (author). “Tip vortex modelling for cavitation noise applications: A verification and validation study in ReFRESCO.” 2019. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:38888cc9-a116-42fa-bb2d-bdc7f407a78f.

MLA Handbook (7th Edition):

Liebrand, Rens (author). “Tip vortex modelling for cavitation noise applications: A verification and validation study in ReFRESCO.” 2019. Web. 30 Sep 2020.

Vancouver:

Liebrand R(. Tip vortex modelling for cavitation noise applications: A verification and validation study in ReFRESCO. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:38888cc9-a116-42fa-bb2d-bdc7f407a78f.

Council of Science Editors:

Liebrand R(. Tip vortex modelling for cavitation noise applications: A verification and validation study in ReFRESCO. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:38888cc9-a116-42fa-bb2d-bdc7f407a78f

8. León Calderón, Lucía. Numerical simulations of the tip leakage vortex in a waterjet pump using a Reynolds averaged approach .

Degree: Chalmers tekniska högskola / Institutionen för mekanik och maritima vetenskaper, 2019, Chalmers University of Technology

 Waterjet pumps are widely used among maritime transport vehicles, such as high-speed vessels. Many experiments have been performed to analyze the complex flow patterns present… (more)

Subjects/Keywords: Waterjet Pump; RANS; Tip Leakage Vortex; MRF; Sliding Mesh; CFD

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APA (6th Edition):

León Calderón, L. (2019). Numerical simulations of the tip leakage vortex in a waterjet pump using a Reynolds averaged approach . (Thesis). Chalmers University of Technology. Retrieved from http://hdl.handle.net/20.500.12380/300163

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):

León Calderón, Lucía. “Numerical simulations of the tip leakage vortex in a waterjet pump using a Reynolds averaged approach .” 2019. Thesis, Chalmers University of Technology. Accessed September 30, 2020. http://hdl.handle.net/20.500.12380/300163.

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

MLA Handbook (7th Edition):

León Calderón, Lucía. “Numerical simulations of the tip leakage vortex in a waterjet pump using a Reynolds averaged approach .” 2019. Web. 30 Sep 2020.

Vancouver:

León Calderón L. Numerical simulations of the tip leakage vortex in a waterjet pump using a Reynolds averaged approach . [Internet] [Thesis]. Chalmers University of Technology; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/20.500.12380/300163.

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

Council of Science Editors:

León Calderón L. Numerical simulations of the tip leakage vortex in a waterjet pump using a Reynolds averaged approach . [Thesis]. Chalmers University of Technology; 2019. Available from: http://hdl.handle.net/20.500.12380/300163

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


University of Notre Dame

9. Travis Charles Douville. The Effect of Gap Size and Reynolds Number on Turbine Blade Flat and Suction-Side Squealer Tip Flowfields</h1>.

Degree: Aerospace and Mechanical Engineering, 2005, University of Notre Dame

  In order to further the understanding of turbine tip leakage and passage flow mechanisms for undesirable entropy production, an experiment was conducted in a… (more)

Subjects/Keywords: squealer tip; tip leakage vortex; linear cascade; turbine rotor

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APA (6th Edition):

Douville, T. C. (2005). The Effect of Gap Size and Reynolds Number on Turbine Blade Flat and Suction-Side Squealer Tip Flowfields</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/w9504x5427n

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):

Douville, Travis Charles. “The Effect of Gap Size and Reynolds Number on Turbine Blade Flat and Suction-Side Squealer Tip Flowfields</h1>.” 2005. Thesis, University of Notre Dame. Accessed September 30, 2020. https://curate.nd.edu/show/w9504x5427n.

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

MLA Handbook (7th Edition):

Douville, Travis Charles. “The Effect of Gap Size and Reynolds Number on Turbine Blade Flat and Suction-Side Squealer Tip Flowfields</h1>.” 2005. Web. 30 Sep 2020.

Vancouver:

Douville TC. The Effect of Gap Size and Reynolds Number on Turbine Blade Flat and Suction-Side Squealer Tip Flowfields</h1>. [Internet] [Thesis]. University of Notre Dame; 2005. [cited 2020 Sep 30]. Available from: https://curate.nd.edu/show/w9504x5427n.

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

Council of Science Editors:

Douville TC. The Effect of Gap Size and Reynolds Number on Turbine Blade Flat and Suction-Side Squealer Tip Flowfields</h1>. [Thesis]. University of Notre Dame; 2005. Available from: https://curate.nd.edu/show/w9504x5427n

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


Delft University of Technology

10. van der Meer, Sylvain (author). Numerical Assessment of Directional Stability and Control with Tip-mounted Propellers.

