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You searched for subject:(unsteady flow). Showing records 1 – 30 of 227 total matches.

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Rutgers University

1. Jujjavarapu, Pruthvi K., 1991-. Analysis of unsteady flows with vortex based method and N-S solver.

Degree: MS, Mechanical and Aerospace Engineering, 2016, Rutgers University

Unsteady flows are very common in nature. Birds, insects, fish and other animals predominantly rely on unsteady phenomena for locomotion. In the past century the… (more)

Subjects/Keywords: Unsteady flow (Aerodynamics)

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

APA (6th Edition):

Jujjavarapu, Pruthvi K., 1. (2016). Analysis of unsteady flows with vortex based method and N-S solver. (Masters Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/49243/

Chicago Manual of Style (16th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Masters Thesis, Rutgers University. Accessed January 21, 2020. https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

MLA Handbook (7th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Web. 21 Jan 2020.

Vancouver:

Jujjavarapu, Pruthvi K. 1. Analysis of unsteady flows with vortex based method and N-S solver. [Internet] [Masters thesis]. Rutgers University; 2016. [cited 2020 Jan 21]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

Council of Science Editors:

Jujjavarapu, Pruthvi K. 1. Analysis of unsteady flows with vortex based method and N-S solver. [Masters Thesis]. Rutgers University; 2016. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/49243/

2. Gong, Yanan. Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing.

Degree: 2014, University of Tennessee – Chattanooga

 A two-dimensional dynamic moving mesh algorithm is implemented for simulating aerodynamic oscillating airfoils. The airfoil is inserted into a uniform unstructured background mesh by exploiting… (more)

Subjects/Keywords: Aerofoils; Unsteady flow (Aerodynamics)

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APA (6th Edition):

Gong, Y. (2014). Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing. (Masters Thesis). University of Tennessee – Chattanooga. Retrieved from https://scholar.utc.edu/theses/152

Chicago Manual of Style (16th Edition):

Gong, Yanan. “Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing.” 2014. Masters Thesis, University of Tennessee – Chattanooga. Accessed January 21, 2020. https://scholar.utc.edu/theses/152.

MLA Handbook (7th Edition):

Gong, Yanan. “Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing.” 2014. Web. 21 Jan 2020.

Vancouver:

Gong Y. Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing. [Internet] [Masters thesis]. University of Tennessee – Chattanooga; 2014. [cited 2020 Jan 21]. Available from: https://scholar.utc.edu/theses/152.

Council of Science Editors:

Gong Y. Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing. [Masters Thesis]. University of Tennessee – Chattanooga; 2014. Available from: https://scholar.utc.edu/theses/152


Texas A&M University

3. Ozturk, Burak. Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade.

Degree: 2009, Texas A&M University

 Detailed experimental investigation has been conducted to provide a detailed insight into the heat transfer and aerodynamic behavior of a separation zone that is generated… (more)

Subjects/Keywords: unsteady boundary layer measurements; separation; reattachment; transition; unsteady wake flow

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APA (6th Edition):

Ozturk, B. (2009). Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1150

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):

Ozturk, Burak. “Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade.” 2009. Thesis, Texas A&M University. Accessed January 21, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1150.

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

MLA Handbook (7th Edition):

Ozturk, Burak. “Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade.” 2009. Web. 21 Jan 2020.

Vancouver:

Ozturk B. Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1150.

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

Council of Science Editors:

Ozturk B. Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1150

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


Texas A&M University

4. Weber, Jamie. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.

Degree: 2012, Texas A&M University

 Stochastic flow conditions, such as large unsteady wind gusts and coherent structures in turbulent winds, cause detrimental blade loadings to horizontal axis wind turbines (HAWT).… (more)

Subjects/Keywords: unsteady aerodynamics; flow control; wind turbine blade

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APA (6th Edition):

Weber, J. (2012). Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156350

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):

Weber, Jamie. “Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.” 2012. Thesis, Texas A&M University. Accessed January 21, 2020. http://hdl.handle.net/1969.1/156350.

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

MLA Handbook (7th Edition):

Weber, Jamie. “Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.” 2012. Web. 21 Jan 2020.

Vancouver:

Weber J. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/1969.1/156350.

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

Council of Science Editors:

Weber J. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/156350

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


Texas A&M University

5. Bertsch, Rebecca Lynne. Effect of Inhomogeneity and Unsteadiness on the Stability of High-Speed Shear Flows.

Degree: 2014, Texas A&M University

 In hypersonic flows, turbulence critically influences mass and momentum transport, mixing, heat transfer and acoustic noise generation. In contrast to incompressible flow, in high speed… (more)

Subjects/Keywords: High-speed; compressible; Shear flow; Inhomogeneous; Unsteady

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APA (6th Edition):

Bertsch, R. L. (2014). Effect of Inhomogeneity and Unsteadiness on the Stability of High-Speed Shear Flows. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153368

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):

Bertsch, Rebecca Lynne. “Effect of Inhomogeneity and Unsteadiness on the Stability of High-Speed Shear Flows.” 2014. Thesis, Texas A&M University. Accessed January 21, 2020. http://hdl.handle.net/1969.1/153368.

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

MLA Handbook (7th Edition):

Bertsch, Rebecca Lynne. “Effect of Inhomogeneity and Unsteadiness on the Stability of High-Speed Shear Flows.” 2014. Web. 21 Jan 2020.

