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You searched for subject:(low Reynolds number). Showing records 1 – 30 of 144 total matches.

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Cornell University

1. Bae, Albert. Explorations Into The Life Of Dictyostelium Discoideum.

Degree: PhD, Physics, 2011, Cornell University

 In this dissertation, we explore several aspects of the Dictyostelium discoideum life cycle: growth, aggregation, and differentiation: We present experiments that question the conventional wisdom… (more)

Subjects/Keywords: Dictyostelium; Chemotaxis; Low Reynolds number swimming

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APA (6th Edition):

Bae, A. (2011). Explorations Into The Life Of Dictyostelium Discoideum. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/29116

Chicago Manual of Style (16th Edition):

Bae, Albert. “Explorations Into The Life Of Dictyostelium Discoideum.” 2011. Doctoral Dissertation, Cornell University. Accessed January 18, 2021. http://hdl.handle.net/1813/29116.

MLA Handbook (7th Edition):

Bae, Albert. “Explorations Into The Life Of Dictyostelium Discoideum.” 2011. Web. 18 Jan 2021.

Vancouver:

Bae A. Explorations Into The Life Of Dictyostelium Discoideum. [Internet] [Doctoral dissertation]. Cornell University; 2011. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1813/29116.

Council of Science Editors:

Bae A. Explorations Into The Life Of Dictyostelium Discoideum. [Doctoral Dissertation]. Cornell University; 2011. Available from: http://hdl.handle.net/1813/29116


University of Cambridge

2. Wilsby, Oscar. Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number.

Degree: PhD, 2019, University of Cambridge

 This thesis is an investigation into the production and prediction of broadband noise in axial compressors operating at low Reynolds number. The low Reynolds number(more)

Subjects/Keywords: Large eddy simulation; low reynolds number; aeroacoustics

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APA (6th Edition):

Wilsby, O. (2019). Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/294622

Chicago Manual of Style (16th Edition):

Wilsby, Oscar. “Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://www.repository.cam.ac.uk/handle/1810/294622.

MLA Handbook (7th Edition):

Wilsby, Oscar. “Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number.” 2019. Web. 18 Jan 2021.

Vancouver:

Wilsby O. Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/294622.

Council of Science Editors:

Wilsby O. Broadband Noise Prediction of an Axial Compressor Operating at Low Reynolds Number. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/294622


Georgia Tech

3. Shukla, Dhwanil P. EXPERIMENTAL STUDY OF LOW REYNOLDS NUMBER MULTIROTOR AERODYNAMIC INTERACTIONS.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 In recent years, Vertical Take-off and Landing (VTOL) rotor Unmanned Aerial Vehicles (UAVs) have gained importance in various application suited to their small size and… (more)

Subjects/Keywords: Drone; Low Reynolds Number; Rotor; PIV; Vortex

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APA (6th Edition):

Shukla, D. P. (2019). EXPERIMENTAL STUDY OF LOW REYNOLDS NUMBER MULTIROTOR AERODYNAMIC INTERACTIONS. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/63521

Chicago Manual of Style (16th Edition):

Shukla, Dhwanil P. “EXPERIMENTAL STUDY OF LOW REYNOLDS NUMBER MULTIROTOR AERODYNAMIC INTERACTIONS.” 2019. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/63521.

MLA Handbook (7th Edition):

Shukla, Dhwanil P. “EXPERIMENTAL STUDY OF LOW REYNOLDS NUMBER MULTIROTOR AERODYNAMIC INTERACTIONS.” 2019. Web. 18 Jan 2021.

Vancouver:

Shukla DP. EXPERIMENTAL STUDY OF LOW REYNOLDS NUMBER MULTIROTOR AERODYNAMIC INTERACTIONS. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/63521.

Council of Science Editors:

Shukla DP. EXPERIMENTAL STUDY OF LOW REYNOLDS NUMBER MULTIROTOR AERODYNAMIC INTERACTIONS. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/63521


University of Cambridge

4. Wilsby, Oscar. Broadband noise prediction of an axial compressor operating at low Reynolds number.

Degree: PhD, 2019, University of Cambridge

 This thesis is an investigation into the production and prediction of broadband noise in axial compressors operating at low Reynolds number. The low Reynolds number(more)

Subjects/Keywords: Large eddy simulation; low reynolds number; aeroacoustics

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APA (6th Edition):

Wilsby, O. (2019). Broadband noise prediction of an axial compressor operating at low Reynolds number. (Doctoral Dissertation). University of Cambridge. Retrieved from https://doi.org/10.17863/CAM.41726 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.782948

Chicago Manual of Style (16th Edition):

Wilsby, Oscar. “Broadband noise prediction of an axial compressor operating at low Reynolds number.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://doi.org/10.17863/CAM.41726 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.782948.

MLA Handbook (7th Edition):

Wilsby, Oscar. “Broadband noise prediction of an axial compressor operating at low Reynolds number.” 2019. Web. 18 Jan 2021.

Vancouver:

Wilsby O. Broadband noise prediction of an axial compressor operating at low Reynolds number. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 18]. Available from: https://doi.org/10.17863/CAM.41726 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.782948.

