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You searched for subject:(Boundary layer separation). Showing records 1 – 30 of 54 total matches.

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University of Manchester

1. Yumashev, Dmitry. Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature.

Degree: PhD, 2010, University of Manchester

 The work addresses an important question of whether a discontinuity in wall curvature can cause boundary layer separation at transonic speeds. Firstly an inviscid transonic… (more)

Subjects/Keywords: 519; transonic boundary layer separation

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

APA (6th Edition):

Yumashev, D. (2010). Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398

Chicago Manual of Style (16th Edition):

Yumashev, Dmitry. “Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature.” 2010. Doctoral Dissertation, University of Manchester. Accessed August 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398.

MLA Handbook (7th Edition):

Yumashev, Dmitry. “Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature.” 2010. Web. 18 Aug 2019.

Vancouver:

Yumashev D. Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature. [Internet] [Doctoral dissertation]. University of Manchester; 2010. [cited 2019 Aug 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398.

Council of Science Editors:

Yumashev D. Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature. [Doctoral Dissertation]. University of Manchester; 2010. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398


University of Arizona

2. Balthazar, Michael Aeko. Experimental Investigation of Boundary Layer Separation .

Degree: 2018, University of Arizona

 A study of boundary layer separation in wind tunnel, water tunnel, and free-flight conditions is reported on within these pages. Methods and results for building… (more)

Subjects/Keywords: boundary layer; flow control; laminar separation

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APA (6th Edition):

Balthazar, M. A. (2018). Experimental Investigation of Boundary Layer Separation . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/630146

Chicago Manual of Style (16th Edition):

Balthazar, Michael Aeko. “Experimental Investigation of Boundary Layer Separation .” 2018. Masters Thesis, University of Arizona. Accessed August 18, 2019. http://hdl.handle.net/10150/630146.

MLA Handbook (7th Edition):

Balthazar, Michael Aeko. “Experimental Investigation of Boundary Layer Separation .” 2018. Web. 18 Aug 2019.

Vancouver:

Balthazar MA. Experimental Investigation of Boundary Layer Separation . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10150/630146.

Council of Science Editors:

Balthazar MA. Experimental Investigation of Boundary Layer Separation . [Masters Thesis]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/630146


Indian Institute of Science

3. Suneesh, S S. Experimental Studies on the Effect of an Upstream Periodic Wake on a Turbulent Separation Bubble.

Degree: 2016, Indian Institute of Science

 The object of the present work is to experimentally study the case of a turbulent boundary layer subjected to an Adverse Pressure Gradient (APG) with… (more)

Subjects/Keywords: Turbulent Boundary Layer Separation; Wake Boundary Layer Interaction; Wind Tunnel; Turbulent Separation Bubble Structure; Turbulent Separation Bubble; Turbulent Boundary Layer; Adverse Pressure Gradient (APG); Phase Averaging Technique; Aerospace Engineering

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APA (6th Edition):

Suneesh, S. S. (2016). Experimental Studies on the Effect of an Upstream Periodic Wake on a Turbulent Separation Bubble. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3762 ; http://etd.iisc.ernet.in/abstracts/4633/G28454-Abs.pdf

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

Chicago Manual of Style (16th Edition):

Suneesh, S S. “Experimental Studies on the Effect of an Upstream Periodic Wake on a Turbulent Separation Bubble.” 2016. Thesis, Indian Institute of Science. Accessed August 18, 2019. http://etd.iisc.ernet.in/2005/3762 ; http://etd.iisc.ernet.in/abstracts/4633/G28454-Abs.pdf.

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

MLA Handbook (7th Edition):

Suneesh, S S. “Experimental Studies on the Effect of an Upstream Periodic Wake on a Turbulent Separation Bubble.” 2016. Web. 18 Aug 2019.