Degree: 2020, Delft University of Technology

 A propeller has a high propulsive efficiency, yet inherently leaves the air it propels swirling. The efficiency of a propeller can be enhanced by placing… (more)

Subjects/Keywords: tip-mounted propeller; propeller; propeller-wing interaction; tip-vortex; stability and control; directional stability and control

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APA (6th Edition):

van der Meer, S. (. (2020). Numerical Assessment of Directional Stability and Control with Tip-mounted Propellers. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9a40cac7-f43f-4227-9ece-4f84acab29c6

Chicago Manual of Style (16th Edition):

van der Meer, Sylvain (author). “Numerical Assessment of Directional Stability and Control with Tip-mounted Propellers.” 2020. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:9a40cac7-f43f-4227-9ece-4f84acab29c6.

MLA Handbook (7th Edition):

van der Meer, Sylvain (author). “Numerical Assessment of Directional Stability and Control with Tip-mounted Propellers.” 2020. Web. 30 Sep 2020.

Vancouver:

van der Meer S(. Numerical Assessment of Directional Stability and Control with Tip-mounted Propellers. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:9a40cac7-f43f-4227-9ece-4f84acab29c6.

Council of Science Editors:

van der Meer S(. Numerical Assessment of Directional Stability and Control with Tip-mounted Propellers. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:9a40cac7-f43f-4227-9ece-4f84acab29c6


Università degli Studi di Bergamo

11. MIORINI, RINALDO LUIGI. Investigations on the flow inside pumps by means of 2D particle image velocimetry.

Degree: 2010, Università degli Studi di Bergamo

In the first part of the work, a centrifugal pump is run at various capacities to derive information about the flow around the diffuser vanes.… (more)

Subjects/Keywords: axial pump; centrifugal pump; diffuser; particle image velocimetry; phase average; rotor; tip leakage vortex; wake

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APA (6th Edition):

MIORINI, R. L. (2010). Investigations on the flow inside pumps by means of 2D particle image velocimetry. (Thesis). Università degli Studi di Bergamo. Retrieved from http://hdl.handle.net/10446/615

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):

MIORINI, RINALDO LUIGI. “Investigations on the flow inside pumps by means of 2D particle image velocimetry.” 2010. Thesis, Università degli Studi di Bergamo. Accessed September 30, 2020. http://hdl.handle.net/10446/615.

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

MLA Handbook (7th Edition):

MIORINI, RINALDO LUIGI. “Investigations on the flow inside pumps by means of 2D particle image velocimetry.” 2010. Web. 30 Sep 2020.

Vancouver:

MIORINI RL. Investigations on the flow inside pumps by means of 2D particle image velocimetry. [Internet] [Thesis]. Università degli Studi di Bergamo; 2010. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10446/615.

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

Council of Science Editors:

MIORINI RL. Investigations on the flow inside pumps by means of 2D particle image velocimetry. [Thesis]. Università degli Studi di Bergamo; 2010. Available from: http://hdl.handle.net/10446/615

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


Delft University of Technology

12. van den Boogaard, Maurits (author). Numerical simulation of a cavitating line vortex in a converging-diverging nozzle: using RANS and SRS methods.

Degree: 2019, Delft University of Technology

Tip vortex cavitation was previously identified as a source of the broadband noise emitted by ships underwater. This leads to unwanted noise and vibrations on… (more)

Subjects/Keywords: Turbulence modeling; Cavitating tip vortex noise; Cavity dynamics; Venturi; Swirling flow; spectral analysis; ReFRESCO

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APA (6th Edition):

van den Boogaard, M. (. (2019). Numerical simulation of a cavitating line vortex in a converging-diverging nozzle: using RANS and SRS methods. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d04e2cb2-7371-4ebf-bc96-6c2e5a48874a

Chicago Manual of Style (16th Edition):

van den Boogaard, Maurits (author). “Numerical simulation of a cavitating line vortex in a converging-diverging nozzle: using RANS and SRS methods.” 2019. Masters Thesis, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:d04e2cb2-7371-4ebf-bc96-6c2e5a48874a.

MLA Handbook (7th Edition):

van den Boogaard, Maurits (author). “Numerical simulation of a cavitating line vortex in a converging-diverging nozzle: using RANS and SRS methods.” 2019. Web. 30 Sep 2020.

Vancouver:

van den Boogaard M(. Numerical simulation of a cavitating line vortex in a converging-diverging nozzle: using RANS and SRS methods. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:d04e2cb2-7371-4ebf-bc96-6c2e5a48874a.

Council of Science Editors:

van den Boogaard M(. Numerical simulation of a cavitating line vortex in a converging-diverging nozzle: using RANS and SRS methods. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:d04e2cb2-7371-4ebf-bc96-6c2e5a48874a


University of Minnesota

13. Dasari, Teja. Near-wake studies of a utility-scale wind turbine using natural snowfall-based visualization and Particle Image Velocimetry.