Council of Science Editors:

Wilsby O. Broadband noise prediction of an axial compressor operating at low Reynolds number. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://doi.org/10.17863/CAM.41726 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.782948


Oklahoma State University

5. Wallace, Joseph Scott. Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows.

Degree: Mechanical and Aerospace Engineering, 2019, Oklahoma State University

 The majority of unmanned aerial vehicles active currently and projected to be active in the future, operate within a low Reynolds number flow regime due… (more)

Subjects/Keywords: airfoil; cfd; low; number; reynolds; solidworks

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APA (6th Edition):

Wallace, J. S. (2019). Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/321619

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):

Wallace, Joseph Scott. “Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows.” 2019. Thesis, Oklahoma State University. Accessed January 18, 2021. http://hdl.handle.net/11244/321619.

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

MLA Handbook (7th Edition):

Wallace, Joseph Scott. “Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows.” 2019. Web. 18 Jan 2021.

Vancouver:

Wallace JS. Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows. [Internet] [Thesis]. Oklahoma State University; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11244/321619.

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

Council of Science Editors:

Wallace JS. Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows. [Thesis]. Oklahoma State University; 2019. Available from: http://hdl.handle.net/11244/321619

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


University of Georgia

6. Manjare, Manoj. Bubble driven catalytic micromotors.

Degree: 2015, University of Georgia

 This year (2014) we celebrate a decade anniversary of catalytic micromotors, in which they have come to represent one of the important technical advances, having… (more)

Subjects/Keywords: Catalytic Micromotors; Bubble Propulsion; Diffusiophoresis; Collective Behavior; Low Reynolds Number Hydrodynamics

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APA (6th Edition):

Manjare, M. (2015). Bubble driven catalytic micromotors. (Thesis). University of Georgia. Retrieved from http://hdl.handle.net/10724/31473

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):

Manjare, Manoj. “Bubble driven catalytic micromotors.” 2015. Thesis, University of Georgia. Accessed January 18, 2021. http://hdl.handle.net/10724/31473.

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

MLA Handbook (7th Edition):

Manjare, Manoj. “Bubble driven catalytic micromotors.” 2015. Web. 18 Jan 2021.

Vancouver:

Manjare M. Bubble driven catalytic micromotors. [Internet] [Thesis]. University of Georgia; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10724/31473.

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

Council of Science Editors:

Manjare M. Bubble driven catalytic micromotors. [Thesis]. University of Georgia; 2015. Available from: http://hdl.handle.net/10724/31473

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


Texas A&M University

7. Semper, Michael Thomas. Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number.

Degree: PhD, Aerospace Engineering, 2013, Texas A&M University

 The purpose of the current study was to answer several questions related to hypersonic, low Reynolds number, turbulent boundary layers, of which available data related… (more)

Subjects/Keywords: hypersonic; turbulent; boundary layer; low Reynolds number; experimental

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APA (6th Edition):

Semper, M. T. (2013). Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/150983

Chicago Manual of Style (16th Edition):

Semper, Michael Thomas. “Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number.” 2013. Doctoral Dissertation, Texas A&M University. Accessed January 18, 2021. http://hdl.handle.net/1969.1/150983.

MLA Handbook (7th Edition):

Semper, Michael Thomas. “Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number.” 2013. Web. 18 Jan 2021.

Vancouver:

Semper MT. Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number. [Internet] [Doctoral dissertation]. Texas A&M University; 2013. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1969.1/150983.

Council of Science Editors:

Semper MT. Examining A Hypersonic Turbulent Boundary Layer at Low Reynolds Number. [Doctoral Dissertation]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/150983


University of Newcastle

8. Forghani, Marveh. Consolidation of large spherical particles at low Reynolds numbers.

Degree: MPhil, 2015, University of Newcastle

Masters Research - Master of Philosophy (MPhil)

This study was concerned with the validation of a new theoretical model (Galvin et al., 2015) to describe… (more)

Subjects/Keywords: consolidation; sedimentation; scaling laws; non-colloidal spheres; low Reynolds number

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APA (6th Edition):

Forghani, M. (2015). Consolidation of large spherical particles at low Reynolds numbers. (Masters Thesis). University of Newcastle. Retrieved from http://hdl.handle.net/1959.13/1308128

Chicago Manual of Style (16th Edition):

Forghani, Marveh. “Consolidation of large spherical particles at low Reynolds numbers.” 2015. Masters Thesis, University of Newcastle. Accessed January 18, 2021. http://hdl.handle.net/1959.13/1308128.

MLA Handbook (7th Edition):

Forghani, Marveh. “Consolidation of large spherical particles at low Reynolds numbers.” 2015. Web. 18 Jan 2021.

Vancouver:

Forghani M. Consolidation of large spherical particles at low Reynolds numbers. [Internet] [Masters thesis]. University of Newcastle; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1959.13/1308128.

Council of Science Editors:

Forghani M. Consolidation of large spherical particles at low Reynolds numbers. [Masters Thesis]. University of Newcastle; 2015. Available from: http://hdl.handle.net/1959.13/1308128


University of Toronto

9. Li, Leon. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.

Degree: 2013, University of Toronto

This work is focused on the aerodynamics for a proprietary laminar flow airfoil for Unmanned Aerial Vehicle (UAV) applications. The two main focuses are (1)… (more)

Subjects/Keywords: low Reynolds number airfoil; laminar separation bubble; oil film interferometry; 0538

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APA (6th Edition):

Li, L. (2013). Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43077

Chicago Manual of Style (16th Edition):

Li, Leon. “Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.” 2013. Masters Thesis, University of Toronto. Accessed January 18, 2021. http://hdl.handle.net/1807/43077.