Vancouver:

Bertsch RL. Effect of Inhomogeneity and Unsteadiness on the Stability of High-Speed Shear Flows. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/1969.1/153368.

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

Council of Science Editors:

Bertsch RL. Effect of Inhomogeneity and Unsteadiness on the Stability of High-Speed Shear Flows. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153368

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


University of Victoria

6. Stockdill, Barton Thomas. Turbulence modelling of unsteady separated flow over an airfoil.

Degree: Dept. of Mechanical Engineering, 2008, University of Victoria

Subjects/Keywords: Unsteady flow (Aerodynamics)

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APA (6th Edition):

Stockdill, B. T. (2008). Turbulence modelling of unsteady separated flow over an airfoil. (Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/384

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):

Stockdill, Barton Thomas. “Turbulence modelling of unsteady separated flow over an airfoil.” 2008. Thesis, University of Victoria. Accessed January 21, 2020. http://hdl.handle.net/1828/384.

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

MLA Handbook (7th Edition):

Stockdill, Barton Thomas. “Turbulence modelling of unsteady separated flow over an airfoil.” 2008. Web. 21 Jan 2020.

Vancouver:

Stockdill BT. Turbulence modelling of unsteady separated flow over an airfoil. [Internet] [Thesis]. University of Victoria; 2008. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/1828/384.

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

Council of Science Editors:

Stockdill BT. Turbulence modelling of unsteady separated flow over an airfoil. [Thesis]. University of Victoria; 2008. Available from: http://hdl.handle.net/1828/384

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


Rutgers University

7. Villegas Vaquero, Arturo. Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition.

Degree: Mechanical and Aerospace Engineering, 2014, Rutgers University

Subjects/Keywords: Unsteady flow (Aerodynamics)

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APA (6th Edition):

Villegas Vaquero, A. (2014). Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition. (Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/44255/

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):

Villegas Vaquero, Arturo. “Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition.” 2014. Thesis, Rutgers University. Accessed January 21, 2020. https://rucore.libraries.rutgers.edu/rutgers-lib/44255/.

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

MLA Handbook (7th Edition):

Villegas Vaquero, Arturo. “Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition.” 2014. Web. 21 Jan 2020.

Vancouver:

Villegas Vaquero A. Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition. [Internet] [Thesis]. Rutgers University; 2014. [cited 2020 Jan 21]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/44255/.

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

Council of Science Editors:

Villegas Vaquero A. Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition. [Thesis]. Rutgers University; 2014. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/44255/

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


University of Arizona

8. Agate, Mark. Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall .

Degree: 2018, University of Arizona

 An investigation of laminar separation bubble behavior on an oscillating X-56A wing section has been performed experimentally at Reynolds number 200,000. Wind tunnel results along… (more)

Subjects/Keywords: Laminar separation bubble; Plunging airfoil; Unsteady flow

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APA (6th Edition):

Agate, M. (2018). Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/630558

Chicago Manual of Style (16th Edition):

Agate, Mark. “Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall .” 2018. Masters Thesis, University of Arizona. Accessed January 21, 2020. http://hdl.handle.net/10150/630558.

MLA Handbook (7th Edition):

Agate, Mark. “Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall .” 2018. Web. 21 Jan 2020.

Vancouver:

Agate M. Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10150/630558.

Council of Science Editors:

Agate M. Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall . [Masters Thesis]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/630558


Indian Institute of Science

9. Ramkrishna, Joshi Pranav. Unsteady Flow Field Downstream Of A Sudden Expansion.

Degree: 2006, Indian Institute of Science

 Separating and reattaching flows are important in a large number of engineering configurations. The flow through a sudden expansion (backward-facing step) represents a conceptually simple… (more)

Subjects/Keywords: Unsteady Flow; Instrumentation; Turbulence; Shear Flow; Shear Layer Instability; Fluid Dynamics; Unsteady Flow Field; Expansion Ratio; Fluid Mechanics

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APA (6th Edition):

Ramkrishna, J. P. (2006). Unsteady Flow Field Downstream Of A Sudden Expansion. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/447

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):

Ramkrishna, Joshi Pranav. “Unsteady Flow Field Downstream Of A Sudden Expansion.” 2006. Thesis, Indian Institute of Science. Accessed January 21, 2020. http://hdl.handle.net/2005/447.

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

MLA Handbook (7th Edition):

Ramkrishna, Joshi Pranav. “Unsteady Flow Field Downstream Of A Sudden Expansion.” 2006. Web. 21 Jan 2020.

Vancouver:

Ramkrishna JP. Unsteady Flow Field Downstream Of A Sudden Expansion. [Internet] [Thesis]. Indian Institute of Science; 2006. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/2005/447.

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

Council of Science Editors:

Ramkrishna JP. Unsteady Flow Field Downstream Of A Sudden Expansion. [Thesis]. Indian Institute of Science; 2006. Available from: http://hdl.handle.net/2005/447

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


University of Illinois – Urbana-Champaign

10. Gupta, Rohit. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.

Degree: MS, Aerospace Engineering, 2016, University of Illinois – Urbana-Champaign

 Active Unsteady Flow Control experiments were performed on a Natural Laminar Flow, NLF 0414 airfoil at Re = 1.0 × 10(6) in a 3-ft ×… (more)

Subjects/Keywords: Unsteady Aerodynamics; Active Flow Control; Natural Laminar Flow; Particle Image Velocimetry

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APA (6th Edition):

Gupta, R. (2016). Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/92747

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):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Thesis, University of Illinois – Urbana-Champaign. Accessed January 21, 2020. http://hdl.handle.net/2142/92747.