Degree: PhD, Mechanical Engineering, 2018, University of Minnesota

 Wind turbine technology has been extensively researched in the past century. A major part of this research effort was to improve the efficiencies of energy… (more)

Subjects/Keywords: Field Measurements; Particle Image Velocimetry; Tip Vortex; Turbine wake; Utility-scale; Wind Turbine

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APA (6th Edition):

Dasari, T. (2018). Near-wake studies of a utility-scale wind turbine using natural snowfall-based visualization and Particle Image Velocimetry. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/202208

Chicago Manual of Style (16th Edition):

Dasari, Teja. “Near-wake studies of a utility-scale wind turbine using natural snowfall-based visualization and Particle Image Velocimetry.” 2018. Doctoral Dissertation, University of Minnesota. Accessed September 30, 2020. http://hdl.handle.net/11299/202208.

MLA Handbook (7th Edition):

Dasari, Teja. “Near-wake studies of a utility-scale wind turbine using natural snowfall-based visualization and Particle Image Velocimetry.” 2018. Web. 30 Sep 2020.

Vancouver:

Dasari T. Near-wake studies of a utility-scale wind turbine using natural snowfall-based visualization and Particle Image Velocimetry. [Internet] [Doctoral dissertation]. University of Minnesota; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/11299/202208.

Council of Science Editors:

Dasari T. Near-wake studies of a utility-scale wind turbine using natural snowfall-based visualization and Particle Image Velocimetry. [Doctoral Dissertation]. University of Minnesota; 2018. Available from: http://hdl.handle.net/11299/202208


Virginia Tech

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

Degree: MS, Aerospace 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 (6th Edition):

Murray, H. H. I. (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, Henry Hall IV. “Turbulence and Sound Generated by a Rotor Operating Near a Wall.” 2016. Masters Thesis, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/71332.

MLA Handbook (7th Edition):

Murray, Henry Hall IV. “Turbulence and Sound Generated by a Rotor Operating Near a Wall.” 2016. Web. 30 Sep 2020.

Vancouver:

Murray HHI. Turbulence and Sound Generated by a Rotor Operating Near a Wall. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/71332.

Council of Science Editors:

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


Virginia Tech

15. Tian, Qing. Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade.

Degree: PhD, Aerospace and Ocean Engineering, 2006, Virginia Tech

 This dissertation presents the results from an experimental study of three-dimensional turbulent tip gap flow in a linear cascade wind tunnel with 3.3% chord tip(more)

Subjects/Keywords: Tip Separation Vortex; Turbulence; Compressor; Three-Dimensional Separation; Tip Leakage Vortex; Laser Doppler Velocimeter; Tip Gap Flow; Oil Flow Visualization

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APA (6th Edition):

Tian, Q. (2006). Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30062

Chicago Manual of Style (16th Edition):

Tian, Qing. “Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade.” 2006. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/30062.

MLA Handbook (7th Edition):

Tian, Qing. “Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade.” 2006. Web. 30 Sep 2020.

Vancouver:

Tian Q. Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade. [Internet] [Doctoral dissertation]. Virginia Tech; 2006. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/30062.

Council of Science Editors:

Tian Q. Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade. [Doctoral Dissertation]. Virginia Tech; 2006. Available from: http://hdl.handle.net/10919/30062


Virginia Tech

16. Intaratep, Nanyaporn. Formation and Development of the Tip Leakage Vortex in a Simulated Axial Compressor with Unsteady Inflow.

Degree: PhD, Aerospace and Ocean Engineering, 2006, Virginia Tech

 The interaction between rotor blade tip leakage vortex and inflow disturbances, such as encountered in shrouded marine propulsors, was simulated in the Virginia Tech Linear… (more)

Subjects/Keywords: unsteady inflow; vortex shedding; moving endwall; linear cascade; axial compressor; tip leakage vortex

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APA (6th Edition):

Intaratep, N. (2006). Formation and Development of the Tip Leakage Vortex in a Simulated Axial Compressor with Unsteady Inflow. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26771

Chicago Manual of Style (16th Edition):

Intaratep, Nanyaporn. “Formation and Development of the Tip Leakage Vortex in a Simulated Axial Compressor with Unsteady Inflow.” 2006. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/26771.

MLA Handbook (7th Edition):

Intaratep, Nanyaporn. “Formation and Development of the Tip Leakage Vortex in a Simulated Axial Compressor with Unsteady Inflow.” 2006. Web. 30 Sep 2020.

Vancouver:

Intaratep N. Formation and Development of the Tip Leakage Vortex in a Simulated Axial Compressor with Unsteady Inflow. [Internet] [Doctoral dissertation]. Virginia Tech; 2006. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/26771.

Council of Science Editors:

Intaratep N. Formation and Development of the Tip Leakage Vortex in a Simulated Axial Compressor with Unsteady Inflow. [Doctoral Dissertation]. Virginia Tech; 2006. Available from: http://hdl.handle.net/10919/26771

17. Li, Bo. Aerodynamic and acoustic analysis of the tip-leakage flow past a single ailfoil : Analyse aérodynamique et acoustique de l’écoulement de jeu d’un profil isolé.