Vancouver:

Suneesh SS. Experimental Studies on the Effect of an Upstream Periodic Wake on a Turbulent Separation Bubble. [Internet] [Thesis]. Indian Institute of Science; 2016. [cited 2019 Aug 18]. Available from: http://etd.iisc.ernet.in/2005/3762 ; http://etd.iisc.ernet.in/abstracts/4633/G28454-Abs.pdf.

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

Council of Science Editors:

Suneesh SS. Experimental Studies on the Effect of an Upstream Periodic Wake on a Turbulent Separation Bubble. [Thesis]. Indian Institute of Science; 2016. Available from: http://etd.iisc.ernet.in/2005/3762 ; http://etd.iisc.ernet.in/abstracts/4633/G28454-Abs.pdf

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

4. Chandarki, Imran Mushtaque Ahmad. On the laminar similarity boundary layer equations; -.

Degree: Fluid Dynamics, 2014, Dr. Babasaheb Ambedkar Technological University

The deduction of the boundary layer equations from Navier Stokes equations was one of the most important advances in fluid dynamics Using an order of… (more)

Subjects/Keywords: Laminar Flow; Turbulent flow; MHD Flows; Boundary Layer Theory; Boundary Layer Separation; Similarity Transformations; Prandtls Boundary equations

Page 1

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APA (6th Edition):

Chandarki, I. M. A. (2014). On the laminar similarity boundary layer equations; -. (Thesis). Dr. Babasaheb Ambedkar Technological University. Retrieved from http://shodhganga.inflibnet.ac.in/handle/10603/26693

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):

Chandarki, Imran Mushtaque Ahmad. “On the laminar similarity boundary layer equations; -.” 2014. Thesis, Dr. Babasaheb Ambedkar Technological University. Accessed August 18, 2019. http://shodhganga.inflibnet.ac.in/handle/10603/26693.

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

MLA Handbook (7th Edition):

Chandarki, Imran Mushtaque Ahmad. “On the laminar similarity boundary layer equations; -.” 2014. Web. 18 Aug 2019.

Vancouver:

Chandarki IMA. On the laminar similarity boundary layer equations; -. [Internet] [Thesis]. Dr. Babasaheb Ambedkar Technological University; 2014. [cited 2019 Aug 18]. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/26693.

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

Council of Science Editors:

Chandarki IMA. On the laminar similarity boundary layer equations; -. [Thesis]. Dr. Babasaheb Ambedkar Technological University; 2014. Available from: http://shodhganga.inflibnet.ac.in/handle/10603/26693

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


Texas A&M University

5. 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 August 18, 2019. 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. 18 Aug 2019.

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 2019 Aug 18]. 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


University of Manchester

6. Ahmed, Ishtiaq. THE INTERACTION OF SYNTHETIC JETS WITH ATTACHED AND SEPARATING TURBULENT BOUNDARY LAYER.

Degree: 2014, University of Manchester

 Like virtually every other human activity, air transport has an impact on the environment and similar to all other industries environmental impacts and economic issues… (more)

Subjects/Keywords: Flow separation; Boundary layer; Synthetic jet actuator; vortical structures

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APA (6th Edition):

Ahmed, I. (2014). THE INTERACTION OF SYNTHETIC JETS WITH ATTACHED AND SEPARATING TURBULENT BOUNDARY LAYER. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:223688

Chicago Manual of Style (16th Edition):

Ahmed, Ishtiaq. “THE INTERACTION OF SYNTHETIC JETS WITH ATTACHED AND SEPARATING TURBULENT BOUNDARY LAYER.” 2014. Doctoral Dissertation, University of Manchester. Accessed August 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:223688.

MLA Handbook (7th Edition):

Ahmed, Ishtiaq. “THE INTERACTION OF SYNTHETIC JETS WITH ATTACHED AND SEPARATING TURBULENT BOUNDARY LAYER.” 2014. Web. 18 Aug 2019.

Vancouver:

Ahmed I. THE INTERACTION OF SYNTHETIC JETS WITH ATTACHED AND SEPARATING TURBULENT BOUNDARY LAYER. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Aug 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:223688.