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

MLA Handbook (7th Edition):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Web. 21 Jan 2020.

Vancouver:

Gupta R. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2016. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/2142/92747.

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

Council of Science Editors:

Gupta R. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. [Thesis]. University of Illinois – Urbana-Champaign; 2016. Available from: http://hdl.handle.net/2142/92747

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


Virginia Tech

11. Laadj, Toufik. Initial Value Problems for Creeping Flow of Maxwell Fluids.

Degree: PhD, Mathematics, 2011, Virginia Tech

 We consider the flow of nonlinear Maxwell fluids in the unsteady quasistatic case, where the effect of inertia is neglected. We study the well-posedness of… (more)

Subjects/Keywords: nonlinear Maxwell fluid; unsteady flow; existence and uniqueness; Quasistatic viscoelastic flow

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APA (6th Edition):

Laadj, T. (2011). Initial Value Problems for Creeping Flow of Maxwell Fluids. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/26302

Chicago Manual of Style (16th Edition):

Laadj, Toufik. “Initial Value Problems for Creeping Flow of Maxwell Fluids.” 2011. Doctoral Dissertation, Virginia Tech. Accessed January 21, 2020. http://hdl.handle.net/10919/26302.

MLA Handbook (7th Edition):

Laadj, Toufik. “Initial Value Problems for Creeping Flow of Maxwell Fluids.” 2011. Web. 21 Jan 2020.

Vancouver:

Laadj T. Initial Value Problems for Creeping Flow of Maxwell Fluids. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10919/26302.

Council of Science Editors:

Laadj T. Initial Value Problems for Creeping Flow of Maxwell Fluids. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/26302


University of Tennessee – Knoxville

12. Sharkey, Jennifer Kay. Investigating Instabilities with HEC-RAS Unsteady Flow Modeling for Regulated Rivers at Low Flow Stages.

Degree: MS, Environmental Engineering, 2014, University of Tennessee – Knoxville

  Dams are used throughout the United States for generation of electricity and flood control. The Tennessee River Valley’s regulated river system extends through Tennessee… (more)

Subjects/Keywords: unsteady; flow; modeling; HEC-RAS; low flow; regulated; Hydraulic Engineering

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APA (6th Edition):

Sharkey, J. K. (2014). Investigating Instabilities with HEC-RAS Unsteady Flow Modeling for Regulated Rivers at Low Flow Stages. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/3183

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):

Sharkey, Jennifer Kay. “Investigating Instabilities with HEC-RAS Unsteady Flow Modeling for Regulated Rivers at Low Flow Stages.” 2014. Thesis, University of Tennessee – Knoxville. Accessed January 21, 2020. https://trace.tennessee.edu/utk_gradthes/3183.

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

MLA Handbook (7th Edition):

Sharkey, Jennifer Kay. “Investigating Instabilities with HEC-RAS Unsteady Flow Modeling for Regulated Rivers at Low Flow Stages.” 2014. Web. 21 Jan 2020.

Vancouver:

Sharkey JK. Investigating Instabilities with HEC-RAS Unsteady Flow Modeling for Regulated Rivers at Low Flow Stages. [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2020 Jan 21]. Available from: https://trace.tennessee.edu/utk_gradthes/3183.

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

Council of Science Editors:

Sharkey JK. Investigating Instabilities with HEC-RAS Unsteady Flow Modeling for Regulated Rivers at Low Flow Stages. [Thesis]. University of Tennessee – Knoxville; 2014. Available from: https://trace.tennessee.edu/utk_gradthes/3183

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


University of Wollongong

13. Al-Fadhli, Ishraq Hamdan. Turbulence characteristics in unsteady and non-uniform flows and their impacts on the incipient motion of sediment transport-water resources-river mechanics.

Degree: Master of Engineering - Research, 2013, University of Wollongong

  This study investigates turbulence characteristics in steady and unsteady non-uniform flows and how these flows affect the incipient motion of sediment transport. Specifically, it… (more)

Subjects/Keywords: incipient sediment motion; unsteady/stready flow; non-uniform flow

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APA (6th Edition):

Al-Fadhli, I. H. (2013). Turbulence characteristics in unsteady and non-uniform flows and their impacts on the incipient motion of sediment transport-water resources-river mechanics. (Masters Thesis). University of Wollongong. Retrieved from 090101 Aerodynamics (excl. Hypersonic Aerodynamics) ; https://ro.uow.edu.au/theses/3907

Chicago Manual of Style (16th Edition):

Al-Fadhli, Ishraq Hamdan. “Turbulence characteristics in unsteady and non-uniform flows and their impacts on the incipient motion of sediment transport-water resources-river mechanics.” 2013. Masters Thesis, University of Wollongong. Accessed January 21, 2020. 090101 Aerodynamics (excl. Hypersonic Aerodynamics) ; https://ro.uow.edu.au/theses/3907.

MLA Handbook (7th Edition):

Al-Fadhli, Ishraq Hamdan. “Turbulence characteristics in unsteady and non-uniform flows and their impacts on the incipient motion of sediment transport-water resources-river mechanics.” 2013. Web. 21 Jan 2020.