MLA Handbook (7th Edition):

Li, Leon. “Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.” 2013. Web. 18 Jan 2021.

Vancouver:

Li L. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1807/43077.

Council of Science Editors:

Li L. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43077


University of Cambridge

10. Corkery, Simon James. Unsteady Aerodynamics of Wing-Gust Encounters.

Degree: PhD, 2019, University of Cambridge

 Wind gusts can be highly detrimental to the performance of fixed wing aircraft. At low flight speeds, gusts transverse to the lifting surfaces can cause… (more)

Subjects/Keywords: Low Reynolds Number; Wagner; Kussner; Added Mass; Virtual Mass; Gust Encounter

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APA (6th Edition):

Corkery, S. J. (2019). Unsteady Aerodynamics of Wing-Gust Encounters. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/296842

Chicago Manual of Style (16th Edition):

Corkery, Simon James. “Unsteady Aerodynamics of Wing-Gust Encounters.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://www.repository.cam.ac.uk/handle/1810/296842.

MLA Handbook (7th Edition):

Corkery, Simon James. “Unsteady Aerodynamics of Wing-Gust Encounters.” 2019. Web. 18 Jan 2021.

Vancouver:

Corkery SJ. Unsteady Aerodynamics of Wing-Gust Encounters. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/296842.

Council of Science Editors:

Corkery SJ. Unsteady Aerodynamics of Wing-Gust Encounters. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/296842


University of Colorado

11. Ratcliffe, Thomas John. The Creeping Motion and Deformation of Drops in Solid Constrictions.

Degree: PhD, Chemical & Biochemical Engineering, 2011, University of Colorado

  Understanding the nature of emulsion flows through confined geometries (i.e., packed beds, porous media, and the cardiovascular system) is substantially meaningful to numerous applications,… (more)

Subjects/Keywords: Emulsion Flows; Low Reynolds number flows; Chemical Engineering

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APA (6th Edition):

Ratcliffe, T. J. (2011). The Creeping Motion and Deformation of Drops in Solid Constrictions. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/chbe_gradetds/12

Chicago Manual of Style (16th Edition):

Ratcliffe, Thomas John. “The Creeping Motion and Deformation of Drops in Solid Constrictions.” 2011. Doctoral Dissertation, University of Colorado. Accessed January 18, 2021. https://scholar.colorado.edu/chbe_gradetds/12.

MLA Handbook (7th Edition):

Ratcliffe, Thomas John. “The Creeping Motion and Deformation of Drops in Solid Constrictions.” 2011. Web. 18 Jan 2021.

Vancouver:

Ratcliffe TJ. The Creeping Motion and Deformation of Drops in Solid Constrictions. [Internet] [Doctoral dissertation]. University of Colorado; 2011. [cited 2021 Jan 18]. Available from: https://scholar.colorado.edu/chbe_gradetds/12.

Council of Science Editors:

Ratcliffe TJ. The Creeping Motion and Deformation of Drops in Solid Constrictions. [Doctoral Dissertation]. University of Colorado; 2011. Available from: https://scholar.colorado.edu/chbe_gradetds/12


University of Bath

12. Cleaver, David. Low Reynolds number flow control through small-amplitude high-frequency motion.

Degree: PhD, 2011, University of Bath

 There is currently growing interest in the field of Micro Air Vehicles (MAVs). A MAV is characterized by its low Reynolds numbers flight regime which… (more)

Subjects/Keywords: 629.13; aerodynamics; flow control; low reynolds number; flapping

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APA (6th Edition):

Cleaver, D. (2011). Low Reynolds number flow control through small-amplitude high-frequency motion. (Doctoral Dissertation). University of Bath. Retrieved from https://researchportal.bath.ac.uk/en/studentthesis/low-reynolds-number-flow-control-through-smallamplitude-highfrequency-motion(55149f4d-bb16-4aac-8f41-2fe6185c50c8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.547620

Chicago Manual of Style (16th Edition):

Cleaver, David. “Low Reynolds number flow control through small-amplitude high-frequency motion.” 2011. Doctoral Dissertation, University of Bath. Accessed January 18, 2021. https://researchportal.bath.ac.uk/en/studentthesis/low-reynolds-number-flow-control-through-smallamplitude-highfrequency-motion(55149f4d-bb16-4aac-8f41-2fe6185c50c8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.547620.

MLA Handbook (7th Edition):

Cleaver, David. “Low Reynolds number flow control through small-amplitude high-frequency motion.” 2011. Web. 18 Jan 2021.

Vancouver:

Cleaver D. Low Reynolds number flow control through small-amplitude high-frequency motion. [Internet] [Doctoral dissertation]. University of Bath; 2011. [cited 2021 Jan 18]. Available from: https://researchportal.bath.ac.uk/en/studentthesis/low-reynolds-number-flow-control-through-smallamplitude-highfrequency-motion(55149f4d-bb16-4aac-8f41-2fe6185c50c8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.547620.

Council of Science Editors:

Cleaver D. Low Reynolds number flow control through small-amplitude high-frequency motion. [Doctoral Dissertation]. University of Bath; 2011. Available from: https://researchportal.bath.ac.uk/en/studentthesis/low-reynolds-number-flow-control-through-smallamplitude-highfrequency-motion(55149f4d-bb16-4aac-8f41-2fe6185c50c8).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.547620


Iowa State University

13. Grager, Travis Nicholas. Experimental study of low Reynolds number flow control devices: dynamic burst control plate and dynamic roughness.