Degree: Docteur es, Mécanique des fluides et aéroacoustique, 2016, Lyon

L'écoulement de jeu est un phénomène très important dans les turbomachines. Il provient du mouvement relatif entre la pale et la paroi d'extrémité, et la… (more)

Subjects/Keywords: Écoulement de jeu; Tip-leakage flow; Zonal large-eddy simulation; Reynolds-averaged Navier-Stokes; Vortex wandering; Far-field noise modelling

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APA (6th Edition):

Li, B. (2016). Aerodynamic and acoustic analysis of the tip-leakage flow past a single ailfoil : Analyse aérodynamique et acoustique de l’écoulement de jeu d’un profil isolé. (Doctoral Dissertation). Lyon. Retrieved from http://www.theses.fr/2016LYSEC042

Chicago Manual of Style (16th Edition):

Li, Bo. “Aerodynamic and acoustic analysis of the tip-leakage flow past a single ailfoil : Analyse aérodynamique et acoustique de l’écoulement de jeu d’un profil isolé.” 2016. Doctoral Dissertation, Lyon. Accessed September 30, 2020. http://www.theses.fr/2016LYSEC042.

MLA Handbook (7th Edition):

Li, Bo. “Aerodynamic and acoustic analysis of the tip-leakage flow past a single ailfoil : Analyse aérodynamique et acoustique de l’écoulement de jeu d’un profil isolé.” 2016. Web. 30 Sep 2020.

Vancouver:

Li B. Aerodynamic and acoustic analysis of the tip-leakage flow past a single ailfoil : Analyse aérodynamique et acoustique de l’écoulement de jeu d’un profil isolé. [Internet] [Doctoral dissertation]. Lyon; 2016. [cited 2020 Sep 30]. Available from: http://www.theses.fr/2016LYSEC042.

Council of Science Editors:

Li B. Aerodynamic and acoustic analysis of the tip-leakage flow past a single ailfoil : Analyse aérodynamique et acoustique de l’écoulement de jeu d’un profil isolé. [Doctoral Dissertation]. Lyon; 2016. Available from: http://www.theses.fr/2016LYSEC042

18. Marinelli, Andrea T. Biologically Inspired Wing Tip Geometry Optimization.

Degree: MS, 2010, Worcester Polytechnic Institute

 Wingtip vortices are an important problem in aerodynamic and hydrodynamic engineering because of their contribution to induced drag, tip cavitation, and wake turbulence. These effects… (more)

Subjects/Keywords: genetic algorithms; optimization; tip vortices; winglet; vortex strength

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APA (6th Edition):

Marinelli, A. T. (2010). Biologically Inspired Wing Tip Geometry Optimization. (Thesis). Worcester Polytechnic Institute. Retrieved from etd-051110-094009 ; https://digitalcommons.wpi.edu/etd-theses/805

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):

Marinelli, Andrea T. “Biologically Inspired Wing Tip Geometry Optimization.” 2010. Thesis, Worcester Polytechnic Institute. Accessed September 30, 2020. etd-051110-094009 ; https://digitalcommons.wpi.edu/etd-theses/805.

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

MLA Handbook (7th Edition):

Marinelli, Andrea T. “Biologically Inspired Wing Tip Geometry Optimization.” 2010. Web. 30 Sep 2020.

Vancouver:

Marinelli AT. Biologically Inspired Wing Tip Geometry Optimization. [Internet] [Thesis]. Worcester Polytechnic Institute; 2010. [cited 2020 Sep 30]. Available from: etd-051110-094009 ; https://digitalcommons.wpi.edu/etd-theses/805.

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

Council of Science Editors:

Marinelli AT. Biologically Inspired Wing Tip Geometry Optimization. [Thesis]. Worcester Polytechnic Institute; 2010. Available from: etd-051110-094009 ; https://digitalcommons.wpi.edu/etd-theses/805

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


Brno University of Technology

19. Mazánek, Adam. Přehled prostředků pro snižování indukovaného odporu: Overview of means for reducing induced drag.

Degree: 2019, Brno University of Technology

 This bachelor thesis deals with the creation of overview of means for reducing induced drag on the wing of an airplane. It describes production of… (more)

Subjects/Keywords: indukovaný odpor; vztlak; winglety; zakončení křídla; křídlo; spotřeba paliva; koncový vír; induced drag; lift; winglets; wing tip; wing; fuel consumption; tip vortex

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APA (6th Edition):

Mazánek, A. (2019). Přehled prostředků pro snižování indukovaného odporu: Overview of means for reducing induced drag. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/66888

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):

Mazánek, Adam. “Přehled prostředků pro snižování indukovaného odporu: Overview of means for reducing induced drag.” 2019. Thesis, Brno University of Technology. Accessed September 30, 2020. http://hdl.handle.net/11012/66888.