Vancouver:

Al-Fadhli IH. Turbulence characteristics in unsteady and non-uniform flows and their impacts on the incipient motion of sediment transport-water resources-river mechanics. [Internet] [Masters thesis]. University of Wollongong; 2013. [cited 2020 Jan 21]. Available from: 090101 Aerodynamics (excl. Hypersonic Aerodynamics) ; https://ro.uow.edu.au/theses/3907.

Council of Science Editors:

Al-Fadhli IH. Turbulence characteristics in unsteady and non-uniform flows and their impacts on the incipient motion of sediment transport-water resources-river mechanics. [Masters Thesis]. University of Wollongong; 2013. Available from: 090101 Aerodynamics (excl. Hypersonic Aerodynamics) ; https://ro.uow.edu.au/theses/3907


University of Texas – Austin

14. -4399-6341. Brownian motion in liquids : theory and experiment.

Degree: PhD, Physics, 2017, University of Texas – Austin

 Since the theoretical work of Einstein [1905] and von Smoluckowski [1906], and the experiments of Perrin [1909], Brownian motion at long time-scales has been extensively… (more)

Subjects/Keywords: Brownian motion; Unsteady Stokes flow; Low Reynolds number flow

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APA (6th Edition):

-4399-6341. (2017). Brownian motion in liquids : theory and experiment. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/63654

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

Chicago Manual of Style (16th Edition):

-4399-6341. “Brownian motion in liquids : theory and experiment.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed January 21, 2020. http://hdl.handle.net/2152/63654.

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

MLA Handbook (7th Edition):

-4399-6341. “Brownian motion in liquids : theory and experiment.” 2017. Web. 21 Jan 2020.

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

Vancouver:

-4399-6341. Brownian motion in liquids : theory and experiment. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/2152/63654.

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

Council of Science Editors:

-4399-6341. Brownian motion in liquids : theory and experiment. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/63654

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


University of Windsor

15. Hannoura, Abdel-Alim Aly. Numerical and experimental modelling of unsteady flow in rockfill embankments.

Degree: PhD, Civil and Environmental Engineering, 1972, University of Windsor

Subjects/Keywords: EMBANKMENTS; EXPERIMENTAL; Embankments; FLOW; MODELLING; NUMERICAL; ROCKFILL; Rockfill; UNSTEADY; UNSTEADY FLOW; Unsteady flow

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APA (6th Edition):

Hannoura, A. A. (1972). Numerical and experimental modelling of unsteady flow in rockfill embankments. (Doctoral Dissertation). University of Windsor. Retrieved from https://scholar.uwindsor.ca/etd/6115

Chicago Manual of Style (16th Edition):

Hannoura, Abdel-Alim Aly. “Numerical and experimental modelling of unsteady flow in rockfill embankments.” 1972. Doctoral Dissertation, University of Windsor. Accessed January 21, 2020. https://scholar.uwindsor.ca/etd/6115.

MLA Handbook (7th Edition):

Hannoura, Abdel-Alim Aly. “Numerical and experimental modelling of unsteady flow in rockfill embankments.” 1972. Web. 21 Jan 2020.

Vancouver:

Hannoura AA. Numerical and experimental modelling of unsteady flow in rockfill embankments. [Internet] [Doctoral dissertation]. University of Windsor; 1972. [cited 2020 Jan 21]. Available from: https://scholar.uwindsor.ca/etd/6115.

Council of Science Editors:

Hannoura AA. Numerical and experimental modelling of unsteady flow in rockfill embankments. [Doctoral Dissertation]. University of Windsor; 1972. Available from: https://scholar.uwindsor.ca/etd/6115


Texas Tech University

16. -8727-4981. Impedance of circular tubes with slowly varying cross-sections for unsteady laminar flow.

Degree: MSin Mechanical Engineering, Mechanical Engineering, 2017, Texas Tech University

 This thesis describes the resistance and the phase lag for an unsteady flow driven by a sinusoidally fluctuating pressure difference inside a rigid circular channel… (more)

Subjects/Keywords: Unsteady transport; channel flow; axially varying cross-section; conduit impedance; laminar flow; pipe flow

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APA (6th Edition):

-8727-4981. (2017). Impedance of circular tubes with slowly varying cross-sections for unsteady laminar flow. (Masters Thesis). Texas Tech University. Retrieved from http://hdl.handle.net/2346/82045

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

Chicago Manual of Style (16th Edition):

-8727-4981. “Impedance of circular tubes with slowly varying cross-sections for unsteady laminar flow.” 2017. Masters Thesis, Texas Tech University. Accessed January 21, 2020. http://hdl.handle.net/2346/82045.

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

MLA Handbook (7th Edition):

-8727-4981. “Impedance of circular tubes with slowly varying cross-sections for unsteady laminar flow.” 2017. Web. 21 Jan 2020.

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

Vancouver:

-8727-4981. Impedance of circular tubes with slowly varying cross-sections for unsteady laminar flow. [Internet] [Masters thesis]. Texas Tech University; 2017. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/2346/82045.

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

Council of Science Editors:

-8727-4981. Impedance of circular tubes with slowly varying cross-sections for unsteady laminar flow. [Masters Thesis]. Texas Tech University; 2017. Available from: http://hdl.handle.net/2346/82045

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


University of New Mexico

17. White, Ross. Oblique shock interactions with gas cylinder interfaces.

Degree: Mechanical Engineering, 2012, University of New Mexico

 This thesis presents an experimental study of fluid instabilities formed due to an oblique interatction of a shock wave with a cylindrical gas column seeded… (more)

Subjects/Keywords: Unsteady flow (Fluid dynamics); Shock (Mechanics); Gas tubes.