Degree: 2011, Iowa State University

 Two experimental studies were conducted to investigate the use of surface actuation devices to suppress stall on a NACA 0012 airfoil by preventing the bursting… (more)

Subjects/Keywords: dynamic roughness; flow control; low Reynolds number; Aerospace Engineering

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APA (6th Edition):

Grager, T. N. (2011). Experimental study of low Reynolds number flow control devices: dynamic burst control plate and dynamic roughness. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/10111

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):

Grager, Travis Nicholas. “Experimental study of low Reynolds number flow control devices: dynamic burst control plate and dynamic roughness.” 2011. Thesis, Iowa State University. Accessed January 18, 2021. https://lib.dr.iastate.edu/etd/10111.

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

MLA Handbook (7th Edition):

Grager, Travis Nicholas. “Experimental study of low Reynolds number flow control devices: dynamic burst control plate and dynamic roughness.” 2011. Web. 18 Jan 2021.

Vancouver:

Grager TN. Experimental study of low Reynolds number flow control devices: dynamic burst control plate and dynamic roughness. [Internet] [Thesis]. Iowa State University; 2011. [cited 2021 Jan 18]. Available from: https://lib.dr.iastate.edu/etd/10111.

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

Council of Science Editors:

Grager TN. Experimental study of low Reynolds number flow control devices: dynamic burst control plate and dynamic roughness. [Thesis]. Iowa State University; 2011. Available from: https://lib.dr.iastate.edu/etd/10111

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


University of Illinois – Urbana-Champaign

14. Tehrani, Kian. Propellers in yawed flow at low speeds.

Degree: M.S. (master's), Engineering, 2006, University of Illinois – Urbana-Champaign

 The performance characteristics of propellers at high speeds have been obtained in the past and are well documented. But neither their performance at low Reynolds(more)

Subjects/Keywords: Propellers; Low Reynolds number aerodynamics

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APA (6th Edition):

Tehrani, K. (2006). Propellers in yawed flow at low speeds. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/98461

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):

Tehrani, Kian. “Propellers in yawed flow at low speeds.” 2006. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/98461.

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

MLA Handbook (7th Edition):

Tehrani, Kian. “Propellers in yawed flow at low speeds.” 2006. Web. 18 Jan 2021.

Vancouver:

Tehrani K. Propellers in yawed flow at low speeds. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2006. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/98461.

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

Council of Science Editors:

Tehrani K. Propellers in yawed flow at low speeds. [Thesis]. University of Illinois – Urbana-Champaign; 2006. Available from: http://hdl.handle.net/2142/98461

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


Virginia Tech

15. Chien, Ssu-Ying. Compressible Lubrication Theory in Pressurized Gases.

Degree: PhD, Engineering Mechanics, 2019, Virginia Tech

 Lubrication theory plays a fundamental role in all mechanical design as well as applications to biomechanics. All machinery are composed of moving parts which must… (more)

Subjects/Keywords: Fluid mechanics; Supercritical fluids; Compressible lubrication; Low Reynolds number

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APA (6th Edition):

Chien, S. (2019). Compressible Lubrication Theory in Pressurized Gases. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/88868

Chicago Manual of Style (16th Edition):

Chien, Ssu-Ying. “Compressible Lubrication Theory in Pressurized Gases.” 2019. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/88868.

MLA Handbook (7th Edition):

Chien, Ssu-Ying. “Compressible Lubrication Theory in Pressurized Gases.” 2019. Web. 18 Jan 2021.

Vancouver:

Chien S. Compressible Lubrication Theory in Pressurized Gases. [Internet] [Doctoral dissertation]. Virginia Tech; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/88868.

Council of Science Editors:

Chien S. Compressible Lubrication Theory in Pressurized Gases. [Doctoral Dissertation]. Virginia Tech; 2019. Available from: http://hdl.handle.net/10919/88868


Virginia Tech

16. Shehata, Hisham. Unsteady Aerodynamic/Hydrodynamic Analysis of Bio-inspired Flapping Elements at Low Reynolds Number.

Degree: PhD, Engineering Mechanics, 2020, Virginia Tech

 It is by no surprise that animal locomotion continues to inspire the design of flying and swimming vehicles. Although nature produces complex kinematics and highly… (more)

Subjects/Keywords: Unsteady Aerodynamic; Hydrodynamic; Low Reynolds number; Frequency response; Flexibility; Pisciform Locomotion

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

APA (6th Edition):

Shehata, H. (2020). Unsteady Aerodynamic/Hydrodynamic Analysis of Bio-inspired Flapping Elements at Low Reynolds Number. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/97567

Chicago Manual of Style (16th Edition):

Shehata, Hisham. “Unsteady Aerodynamic/Hydrodynamic Analysis of Bio-inspired Flapping Elements at Low Reynolds Number.” 2020. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/97567.

MLA Handbook (7th Edition):

Shehata, Hisham. “Unsteady Aerodynamic/Hydrodynamic Analysis of Bio-inspired Flapping Elements at Low Reynolds Number.” 2020. Web. 18 Jan 2021.