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

MLA Handbook (7th Edition):

Mazánek, Adam. “Přehled prostředků pro snižování indukovaného odporu: Overview of means for reducing induced drag.” 2019. Web. 30 Sep 2020.

Vancouver:

Mazánek A. Přehled prostředků pro snižování indukovaného odporu: Overview of means for reducing induced drag. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/11012/66888.

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

Council of Science Editors:

Mazánek A. Přehled prostředků pro snižování indukovaného odporu: Overview of means for reducing induced drag. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/66888

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

20. Riera, William. Evaluation of the ZDES method on an axial compressor : analysis of the effects of upstream wake and throttle on the tip-leakage flow. : Evaluation de la méthode ZDES sur un compresseur axial : analyse des effets de sillages venant de l’amont et du vannage sur le tourbillon de jeu.

Degree: Docteur es, Mécanique des milieux fluides, 2014, Ecully, Ecole centrale de Lyon

L’écoulement de jeu dans les compresseurs axiaux est étudié à l’aide de la Zonal Detached Eddy Simulation (ZDES). L’objectif consiste à évaluer la capacité de… (more)

Subjects/Keywords: Simulation numérique; RANS; LES; ZDES; Écoulement de jeu; Compresseur axial; CREATE; Distorsion amont; Tourbillon de jeu; Interaction sillage tourbillon; Vannage; Numerical simulation; RANS; LES; ZDES; Tip leakage flow; Axial compressor; CREATE; Upstream distortion; Tip leakage vortex; Wake vortex interaction; Throttle

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APA (6th Edition):

Riera, W. (2014). Evaluation of the ZDES method on an axial compressor : analysis of the effects of upstream wake and throttle on the tip-leakage flow. : Evaluation de la méthode ZDES sur un compresseur axial : analyse des effets de sillages venant de l’amont et du vannage sur le tourbillon de jeu. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon. Retrieved from http://www.theses.fr/2014ECDL0030

Chicago Manual of Style (16th Edition):

Riera, William. “Evaluation of the ZDES method on an axial compressor : analysis of the effects of upstream wake and throttle on the tip-leakage flow. : Evaluation de la méthode ZDES sur un compresseur axial : analyse des effets de sillages venant de l’amont et du vannage sur le tourbillon de jeu.” 2014. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed September 30, 2020. http://www.theses.fr/2014ECDL0030.

MLA Handbook (7th Edition):

Riera, William. “Evaluation of the ZDES method on an axial compressor : analysis of the effects of upstream wake and throttle on the tip-leakage flow. : Evaluation de la méthode ZDES sur un compresseur axial : analyse des effets de sillages venant de l’amont et du vannage sur le tourbillon de jeu.” 2014. Web. 30 Sep 2020.

Vancouver:

Riera W. Evaluation of the ZDES method on an axial compressor : analysis of the effects of upstream wake and throttle on the tip-leakage flow. : Evaluation de la méthode ZDES sur un compresseur axial : analyse des effets de sillages venant de l’amont et du vannage sur le tourbillon de jeu. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2014. [cited 2020 Sep 30]. Available from: http://www.theses.fr/2014ECDL0030.

Council of Science Editors:

Riera W. Evaluation of the ZDES method on an axial compressor : analysis of the effects of upstream wake and throttle on the tip-leakage flow. : Evaluation de la méthode ZDES sur un compresseur axial : analyse des effets de sillages venant de l’amont et du vannage sur le tourbillon de jeu. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; 2014. Available from: http://www.theses.fr/2014ECDL0030


University of Michigan

21. Oweis, Ghanem Farah. An experimental investigation into the dynamics of propeller tip vortices and the associated cavitation noise.

Degree: PhD, Ocean engineering, 2003, University of Michigan

 An experimental investigation into the tip leakage vortex (TLV) flow from a 3-bladed ducted marine propulsor was performed to assist in understanding the dynamics of… (more)

Subjects/Keywords: Associated; Cavitation Noise; Dynamics; Experimental; Investigation; Propeller; Tip Leakage Vortex; Vortices

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APA (6th Edition):

Oweis, G. F. (2003). An experimental investigation into the dynamics of propeller tip vortices and the associated cavitation noise. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/123928

Chicago Manual of Style (16th Edition):

Oweis, Ghanem Farah. “An experimental investigation into the dynamics of propeller tip vortices and the associated cavitation noise.” 2003. Doctoral Dissertation, University of Michigan. Accessed September 30, 2020. http://hdl.handle.net/2027.42/123928.

MLA Handbook (7th Edition):

Oweis, Ghanem Farah. “An experimental investigation into the dynamics of propeller tip vortices and the associated cavitation noise.” 2003. Web. 30 Sep 2020.

Vancouver:

Oweis GF. An experimental investigation into the dynamics of propeller tip vortices and the associated cavitation noise. [Internet] [Doctoral dissertation]. University of Michigan; 2003. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/2027.42/123928.