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APA (6th Edition):

White, R. (2012). Oblique shock interactions with gas cylinder interfaces. (Masters Thesis). University of New Mexico. Retrieved from http://hdl.handle.net/1928/21012

Chicago Manual of Style (16th Edition):

White, Ross. “Oblique shock interactions with gas cylinder interfaces.” 2012. Masters Thesis, University of New Mexico. Accessed January 21, 2020. http://hdl.handle.net/1928/21012.

MLA Handbook (7th Edition):

White, Ross. “Oblique shock interactions with gas cylinder interfaces.” 2012. Web. 21 Jan 2020.

Vancouver:

White R. Oblique shock interactions with gas cylinder interfaces. [Internet] [Masters thesis]. University of New Mexico; 2012. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/1928/21012.

Council of Science Editors:

White R. Oblique shock interactions with gas cylinder interfaces. [Masters Thesis]. University of New Mexico; 2012. Available from: http://hdl.handle.net/1928/21012


North Carolina State University

18. McMullan, Richard Jeffrey. Numerical Boundary Conditions Simulating the Interaction Between Upstream Disturbances and an Axial Compressor.

Degree: PhD, Aerospace Engineering, 2002, North Carolina State University

 New small disturbance and area reduction compressor face boundary conditions that model the unsteady interactions of acoustic disturbances with an axial compressor are presented. The… (more)

Subjects/Keywords: computational fluid dynamics; unsteady flow

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APA (6th Edition):

McMullan, R. J. (2002). Numerical Boundary Conditions Simulating the Interaction Between Upstream Disturbances and an Axial Compressor. (Doctoral Dissertation). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/4436

Chicago Manual of Style (16th Edition):

McMullan, Richard Jeffrey. “Numerical Boundary Conditions Simulating the Interaction Between Upstream Disturbances and an Axial Compressor.” 2002. Doctoral Dissertation, North Carolina State University. Accessed January 21, 2020. http://www.lib.ncsu.edu/resolver/1840.16/4436.

MLA Handbook (7th Edition):

McMullan, Richard Jeffrey. “Numerical Boundary Conditions Simulating the Interaction Between Upstream Disturbances and an Axial Compressor.” 2002. Web. 21 Jan 2020.

Vancouver:

McMullan RJ. Numerical Boundary Conditions Simulating the Interaction Between Upstream Disturbances and an Axial Compressor. [Internet] [Doctoral dissertation]. North Carolina State University; 2002. [cited 2020 Jan 21]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/4436.

Council of Science Editors:

McMullan RJ. Numerical Boundary Conditions Simulating the Interaction Between Upstream Disturbances and an Axial Compressor. [Doctoral Dissertation]. North Carolina State University; 2002. Available from: http://www.lib.ncsu.edu/resolver/1840.16/4436


University of Notre Dame

19. David M Schatzman. A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2011, University of Notre Dame

  An experimental investigation focused on the study of the physics of unsteady turbulent boundary layer separation under conditions relevant to the dynamic stall process… (more)

Subjects/Keywords: plasma; unsteady; turbulence; boundary layers; flow control; separation

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APA (6th Edition):

Schatzman, D. M. (2011). A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/cf95j96242f

Chicago Manual of Style (16th Edition):

Schatzman, David M. “A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics</h1>.” 2011. Doctoral Dissertation, University of Notre Dame. Accessed January 21, 2020. https://curate.nd.edu/show/cf95j96242f.

MLA Handbook (7th Edition):

Schatzman, David M. “A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics</h1>.” 2011. Web. 21 Jan 2020.

Vancouver:

Schatzman DM. A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2011. [cited 2020 Jan 21]. Available from: https://curate.nd.edu/show/cf95j96242f.

Council of Science Editors:

Schatzman DM. A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics</h1>. [Doctoral Dissertation]. University of Notre Dame; 2011. Available from: https://curate.nd.edu/show/cf95j96242f

20. 田中, 誠一. ディフューザ型バルブレスマイクロポンプに関する研究 : A Study of the diffuser/nozzle based valveless micropump.

Degree: 博士(工学), 2017, Kyushu Institute of Technology / 九州工業大学

九州工業大学博士学位論文 学位記番号:生工博甲第105号 学位授与年月日:平成21年3月25日

第1 章序論|第2 章実験|第3 章理論解析|第4 章考察|第5 章結論|付録A

平成20年度

Advisors/Committee Members: 塚本, 寛.

Subjects/Keywords: Micropump; Micro fluid; Unsteady flow; Valveless micropump; CFD

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APA (6th Edition):

田中, . (2017). ディフューザ型バルブレスマイクロポンプに関する研究 : A Study of the diffuser/nozzle based valveless micropump. (Thesis). Kyushu Institute of Technology / 九州工業大学. Retrieved from http://hdl.handle.net/10228/2552

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):

田中, 誠一. “ディフューザ型バルブレスマイクロポンプに関する研究 : A Study of the diffuser/nozzle based valveless micropump.” 2017. Thesis, Kyushu Institute of Technology / 九州工業大学. Accessed January 21, 2020. http://hdl.handle.net/10228/2552.