Council of Science Editors:

Ahmed I. THE INTERACTION OF SYNTHETIC JETS WITH ATTACHED AND SEPARATING TURBULENT BOUNDARY LAYER. [Doctoral Dissertation]. University of Manchester; 2014. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:223688


Mississippi State University

7. Wahidi, Redha. AN EXPERIMENTAL INVESTIGATION OF AIRFOILS WITH LAMINAR SEPARATION BUBBLES AND EFFECTS OF DISTRIBUTED SUCTION.

Degree: PhD, Aerospace Engineering, 2009, Mississippi State University

  In an effort to understand the behavior of the laminar separation bubbles on NACA 0012 and Liebeck LA2573a airfoils at different Reynolds numbers and… (more)

Subjects/Keywords: aerodynamics; boundary layer; control; suction; Laminar Separation Bubble

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APA (6th Edition):

Wahidi, R. (2009). AN EXPERIMENTAL INVESTIGATION OF AIRFOILS WITH LAMINAR SEPARATION BUBBLES AND EFFECTS OF DISTRIBUTED SUCTION. (Doctoral Dissertation). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-11052009-213322/ ;

Chicago Manual of Style (16th Edition):

Wahidi, Redha. “AN EXPERIMENTAL INVESTIGATION OF AIRFOILS WITH LAMINAR SEPARATION BUBBLES AND EFFECTS OF DISTRIBUTED SUCTION.” 2009. Doctoral Dissertation, Mississippi State University. Accessed August 18, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-11052009-213322/ ;.

MLA Handbook (7th Edition):

Wahidi, Redha. “AN EXPERIMENTAL INVESTIGATION OF AIRFOILS WITH LAMINAR SEPARATION BUBBLES AND EFFECTS OF DISTRIBUTED SUCTION.” 2009. Web. 18 Aug 2019.

Vancouver:

Wahidi R. AN EXPERIMENTAL INVESTIGATION OF AIRFOILS WITH LAMINAR SEPARATION BUBBLES AND EFFECTS OF DISTRIBUTED SUCTION. [Internet] [Doctoral dissertation]. Mississippi State University; 2009. [cited 2019 Aug 18]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-11052009-213322/ ;.

Council of Science Editors:

Wahidi R. AN EXPERIMENTAL INVESTIGATION OF AIRFOILS WITH LAMINAR SEPARATION BUBBLES AND EFFECTS OF DISTRIBUTED SUCTION. [Doctoral Dissertation]. Mississippi State University; 2009. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-11052009-213322/ ;


University of Cambridge

8. Xiang, Xue. Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels.

Degree: PhD, 2018, University of Cambridge

 In a rectangular cross-section wind tunnel a separated oblique shock reflection is set to interact with the turbulent boundary layer (oblique SBLI) both on the… (more)

Subjects/Keywords: boundary layer separation; high-speed flow; oblique shock waves

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APA (6th Edition):

Xiang, X. (2018). Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/287477 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763734

Chicago Manual of Style (16th Edition):

Xiang, Xue. “Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels.” 2018. Doctoral Dissertation, University of Cambridge. Accessed August 18, 2019. https://www.repository.cam.ac.uk/handle/1810/287477 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763734.

MLA Handbook (7th Edition):

Xiang, Xue. “Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels.” 2018. Web. 18 Aug 2019.

Vancouver:

Xiang X. Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2019 Aug 18]. Available from: https://www.repository.cam.ac.uk/handle/1810/287477 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763734.