Council of Science Editors:

Oweis GF. An experimental investigation into the dynamics of propeller tip vortices and the associated cavitation noise. [Doctoral Dissertation]. University of Michigan; 2003. Available from: http://hdl.handle.net/2027.42/123928


Virginia Tech

22. Shin, Sangmook. Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid.

Degree: PhD, Aerospace and Ocean Engineering, 2001, Virginia Tech

 A three-dimensional unstructured incompressible RANS code has been developed using artificial compressibility and Spalart-Allmaras eddy viscosity model. A node-based finite volume method is used in… (more)

Subjects/Keywords: tetrahedral grid; connectivity pattern; tip leakage vortex; incompressible RANS code

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APA (6th Edition):

Shin, S. (2001). Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28947

Chicago Manual of Style (16th Edition):

Shin, Sangmook. “Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid.” 2001. Doctoral Dissertation, Virginia Tech. Accessed September 30, 2020. http://hdl.handle.net/10919/28947.

MLA Handbook (7th Edition):

Shin, Sangmook. “Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid.” 2001. Web. 30 Sep 2020.

Vancouver:

Shin S. Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid. [Internet] [Doctoral dissertation]. Virginia Tech; 2001. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10919/28947.

Council of Science Editors:

Shin S. Reynolds-Averaged Navier-Stokes Computation of Tip Clearance Flow in a Compressor Cascade Using an Unstructured Grid. [Doctoral Dissertation]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/28947

23. 若松, 祐樹. 超音速旅客機用結合翼の空力特性に関する数値解析(要旨).

Degree: 修士(科学), 2017, The University of Tokyo / 東京大学

Subjects/Keywords: Supersonic Airplane; Joined Wing; Shock Wave Interference; Wing Tip Vortex

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APA (6th Edition):

若松, . (2017). 超音速旅客機用結合翼の空力特性に関する数値解析(要旨). (Thesis). The University of Tokyo / 東京大学. Retrieved from http://hdl.handle.net/2261/52282

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):

若松, 祐樹. “超音速旅客機用結合翼の空力特性に関する数値解析(要旨).” 2017. Thesis, The University of Tokyo / 東京大学. Accessed September 30, 2020. http://hdl.handle.net/2261/52282.

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

MLA Handbook (7th Edition):

若松, 祐樹. “超音速旅客機用結合翼の空力特性に関する数値解析(要旨).” 2017. Web. 30 Sep 2020.

Vancouver:

若松 . 超音速旅客機用結合翼の空力特性に関する数値解析(要旨). [Internet] [Thesis]. The University of Tokyo / 東京大学; 2017. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/2261/52282.

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

Council of Science Editors:

若松 . 超音速旅客機用結合翼の空力特性に関する数値解析(要旨). [Thesis]. The University of Tokyo / 東京大学; 2017. Available from: http://hdl.handle.net/2261/52282

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


Delft University of Technology

24. Lignarolo, L.E.M. On the Turbulent Mixing in Horizontal Axis Wind Turbine Wakes.

Degree: 2016, Delft University of Technology

 The wake flow of a horizontal axis wind turbine is characterised by lower wind speed and higher turbulence than the free-stream conditions. When clustered in… (more)

Subjects/Keywords: wake mixing; horizontal axis wind turbines; particle image velocimetry; tip vortex instability

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APA (6th Edition):

Lignarolo, L. E. M. (2016). On the Turbulent Mixing in Horizontal Axis Wind Turbine Wakes. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57

Chicago Manual of Style (16th Edition):

Lignarolo, L E M. “On the Turbulent Mixing in Horizontal Axis Wind Turbine Wakes.” 2016. Doctoral Dissertation, Delft University of Technology. Accessed September 30, 2020. http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57.

MLA Handbook (7th Edition):

Lignarolo, L E M. “On the Turbulent Mixing in Horizontal Axis Wind Turbine Wakes.” 2016. Web. 30 Sep 2020.

Vancouver:

Lignarolo LEM. On the Turbulent Mixing in Horizontal Axis Wind Turbine Wakes. [Internet] [Doctoral dissertation]. Delft University of Technology; 2016. [cited 2020 Sep 30]. Available from: http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57.

Council of Science Editors:

Lignarolo LEM. On the Turbulent Mixing in Horizontal Axis Wind Turbine Wakes. [Doctoral Dissertation]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; urn:NBN:nl:ui:24-uuid:057fa33f-82a3-4139-beb8-53f184cd1d57 ; http://resolver.tudelft.nl/uuid:057fa33f-82a3-4139-beb8-53f184cd1d57

25. Margalida, Gabriel. Analyse expérimentale et contrôle actif de l'écoulement dans un compresseur axial mono-étagée durant la transition vers le décrochage tournant : Experimental study and active flow control in a single stage axial compressor during the transition to rotating stall.