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

MLA Handbook (7th Edition):

田中, 誠一. “ディフューザ型バルブレスマイクロポンプに関する研究 : A Study of the diffuser/nozzle based valveless micropump.” 2017. Web. 21 Jan 2020.

Vancouver:

田中 . ディフューザ型バルブレスマイクロポンプに関する研究 : A Study of the diffuser/nozzle based valveless micropump. [Internet] [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. [cited 2020 Jan 21]. Available from: http://hdl.handle.net/10228/2552.

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

Council of Science Editors:

田中 . ディフューザ型バルブレスマイクロポンプに関する研究 : A Study of the diffuser/nozzle based valveless micropump. [Thesis]. Kyushu Institute of Technology / 九州工業大学; 2017. Available from: http://hdl.handle.net/10228/2552

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


University of Southern California

21. Kim, Hyoung-Jin. Numerical and experimental study on dynamics of unsteady pipe flow involving backflow prevention assemblies.

Degree: PhD, Civil Engineering, 2012, University of Southern California

 When control valves at the end of pipeline close simultaneously, two pressure waves are generated at each end and the waves propagate toward to the… (more)

Subjects/Keywords: unsteady pipe flow; water hammer; backflow prevention assemblies

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APA (6th Edition):

Kim, H. (2012). Numerical and experimental study on dynamics of unsteady pipe flow involving backflow prevention assemblies. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/116209/rec/4479

Chicago Manual of Style (16th Edition):

Kim, Hyoung-Jin. “Numerical and experimental study on dynamics of unsteady pipe flow involving backflow prevention assemblies.” 2012. Doctoral Dissertation, University of Southern California. Accessed January 21, 2020. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/116209/rec/4479.

MLA Handbook (7th Edition):

Kim, Hyoung-Jin. “Numerical and experimental study on dynamics of unsteady pipe flow involving backflow prevention assemblies.” 2012. Web. 21 Jan 2020.

Vancouver:

Kim H. Numerical and experimental study on dynamics of unsteady pipe flow involving backflow prevention assemblies. [Internet] [Doctoral dissertation]. University of Southern California; 2012. [cited 2020 Jan 21]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/116209/rec/4479.

Council of Science Editors:

Kim H. Numerical and experimental study on dynamics of unsteady pipe flow involving backflow prevention assemblies. [Doctoral Dissertation]. University of Southern California; 2012. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/116209/rec/4479

22. Liu, Chao. A stabilized finite element dynamic overset method for the Navier-Stokes equations.

Degree: 2016, University of Tennessee – Chattanooga

 In terms of mesh resolution requirements, higher-order finite element discretization methods offer a more economic means of obtaining accurate simulations and/or to resolve physics at… (more)

Subjects/Keywords: Navier-Stokes equations  – Numerical solutions; Unsteady flow (Aerodynamics)

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APA (6th Edition):

Liu, C. (2016). A stabilized finite element dynamic overset method for the Navier-Stokes equations. (Doctoral Dissertation). University of Tennessee – Chattanooga. Retrieved from https://scholar.utc.edu/theses/458

Chicago Manual of Style (16th Edition):

Liu, Chao. “A stabilized finite element dynamic overset method for the Navier-Stokes equations.” 2016. Doctoral Dissertation, University of Tennessee – Chattanooga. Accessed January 21, 2020. https://scholar.utc.edu/theses/458.

MLA Handbook (7th Edition):

Liu, Chao. “A stabilized finite element dynamic overset method for the Navier-Stokes equations.” 2016. Web. 21 Jan 2020.

Vancouver:

Liu C. A stabilized finite element dynamic overset method for the Navier-Stokes equations. [Internet] [Doctoral dissertation]. University of Tennessee – Chattanooga; 2016. [cited 2020 Jan 21]. Available from: https://scholar.utc.edu/theses/458.

Council of Science Editors:

Liu C. A stabilized finite element dynamic overset method for the Navier-Stokes equations. [Doctoral Dissertation]. University of Tennessee – Chattanooga; 2016. Available from: https://scholar.utc.edu/theses/458


Clemson University

23. Schillinger, Mark. Temporal Pier Scour Evolution under Stepped Hydrographs.

Degree: MS, Civil Engineering, 2011, Clemson University

 The present study was aimed at measuring the scour hole profile at bridge piers under clear water scour. Scour tests were performed under both steady… (more)

Subjects/Keywords: Bridges; Clear Water; Piers; Scour; Sediment; Unsteady Flow; Civil Engineering

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APA (6th Edition):

Schillinger, M. (2011). Temporal Pier Scour Evolution under Stepped Hydrographs. (Masters Thesis). Clemson University. Retrieved from https://tigerprints.clemson.edu/all_theses/1225

Chicago Manual of Style (16th Edition):

Schillinger, Mark. “Temporal Pier Scour Evolution under Stepped Hydrographs.” 2011. Masters Thesis, Clemson University. Accessed January 21, 2020. https://tigerprints.clemson.edu/all_theses/1225.

MLA Handbook (7th Edition):

Schillinger, Mark. “Temporal Pier Scour Evolution under Stepped Hydrographs.” 2011. Web. 21 Jan 2020.

Vancouver:

Schillinger M. Temporal Pier Scour Evolution under Stepped Hydrographs. [Internet] [Masters thesis]. Clemson University; 2011. [cited 2020 Jan 21]. Available from: https://tigerprints.clemson.edu/all_theses/1225.