Vancouver:

Shehata H. Unsteady Aerodynamic/Hydrodynamic Analysis of Bio-inspired Flapping Elements at Low Reynolds Number. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/97567.

Council of Science Editors:

Shehata H. Unsteady Aerodynamic/Hydrodynamic Analysis of Bio-inspired Flapping Elements at Low Reynolds Number. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/97567

17. Corkery, Simon James. Unsteady aerodynamics of wing-gust encounters.

Degree: PhD, 2019, University of Cambridge

 Wind gusts can be highly detrimental to the performance of fixed wing aircraft. At low flight speeds, gusts transverse to the lifting surfaces can cause… (more)

Subjects/Keywords: Low Reynolds Number; Wagner; Kussner; Added Mass; Virtual Mass; Gust Encounter

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

APA (6th Edition):

Corkery, S. J. (2019). Unsteady aerodynamics of wing-gust encounters. (Doctoral Dissertation). University of Cambridge. Retrieved from https://doi.org/10.17863/CAM.43887 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.787778

Chicago Manual of Style (16th Edition):

Corkery, Simon James. “Unsteady aerodynamics of wing-gust encounters.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://doi.org/10.17863/CAM.43887 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.787778.

MLA Handbook (7th Edition):

Corkery, Simon James. “Unsteady aerodynamics of wing-gust encounters.” 2019. Web. 18 Jan 2021.

Vancouver:

Corkery SJ. Unsteady aerodynamics of wing-gust encounters. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 18]. Available from: https://doi.org/10.17863/CAM.43887 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.787778.

Council of Science Editors:

Corkery SJ. Unsteady aerodynamics of wing-gust encounters. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://doi.org/10.17863/CAM.43887 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.787778


Virginia Tech

18. Portner, Stephen Michael. Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle.

Degree: MS, Aerospace Engineering, 2014, Virginia Tech

 A methodology for the design of small autonomous underwater vehicle propulsion systems has been developed and applied to the Virginia Tech 690 AUV. The methodology… (more)

Subjects/Keywords: Autonomous Underwater Vehicle; Low Reynolds Number; Propeller; Propulsion

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

APA (6th Edition):

Portner, S. M. (2014). Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50398

Chicago Manual of Style (16th Edition):

Portner, Stephen Michael. “Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle.” 2014. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/50398.

MLA Handbook (7th Edition):

Portner, Stephen Michael. “Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle.” 2014. Web. 18 Jan 2021.

Vancouver:

Portner SM. Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/50398.

Council of Science Editors:

Portner SM. Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/50398


University of Vermont

19. Seksinsky, Drue. Modeling Volcanic Ash Particle Impingement In The Hot Sections Of A Gas Turbine Engine.

Degree: MS, Mechanical Engineering, 2020, University of Vermont

  A computational study was conducted of axisymmetric droplet impingement on a flat surface at low droplet Reynolds numbers. The study was motivated by deposition… (more)

Subjects/Keywords: Droplet; Fluid Mechanics; Low Reynolds Number; Numerical Methods; Spreading; Volcanic Ash

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

APA (6th Edition):

Seksinsky, D. (2020). Modeling Volcanic Ash Particle Impingement In The Hot Sections Of A Gas Turbine Engine. (Thesis). University of Vermont. Retrieved from https://scholarworks.uvm.edu/graddis/1269

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):

Seksinsky, Drue. “Modeling Volcanic Ash Particle Impingement In The Hot Sections Of A Gas Turbine Engine.” 2020. Thesis, University of Vermont. Accessed January 18, 2021. https://scholarworks.uvm.edu/graddis/1269.

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

MLA Handbook (7th Edition):

Seksinsky, Drue. “Modeling Volcanic Ash Particle Impingement In The Hot Sections Of A Gas Turbine Engine.” 2020. Web. 18 Jan 2021.

Vancouver:

Seksinsky D. Modeling Volcanic Ash Particle Impingement In The Hot Sections Of A Gas Turbine Engine. [Internet] [Thesis]. University of Vermont; 2020. [cited 2021 Jan 18]. Available from: https://scholarworks.uvm.edu/graddis/1269.

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

Council of Science Editors:

Seksinsky D. Modeling Volcanic Ash Particle Impingement In The Hot Sections Of A Gas Turbine Engine. [Thesis]. University of Vermont; 2020. Available from: https://scholarworks.uvm.edu/graddis/1269

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


University of New South Wales

20. Zaman, Rakib Imtiaz. Numerical Simulations of High Amplitude Pitching Airfoils at Low Reynolds Numbers.

Degree: Engineering & Information Technology, 2017, University of New South Wales

 Nature is a strong source of inspiration in the development of future technologies. The flapping wing concept has come to the fore in the creation… (more)

Subjects/Keywords: High Amplitude; Flapping Wing; Pitch; Low Reynolds Number

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APA (6th Edition):

Zaman, R. I. (2017). Numerical Simulations of High Amplitude Pitching Airfoils at Low Reynolds Numbers. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/58776 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:47560/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Zaman, Rakib Imtiaz. “Numerical Simulations of High Amplitude Pitching Airfoils at Low Reynolds Numbers.” 2017. Doctoral Dissertation, University of New South Wales. Accessed January 18, 2021. http://handle.unsw.edu.au/1959.4/58776 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:47560/SOURCE02?view=true.