Degree: Docteur es, Mécanique-matériaux (AM), 2019, Paris, ENSAM

Durant la dernière décennie, le secteur aéronautique n’a cessé de croître et le nombre de passagers transportés a considérablement augmenté. En parallèle, des politiques de… (more)

Subjects/Keywords: Décrochage tournant; Contrôle actif d'écoulements; Compresseur axial; Tourbillon de jeu; Turboréacteur; Rotating stall; Active flow control; Axial compressor; Tip gap vortex; Turbojet; 620

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APA (6th Edition):

Margalida, G. (2019). Analyse expérimentale et contrôle actif de l'écoulement dans un compresseur axial mono-étagée durant la transition vers le décrochage tournant : Experimental study and active flow control in a single stage axial compressor during the transition to rotating stall. (Doctoral Dissertation). Paris, ENSAM. Retrieved from http://www.theses.fr/2019ENAM0039

Chicago Manual of Style (16th Edition):

Margalida, Gabriel. “Analyse expérimentale et contrôle actif de l'écoulement dans un compresseur axial mono-étagée durant la transition vers le décrochage tournant : Experimental study and active flow control in a single stage axial compressor during the transition to rotating stall.” 2019. Doctoral Dissertation, Paris, ENSAM. Accessed September 30, 2020. http://www.theses.fr/2019ENAM0039.

MLA Handbook (7th Edition):

Margalida, Gabriel. “Analyse expérimentale et contrôle actif de l'écoulement dans un compresseur axial mono-étagée durant la transition vers le décrochage tournant : Experimental study and active flow control in a single stage axial compressor during the transition to rotating stall.” 2019. Web. 30 Sep 2020.

Vancouver:

Margalida G. Analyse expérimentale et contrôle actif de l'écoulement dans un compresseur axial mono-étagée durant la transition vers le décrochage tournant : Experimental study and active flow control in a single stage axial compressor during the transition to rotating stall. [Internet] [Doctoral dissertation]. Paris, ENSAM; 2019. [cited 2020 Sep 30]. Available from: http://www.theses.fr/2019ENAM0039.

Council of Science Editors:

Margalida G. Analyse expérimentale et contrôle actif de l'écoulement dans un compresseur axial mono-étagée durant la transition vers le décrochage tournant : Experimental study and active flow control in a single stage axial compressor during the transition to rotating stall. [Doctoral Dissertation]. Paris, ENSAM; 2019. Available from: http://www.theses.fr/2019ENAM0039


University of Victoria

26. Franchini, Italo. Experimental studies of a small scale horizontal axis tidal turbine.

Degree: Department of Mechanical Engineering, 2016, University of Victoria

 The research in this thesis focuses on the investigation of tidal turbines using a small scale horizontal axis tidal turbine and a 2D hydrofoil testing… (more)

Subjects/Keywords: tidal turbine; porous disc; tidal power; horizontal axis tidal turbine; 2D hydrodynamic coefficients; blockage effect; free surface effect; foundations; tip vortex; blade design

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APA (6th Edition):

Franchini, I. (2016). Experimental studies of a small scale horizontal axis tidal turbine. (Masters Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/7625

Chicago Manual of Style (16th Edition):

Franchini, Italo. “Experimental studies of a small scale horizontal axis tidal turbine.” 2016. Masters Thesis, University of Victoria. Accessed September 30, 2020. http://hdl.handle.net/1828/7625.

MLA Handbook (7th Edition):

Franchini, Italo. “Experimental studies of a small scale horizontal axis tidal turbine.” 2016. Web. 30 Sep 2020.

Vancouver:

Franchini I. Experimental studies of a small scale horizontal axis tidal turbine. [Internet] [Masters thesis]. University of Victoria; 2016. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/1828/7625.

Council of Science Editors:

Franchini I. Experimental studies of a small scale horizontal axis tidal turbine. [Masters Thesis]. University of Victoria; 2016. Available from: http://hdl.handle.net/1828/7625


Brno University of Technology

27. Kníř, Jakub. Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application.

Degree: 2018, Brno University of Technology

 This present thesis addresses the question whether it is possible to obtain compressor’s performance increase with the aid of flow numerical simulations. The main objective… (more)

Subjects/Keywords: tvarování štěrbiny skříně kompresoru; drážkování skříně; axiální kompresor; rotor 37; koncový vír; proudění ve štěrbině; casing treatment; casing grooves; axial compressor; rotor 37; tip vortex; leakage flow

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

APA (6th Edition):

Kníř, J. (2018). Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27613

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):

Kníř, Jakub. “Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application.” 2018. Thesis, Brno University of Technology. Accessed September 30, 2020. http://hdl.handle.net/11012/27613.

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

MLA Handbook (7th Edition):

Kníř, Jakub. “Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application.” 2018. Web. 30 Sep 2020.

Vancouver:

Kníř J. Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/11012/27613.