Council of Science Editors:

Schillinger M. Temporal Pier Scour Evolution under Stepped Hydrographs. [Masters Thesis]. Clemson University; 2011. Available from: https://tigerprints.clemson.edu/all_theses/1225


University of New South Wales

24. Wu, Chaofan. Jet oscillation applied for aircraft cabin ventilation using active flow control actuators.

Degree: Mechanical & Manufacturing Engineering, 2014, University of New South Wales

 Maintaining a healthy cabin environment during flight relies on continual extraction of fresh air from the engine. To meet passengers' expectation for more comfortable cabin… (more)

Subjects/Keywords: Unsteady air supply; Synthetic jet; Active flow control

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APA (6th Edition):

Wu, C. (2014). Jet oscillation applied for aircraft cabin ventilation using active flow control actuators. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/53544 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12239/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Wu, Chaofan. “Jet oscillation applied for aircraft cabin ventilation using active flow control actuators.” 2014. Doctoral Dissertation, University of New South Wales. Accessed January 21, 2020. http://handle.unsw.edu.au/1959.4/53544 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12239/SOURCE02?view=true.

MLA Handbook (7th Edition):

Wu, Chaofan. “Jet oscillation applied for aircraft cabin ventilation using active flow control actuators.” 2014. Web. 21 Jan 2020.

Vancouver:

Wu C. Jet oscillation applied for aircraft cabin ventilation using active flow control actuators. [Internet] [Doctoral dissertation]. University of New South Wales; 2014. [cited 2020 Jan 21]. Available from: http://handle.unsw.edu.au/1959.4/53544 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12239/SOURCE02?view=true.

Council of Science Editors:

Wu C. Jet oscillation applied for aircraft cabin ventilation using active flow control actuators. [Doctoral Dissertation]. University of New South Wales; 2014. Available from: http://handle.unsw.edu.au/1959.4/53544 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12239/SOURCE02?view=true


Queen Mary, University of London

25. Baral, Bishnu Raj. Numerical modelling of braiding processes in gravel-bed rivers.

Degree: PhD, 2018, Queen Mary, University of London

 Gravel bed braided rivers are distinctive natural environments that provide a wide range of key environmental, economic and recreational services. There is, however, a growing… (more)

Subjects/Keywords: Braiding processes; Gravel-bed rivers; Numerical modelling; Unsteady flow; Vegetation; BASEMENT

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APA (6th Edition):

Baral, B. R. (2018). Numerical modelling of braiding processes in gravel-bed rivers. (Doctoral Dissertation). Queen Mary, University of London. Retrieved from http://qmro.qmul.ac.uk/xmlui/handle/123456789/44686 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.766212

Chicago Manual of Style (16th Edition):

Baral, Bishnu Raj. “Numerical modelling of braiding processes in gravel-bed rivers.” 2018. Doctoral Dissertation, Queen Mary, University of London. Accessed January 21, 2020. http://qmro.qmul.ac.uk/xmlui/handle/123456789/44686 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.766212.

MLA Handbook (7th Edition):

Baral, Bishnu Raj. “Numerical modelling of braiding processes in gravel-bed rivers.” 2018. Web. 21 Jan 2020.

Vancouver:

Baral BR. Numerical modelling of braiding processes in gravel-bed rivers. [Internet] [Doctoral dissertation]. Queen Mary, University of London; 2018. [cited 2020 Jan 21]. Available from: http://qmro.qmul.ac.uk/xmlui/handle/123456789/44686 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.766212.

Council of Science Editors:

Baral BR. Numerical modelling of braiding processes in gravel-bed rivers. [Doctoral Dissertation]. Queen Mary, University of London; 2018. Available from: http://qmro.qmul.ac.uk/xmlui/handle/123456789/44686 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.766212


Florida Atlantic University

26. Finkel, Cyndee L. Synchronization and phase dynamics of oscillating foils.

Degree: PhD, 2013, Florida Atlantic University

Summary: In this work, a two-dimensional model representing the vortices that animals produce, when they are flying/swimming, was constructed. A D{shaped cylinder and an oscillating… (more)

Subjects/Keywords: Mathematical physics; Fluid dynamics; Unsteady flow (Fluid dynamics); Aerofoils; Aerodynamics

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APA (6th Edition):

Finkel, C. L. (2013). Synchronization and phase dynamics of oscillating foils. (Doctoral Dissertation). Florida Atlantic University. Retrieved from http://purl.flvc.org/fcla/dt/3362333

Chicago Manual of Style (16th Edition):

Finkel, Cyndee L. “Synchronization and phase dynamics of oscillating foils.” 2013. Doctoral Dissertation, Florida Atlantic University. Accessed January 21, 2020. http://purl.flvc.org/fcla/dt/3362333.

MLA Handbook (7th Edition):

Finkel, Cyndee L. “Synchronization and phase dynamics of oscillating foils.” 2013. Web. 21 Jan 2020.

Vancouver:

Finkel CL. Synchronization and phase dynamics of oscillating foils. [Internet] [Doctoral dissertation]. Florida Atlantic University; 2013. [cited 2020 Jan 21]. Available from: http://purl.flvc.org/fcla/dt/3362333.

Council of Science Editors:

Finkel CL. Synchronization and phase dynamics of oscillating foils. [Doctoral Dissertation]. Florida Atlantic University; 2013. Available from: http://purl.flvc.org/fcla/dt/3362333


University of Texas – Austin

27. -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 January 21, 2020. 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. 21 Jan 2020.