MLA Handbook (7th Edition):

Zaman, Rakib Imtiaz. “Numerical Simulations of High Amplitude Pitching Airfoils at Low Reynolds Numbers.” 2017. Web. 18 Jan 2021.

Vancouver:

Zaman RI. Numerical Simulations of High Amplitude Pitching Airfoils at Low Reynolds Numbers. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2021 Jan 18]. Available from: http://handle.unsw.edu.au/1959.4/58776 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:47560/SOURCE02?view=true.

Council of Science Editors:

Zaman RI. Numerical Simulations of High Amplitude Pitching Airfoils at Low Reynolds Numbers. [Doctoral Dissertation]. University of New South Wales; 2017. Available from: http://handle.unsw.edu.au/1959.4/58776 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:47560/SOURCE02?view=true


University of Texas – Austin

21. -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 18, 2021. 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. 18 Jan 2021.

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 2021 Jan 18]. 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 Pennsylvania

22. Gagnon, David A. Locomotion At Low Reynolds Number: Dynamics In Newtonian And Non-Newtonian Systems With Biomedical Applications.

Degree: 2017, University of Pennsylvania

 Swimming microorganisms such as bacteria, spermatozoa, algae, and nematodes are critical to ubiquitous biological phenomena such as disease and infection, ecosystem dynamics, and mammalian fertilization.… (more)

Subjects/Keywords: Complex fluids; Fluid rheology; Swimming at low Reynolds number; Physics

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APA (6th Edition):

Gagnon, D. A. (2017). Locomotion At Low Reynolds Number: Dynamics In Newtonian And Non-Newtonian Systems With Biomedical Applications. (Thesis). University of Pennsylvania. Retrieved from https://repository.upenn.edu/edissertations/2293

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):

Gagnon, David A. “Locomotion At Low Reynolds Number: Dynamics In Newtonian And Non-Newtonian Systems With Biomedical Applications.” 2017. Thesis, University of Pennsylvania. Accessed January 18, 2021. https://repository.upenn.edu/edissertations/2293.

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

MLA Handbook (7th Edition):

Gagnon, David A. “Locomotion At Low Reynolds Number: Dynamics In Newtonian And Non-Newtonian Systems With Biomedical Applications.” 2017. Web. 18 Jan 2021.

Vancouver:

Gagnon DA. Locomotion At Low Reynolds Number: Dynamics In Newtonian And Non-Newtonian Systems With Biomedical Applications. [Internet] [Thesis]. University of Pennsylvania; 2017. [cited 2021 Jan 18]. Available from: https://repository.upenn.edu/edissertations/2293.

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

Council of Science Editors:

Gagnon DA. Locomotion At Low Reynolds Number: Dynamics In Newtonian And Non-Newtonian Systems With Biomedical Applications. [Thesis]. University of Pennsylvania; 2017. Available from: https://repository.upenn.edu/edissertations/2293

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

23. Meshkati, Farshad. Analysis and Modeling of Rigid Microswimmers.

Degree: 2014, University of Nevada – Reno

 In this thesis, we investigate magnetically actuated rigid microswimmers based on analytical and numerical schemes. These swimming micro-robots have medical applications such as drug delivery… (more)

Subjects/Keywords: Fluid Mechanics; Low Reynolds Number; Magnetic Rotation; Microswimmer

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APA (6th Edition):

Meshkati, F. (2014). Analysis and Modeling of Rigid Microswimmers. (Thesis). University of Nevada – Reno. Retrieved from http://hdl.handle.net/11714/2970

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):

Meshkati, Farshad. “Analysis and Modeling of Rigid Microswimmers.” 2014. Thesis, University of Nevada – Reno. Accessed January 18, 2021. http://hdl.handle.net/11714/2970.

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

MLA Handbook (7th Edition):

Meshkati, Farshad. “Analysis and Modeling of Rigid Microswimmers.” 2014. Web. 18 Jan 2021.

Vancouver:

Meshkati F. Analysis and Modeling of Rigid Microswimmers. [Internet] [Thesis]. University of Nevada – Reno; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11714/2970.

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

Council of Science Editors:

Meshkati F. Analysis and Modeling of Rigid Microswimmers. [Thesis]. University of Nevada – Reno; 2014. Available from: http://hdl.handle.net/11714/2970

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


New Jersey Institute of Technology

24. Sanaei, Pejman. Mathematical modeling of membrane filtration.

Degree: PhD, Mathematical Sciences, 2017, New Jersey Institute of Technology

  The purpose of this thesis is to formulate and investigate new mathematical models for membrane filtration. The work presented is divided into six chapters.… (more)

Subjects/Keywords: Modeling; Filtration; Low Reynolds number; Porous media; Suspensions; Fluid mechanics; Mathematics

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

APA (6th Edition):

Sanaei, P. (2017). Mathematical modeling of membrane filtration. (Doctoral Dissertation). New Jersey Institute of Technology. Retrieved from https://digitalcommons.njit.edu/dissertations/24

Chicago Manual of Style (16th Edition):

Sanaei, Pejman. “Mathematical modeling of membrane filtration.” 2017. Doctoral Dissertation, New Jersey Institute of Technology. Accessed January 18, 2021. https://digitalcommons.njit.edu/dissertations/24.

MLA Handbook (7th Edition):

Sanaei, Pejman. “Mathematical modeling of membrane filtration.” 2017. Web. 18 Jan 2021.