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

Council of Science Editors:

Kníř J. Parametrická studie vlivu tvaru štěrbiny mezi lopatkou rotoru turbíny a skříní motoru na aerodynamické vlastnosti rotoru: Parametric study of casing treatment for turbine blade in aero engine application. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/27613

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


University of Maryland

28. Duraisamy, Karthikeyan. Studies in Tip Vortex Formation, Evolution and Control.

Degree: Aerospace Engineering, 2005, University of Maryland

 A high resolution computational methodology is developed for the solution of the Compressible Reynolds Averaged Navier Stokes (RANS) equations. This methodology is used to study… (more)

Subjects/Keywords: Engineering, Aerospace; Tip vortex; RANS; flow control; Spanwise blowing; rotational correction

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

APA (6th Edition):

Duraisamy, K. (2005). Studies in Tip Vortex Formation, Evolution and Control. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/2372

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):

Duraisamy, Karthikeyan. “Studies in Tip Vortex Formation, Evolution and Control.” 2005. Thesis, University of Maryland. Accessed September 30, 2020. http://hdl.handle.net/1903/2372.

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

MLA Handbook (7th Edition):

Duraisamy, Karthikeyan. “Studies in Tip Vortex Formation, Evolution and Control.” 2005. Web. 30 Sep 2020.

Vancouver:

Duraisamy K. Studies in Tip Vortex Formation, Evolution and Control. [Internet] [Thesis]. University of Maryland; 2005. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/1903/2372.

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

Council of Science Editors:

Duraisamy K. Studies in Tip Vortex Formation, Evolution and Control. [Thesis]. University of Maryland; 2005. Available from: http://hdl.handle.net/1903/2372

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

29. Pentelow, Steffen L. Wing-tip Vortex Structure and Wandering .

Degree: 2014, University of Ottawa

 An isolated wing-tip vortex from a square-tipped NACA 0012 wing at an angle of attack of 5 degrees was studied in a water tunnel at… (more)

Subjects/Keywords: wing-tip vortex; trailing vortex; fluid dynamics; stereo particle image velocimetry; laser induced fluorescence; dye visualization; vortex wandering; vortex axis identification; vortex velocity profile; grid generated turbulence

…of wing-tip vortices have provided insights into wing-tip vortex structure and behaviour… …Experimental studies have consistently found that the path of a wing-tip vortex axis does not remain… …straight behind the wing-tip but bends as a result of what is termed vortex wandering. There is… …primary objective of this thesis was to study a wing-tip vortex under various freestream… …accomplish this, an isolated wing-tip vortex was investigated 1 2 in a water tunnel under three… 

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

APA (6th Edition):

Pentelow, S. L. (2014). Wing-tip Vortex Structure and Wandering . (Thesis). University of Ottawa. Retrieved from http://hdl.handle.net/10393/31114

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):

Pentelow, Steffen L. “Wing-tip Vortex Structure and Wandering .” 2014. Thesis, University of Ottawa. Accessed September 30, 2020. http://hdl.handle.net/10393/31114.

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

MLA Handbook (7th Edition):

Pentelow, Steffen L. “Wing-tip Vortex Structure and Wandering .” 2014. Web. 30 Sep 2020.

Vancouver:

Pentelow SL. Wing-tip Vortex Structure and Wandering . [Internet] [Thesis]. University of Ottawa; 2014. [cited 2020 Sep 30]. Available from: http://hdl.handle.net/10393/31114.

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

Council of Science Editors:

Pentelow SL. Wing-tip Vortex Structure and Wandering . [Thesis]. University of Ottawa; 2014. Available from: http://hdl.handle.net/10393/31114

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


Penn State University

30. Tallman, James Albert. A Computational Study of Tip Desensitization in Axial Flow Turbines.

Degree: 2008, Penn State University

 This study investigates the use of modified blade tip geometries as a means of reducing the leakage flow and vortex in axial flow turbine rotors.… (more)

Subjects/Keywords: Tip Treatment; Tip Desensitization; Leakage Vortex; Computational Fluid Dynamics; Turbine; Leakage Flow; Axial Flow Turbine

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

APA (6th Edition):

Tallman, J. A. (2008). A Computational Study of Tip Desensitization in Axial Flow Turbines. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/6034

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):

Tallman, James Albert. “A Computational Study of Tip Desensitization in Axial Flow Turbines.” 2008. Thesis, Penn State University. Accessed September 30, 2020. https://submit-etda.libraries.psu.edu/catalog/6034.

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

MLA Handbook (7th Edition):

Tallman, James Albert. “A Computational Study of Tip Desensitization in Axial Flow Turbines.” 2008. Web. 30 Sep 2020.

Vancouver:

Tallman JA. A Computational Study of Tip Desensitization in Axial Flow Turbines. [Internet] [Thesis]. Penn State University; 2008. [cited 2020 Sep 30]. Available from: https://submit-etda.libraries.psu.edu/catalog/6034.

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

Council of Science Editors:

Tallman JA. A Computational Study of Tip Desensitization in Axial Flow Turbines. [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/6034

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

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