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 2020 Jan 21]. 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


Wright State University

28. Nessler, Chase A. Characterization of Internal Wake Generator at Low Reynolds Number with a Linear Cascade of Low Pressure Turbine Blades.

Degree: MSEgr, Mechanical Engineering, 2010, Wright State University

Unsteady flow and its effects on the boundary layer of a low pressure turbine blade is complex in nature. The flow encountered in a… (more)

Subjects/Keywords: Engineering; Fluid Dynamics; Mechanical Engineering; Technology; low pressure turbine; unsteady flow; wake generator; unsteady wakes; particle image velocimetry; L1A

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APA (6th Edition):

Nessler, C. A. (2010). Characterization of Internal Wake Generator at Low Reynolds Number with a Linear Cascade of Low Pressure Turbine Blades. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1270749309

Chicago Manual of Style (16th Edition):

Nessler, Chase A. “Characterization of Internal Wake Generator at Low Reynolds Number with a Linear Cascade of Low Pressure Turbine Blades.” 2010. Masters Thesis, Wright State University. Accessed January 21, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=wright1270749309.

MLA Handbook (7th Edition):

Nessler, Chase A. “Characterization of Internal Wake Generator at Low Reynolds Number with a Linear Cascade of Low Pressure Turbine Blades.” 2010. Web. 21 Jan 2020.

Vancouver:

Nessler CA. Characterization of Internal Wake Generator at Low Reynolds Number with a Linear Cascade of Low Pressure Turbine Blades. [Internet] [Masters thesis]. Wright State University; 2010. [cited 2020 Jan 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1270749309.

Council of Science Editors:

Nessler CA. Characterization of Internal Wake Generator at Low Reynolds Number with a Linear Cascade of Low Pressure Turbine Blades. [Masters Thesis]. Wright State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1270749309


University of Florida

29. Hart, Adam Benjamin. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 Natural fliers have shown the capability to utilize unsteady fluid phenomena to increase their flight performance. As engineered vehicles operating in equivalent flight regimes are… (more)

Subjects/Keywords: Aerodynamic lift; Aerodynamics; Aircraft wings; Angle of attack; Flow distribution; Kinematics; Leading edges; Momentum; Unsteady aerodynamics; Velocity; aerodynamics  – piv  – unsteady

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

APA (6th Edition):

Hart, A. B. (2013). Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045179

Chicago Manual of Style (16th Edition):

Hart, Adam Benjamin. “Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.” 2013. Doctoral Dissertation, University of Florida. Accessed January 21, 2020. http://ufdc.ufl.edu/UFE0045179.

MLA Handbook (7th Edition):

Hart, Adam Benjamin. “Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.” 2013. Web. 21 Jan 2020.

Vancouver:

Hart AB. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2020 Jan 21]. Available from: http://ufdc.ufl.edu/UFE0045179.

Council of Science Editors:

Hart AB. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045179

30. Calderón, Raúl. Modélisation des efforts aérodynamiques instationnaires pour la prévision du phénomène de tremblement sur des avions civils : Modelling unsteady aerodynamics loads for buffeting prediction on civil aircrafts.

Degree: Docteur es, Dynamique des fluides, 2014, Toulouse, ISAE

Le tremblement est un phénomène qui touche diverses parties de l'avion, pouvant créer des problèmes de fatigue structurelle ou de confort et limiter l'enveloppe de… (more)

Subjects/Keywords: Tremblement; Instationnaire; Décollement; Aérodynamique; Effort instationnaire; Modélisation; Buffeting; Unsteady; Flow separation; Aerodynamic; Unsteady force; Modelling; 532

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

APA (6th Edition):

Calderón, R. (2014). Modélisation des efforts aérodynamiques instationnaires pour la prévision du phénomène de tremblement sur des avions civils : Modelling unsteady aerodynamics loads for buffeting prediction on civil aircrafts. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2014ESAE0005

Chicago Manual of Style (16th Edition):

Calderón, Raúl. “Modélisation des efforts aérodynamiques instationnaires pour la prévision du phénomène de tremblement sur des avions civils : Modelling unsteady aerodynamics loads for buffeting prediction on civil aircrafts.” 2014. Doctoral Dissertation, Toulouse, ISAE. Accessed January 21, 2020. http://www.theses.fr/2014ESAE0005.

MLA Handbook (7th Edition):

Calderón, Raúl. “Modélisation des efforts aérodynamiques instationnaires pour la prévision du phénomène de tremblement sur des avions civils : Modelling unsteady aerodynamics loads for buffeting prediction on civil aircrafts.” 2014. Web. 21 Jan 2020.

Vancouver:

Calderón R. Modélisation des efforts aérodynamiques instationnaires pour la prévision du phénomène de tremblement sur des avions civils : Modelling unsteady aerodynamics loads for buffeting prediction on civil aircrafts. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2014. [cited 2020 Jan 21]. Available from: http://www.theses.fr/2014ESAE0005.

Council of Science Editors:

Calderón R. Modélisation des efforts aérodynamiques instationnaires pour la prévision du phénomène de tremblement sur des avions civils : Modelling unsteady aerodynamics loads for buffeting prediction on civil aircrafts. [Doctoral Dissertation]. Toulouse, ISAE; 2014. Available from: http://www.theses.fr/2014ESAE0005

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