Vancouver:

Sanaei P. Mathematical modeling of membrane filtration. [Internet] [Doctoral dissertation]. New Jersey Institute of Technology; 2017. [cited 2021 Jan 18]. Available from: https://digitalcommons.njit.edu/dissertations/24.

Council of Science Editors:

Sanaei P. Mathematical modeling of membrane filtration. [Doctoral Dissertation]. New Jersey Institute of Technology; 2017. Available from: https://digitalcommons.njit.edu/dissertations/24


University of Cambridge

25. Pantelidis, Konstantinos. Reynolds number effects on the aerodynamics of compact axial compressors.

Degree: PhD, 2018, University of Cambridge

 An axial compressor for a domestic appliance can be designed to be smaller than an equivalent centrifugal compressor. However, the performance of such a compact… (more)

Subjects/Keywords: 629.132; Low Reynolds Number; Axial Compressor; Aerodynamics; Experiment

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APA (6th Edition):

Pantelidis, K. (2018). Reynolds number effects on the aerodynamics of compact axial compressors. (Doctoral Dissertation). University of Cambridge. Retrieved from https://doi.org/10.17863/CAM.32311 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763599

Chicago Manual of Style (16th Edition):

Pantelidis, Konstantinos. “Reynolds number effects on the aerodynamics of compact axial compressors.” 2018. Doctoral Dissertation, University of Cambridge. Accessed January 18, 2021. https://doi.org/10.17863/CAM.32311 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763599.

MLA Handbook (7th Edition):

Pantelidis, Konstantinos. “Reynolds number effects on the aerodynamics of compact axial compressors.” 2018. Web. 18 Jan 2021.

Vancouver:

Pantelidis K. Reynolds number effects on the aerodynamics of compact axial compressors. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2021 Jan 18]. Available from: https://doi.org/10.17863/CAM.32311 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763599.

Council of Science Editors:

Pantelidis K. Reynolds number effects on the aerodynamics of compact axial compressors. [Doctoral Dissertation]. University of Cambridge; 2018. Available from: https://doi.org/10.17863/CAM.32311 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763599


Oklahoma State University

26. Gamble, Dustin Eli. Automated Dynamic Propeller Testing At Low Reynolds Numbers.

Degree: Mechanical & Aerospace Engineering, 2009, Oklahoma State University

 Experiments were conducted on small propellers using a motor dynamometer in a wind tunnel. The effects at different Reynolds number were observed. To maintain Reynolds(more)

Subjects/Keywords: dynamometer; experimental; low reynolds number; propeller; reynolds number; uav

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

APA (6th Edition):

Gamble, D. E. (2009). Automated Dynamic Propeller Testing At Low Reynolds Numbers. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/9932

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):

Gamble, Dustin Eli. “Automated Dynamic Propeller Testing At Low Reynolds Numbers.” 2009. Thesis, Oklahoma State University. Accessed January 18, 2021. http://hdl.handle.net/11244/9932.

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

MLA Handbook (7th Edition):

Gamble, Dustin Eli. “Automated Dynamic Propeller Testing At Low Reynolds Numbers.” 2009. Web. 18 Jan 2021.

Vancouver:

Gamble DE. Automated Dynamic Propeller Testing At Low Reynolds Numbers. [Internet] [Thesis]. Oklahoma State University; 2009. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11244/9932.

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

Council of Science Editors:

Gamble DE. Automated Dynamic Propeller Testing At Low Reynolds Numbers. [Thesis]. Oklahoma State University; 2009. Available from: http://hdl.handle.net/11244/9932

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


University of Miami

27. Lee, Jaejin. Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows.

Degree: PhD, Physics (Arts and Sciences), 2011, University of Miami

 Hypersonic vehicles generate shocks that can heat the air sufficiently to partially ionize the air and create an electrically conducting plasma that can be studied… (more)

Subjects/Keywords: magnetohydrodynamics; low magnetic Reynolds number; hypersonic flows; low diffusion E-CUSP scheme; WENO scheme

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

APA (6th Edition):

Lee, J. (2011). Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows. (Doctoral Dissertation). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_dissertations/698

Chicago Manual of Style (16th Edition):

Lee, Jaejin. “Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows.” 2011. Doctoral Dissertation, University of Miami. Accessed January 18, 2021. https://scholarlyrepository.miami.edu/oa_dissertations/698.

MLA Handbook (7th Edition):

Lee, Jaejin. “Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows.” 2011. Web. 18 Jan 2021.

Vancouver:

Lee J. Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows. [Internet] [Doctoral dissertation]. University of Miami; 2011. [cited 2021 Jan 18]. Available from: https://scholarlyrepository.miami.edu/oa_dissertations/698.

Council of Science Editors:

Lee J. Numerical Study of Three Dimensional Low Magnetic Reynolds Number Hypersonic Magnetohydrodynamic Flows. [Doctoral Dissertation]. University of Miami; 2011. Available from: https://scholarlyrepository.miami.edu/oa_dissertations/698

28. Dupire, Jules. Dynamique de cellules sanguines dans des microécoulements : Dynamics of blood cells in microflows.

Degree: Docteur es, Biophysique, 2012, Aix Marseille Université

Cette thèse traite de la dynamique de cellules sanguines dans la microcirculation. Cette appellation regroupe les deux thématiques de mon travail. La première est l'étude… (more)

Subjects/Keywords: Globule rouge; Globule blanc; Rhéologie; Bas nombre de Reynolds; Microfluidique; Red blood cell; ,White blood cell; Rheology; Low Reynolds number; Microfluidics

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APA (6th Edition):

Dupire, J. (2012). Dynamique de cellules sanguines dans des microécoulements : Dynamics of blood cells in microflows. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2012AIXM4090

Chicago Manual of Style (16th Edition):

Dupire, Jules. “Dynamique de cellules sanguines dans des microécoulements : Dynamics of blood cells in microflows.” 2012. Doctoral Dissertation, Aix Marseille Université. Accessed January 18, 2021. http://www.theses.fr/2012AIXM4090.

MLA Handbook (7th Edition):

Dupire, Jules. “Dynamique de cellules sanguines dans des microécoulements : Dynamics of blood cells in microflows.” 2012. Web. 18 Jan 2021.

Vancouver:

Dupire J. Dynamique de cellules sanguines dans des microécoulements : Dynamics of blood cells in microflows. [Internet] [Doctoral dissertation]. Aix Marseille Université 2012. [cited 2021 Jan 18]. Available from: http://www.theses.fr/2012AIXM4090.

Council of Science Editors:

Dupire J. Dynamique de cellules sanguines dans des microécoulements : Dynamics of blood cells in microflows. [Doctoral Dissertation]. Aix Marseille Université 2012. Available from: http://www.theses.fr/2012AIXM4090

29. Bernardos Barreda, Luis Francisco. Modélisation de la transition vers la turbulence d'une couche limite décollée : Laminar-to-turbulent transition modeling of a detached boundary layer.

Degree: Docteur es, Mécanique des fluides, 2019, Sorbonne université

Le but de cette thèse est de proposer des modèles qui améliorent la précision des prévisions RANS des bulbes de décollement laminaire. Dans un premier… (more)

Subjects/Keywords: Transition; Turbulence; Modélisation; Bulbe laminaire; Décrochage; Faible nombre de Reynolds; Transition; Turbulence; Modeling; Laminar bulb; Low Reynolds number; 620.106

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APA (6th Edition):

Bernardos Barreda, L. F. (2019). Modélisation de la transition vers la turbulence d'une couche limite décollée : Laminar-to-turbulent transition modeling of a detached boundary layer. (Doctoral Dissertation). Sorbonne université. Retrieved from http://www.theses.fr/2019SORUS184

Chicago Manual of Style (16th Edition):

Bernardos Barreda, Luis Francisco. “Modélisation de la transition vers la turbulence d'une couche limite décollée : Laminar-to-turbulent transition modeling of a detached boundary layer.” 2019. Doctoral Dissertation, Sorbonne université. Accessed January 18, 2021. http://www.theses.fr/2019SORUS184.

MLA Handbook (7th Edition):

Bernardos Barreda, Luis Francisco. “Modélisation de la transition vers la turbulence d'une couche limite décollée : Laminar-to-turbulent transition modeling of a detached boundary layer.” 2019. Web. 18 Jan 2021.

Vancouver:

Bernardos Barreda LF. Modélisation de la transition vers la turbulence d'une couche limite décollée : Laminar-to-turbulent transition modeling of a detached boundary layer. [Internet] [Doctoral dissertation]. Sorbonne université; 2019. [cited 2021 Jan 18]. Available from: http://www.theses.fr/2019SORUS184.

Council of Science Editors:

Bernardos Barreda LF. Modélisation de la transition vers la turbulence d'une couche limite décollée : Laminar-to-turbulent transition modeling of a detached boundary layer. [Doctoral Dissertation]. Sorbonne université; 2019. Available from: http://www.theses.fr/2019SORUS184


University of Michigan

30. Trizila, Patrick Clark. Aerodynamics of Low Reynolds Number Rigid Flapping Wing Under Hover and Freestream Conditions.

Degree: PhD, Aerospace Engineering, 2011, University of Michigan

 Micro air vehicles (MAVs) are defined by all spatial dimensions being less than 15 cm. Equipped with a video camera or a sensor, these vehicles… (more)

Subjects/Keywords: MAV; Aerodynamics; Flapping Wing; Vortex Dynamics; Surrogate Model; Low Reynolds Number; Aerospace Engineering; Engineering

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APA (6th Edition):

Trizila, P. C. (2011). Aerodynamics of Low Reynolds Number Rigid Flapping Wing Under Hover and Freestream Conditions. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/86503

Chicago Manual of Style (16th Edition):

Trizila, Patrick Clark. “Aerodynamics of Low Reynolds Number Rigid Flapping Wing Under Hover and Freestream Conditions.” 2011. Doctoral Dissertation, University of Michigan. Accessed January 18, 2021. http://hdl.handle.net/2027.42/86503.

MLA Handbook (7th Edition):

Trizila, Patrick Clark. “Aerodynamics of Low Reynolds Number Rigid Flapping Wing Under Hover and Freestream Conditions.” 2011. Web. 18 Jan 2021.

Vancouver:

Trizila PC. Aerodynamics of Low Reynolds Number Rigid Flapping Wing Under Hover and Freestream Conditions. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2027.42/86503.

Council of Science Editors:

Trizila PC. Aerodynamics of Low Reynolds Number Rigid Flapping Wing Under Hover and Freestream Conditions. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/86503

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