Council of Science Editors:

Xiang X. Corner effects for oblique shock wave/turbulent boundary layer interactions in rectangular channels. [Doctoral Dissertation]. University of Cambridge; 2018. Available from: https://www.repository.cam.ac.uk/handle/1810/287477 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.763734

9. Kapsalis, Panagiotis - Chrysovalantis. Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής.

Degree: 2016, University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας

 At the beginning of the 21st century, Fluid Mechanics applications are connected with every aspect of human activity. The search for more effective power generation… (more)

Subjects/Keywords: Μετάβαση; Αποκόλληση; Οριακό στρώμα; Ενεργητική καθοδήγηση ροής; Transition; Separation; Boundary layer; Active flow control

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APA (6th Edition):

Kapsalis, P. -. C. (2016). Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής. (Thesis). University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας. Retrieved from http://hdl.handle.net/10442/hedi/37397

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):

Kapsalis, Panagiotis - Chrysovalantis. “Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής.” 2016. Thesis, University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας. Accessed August 18, 2019. http://hdl.handle.net/10442/hedi/37397.

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

MLA Handbook (7th Edition):

Kapsalis, Panagiotis - Chrysovalantis. “Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής.” 2016. Web. 18 Aug 2019.

Vancouver:

Kapsalis P-C. Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής. [Internet] [Thesis]. University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας; 2016. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10442/hedi/37397.

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

Council of Science Editors:

Kapsalis P-C. Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής. [Thesis]. University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας; 2016. Available from: http://hdl.handle.net/10442/hedi/37397

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


University of Alabama

10. Smith, Jonathon Andrew. Turbulent separation control effects of mako shark skin samples on a naca 4412 hydrofoil.

Degree: 2011, University of Alabama

 Shark skin is investigated as a means of passive flow separation control due to its preferential flow direction and the potential for its scales to… (more)

Subjects/Keywords: Electronic Thesis or Dissertation;  – thesis; Aerospace engineering; biological; boundary layer; flow control; passive; separation; turbulent

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APA (6th Edition):

Smith, J. A. (2011). Turbulent separation control effects of mako shark skin samples on a naca 4412 hydrofoil. (Thesis). University of Alabama. Retrieved from http://purl.lib.ua.edu/54156

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):

Smith, Jonathon Andrew. “Turbulent separation control effects of mako shark skin samples on a naca 4412 hydrofoil.” 2011. Thesis, University of Alabama. Accessed August 18, 2019. http://purl.lib.ua.edu/54156.

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

MLA Handbook (7th Edition):

Smith, Jonathon Andrew. “Turbulent separation control effects of mako shark skin samples on a naca 4412 hydrofoil.” 2011. Web. 18 Aug 2019.

Vancouver:

Smith JA. Turbulent separation control effects of mako shark skin samples on a naca 4412 hydrofoil. [Internet] [Thesis]. University of Alabama; 2011. [cited 2019 Aug 18]. Available from: http://purl.lib.ua.edu/54156.

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

Council of Science Editors:

Smith JA. Turbulent separation control effects of mako shark skin samples on a naca 4412 hydrofoil. [Thesis]. University of Alabama; 2011. Available from: http://purl.lib.ua.edu/54156

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


University of Manchester

11. Zhou, Jue. Numerical investigation of the behaviour of circular synthetic jets for effective flow separation control.

Degree: PhD, 2010, University of Manchester

 The stringing regulation on greenhouse gases emissions coupled with the rising fuel price and the growth in aviation transportation have imposed increasing demands on the… (more)

Subjects/Keywords: 629.13; Synthetic jets; Laminar boundary layer; Surface shear stress; Flow separation control; Numerical simulation

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

APA (6th Edition):

Zhou, J. (2010). Numerical investigation of the behaviour of circular synthetic jets for effective flow separation control. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-behaviour-of-circular-synthetic-jets-for-effective-flow-separation-control(6faae20e-82d6-4efb-8044-c02b089d667c).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.527192

Chicago Manual of Style (16th Edition):

Zhou, Jue. “Numerical investigation of the behaviour of circular synthetic jets for effective flow separation control.” 2010. Doctoral Dissertation, University of Manchester. Accessed August 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-behaviour-of-circular-synthetic-jets-for-effective-flow-separation-control(6faae20e-82d6-4efb-8044-c02b089d667c).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.527192.

MLA Handbook (7th Edition):

Zhou, Jue. “Numerical investigation of the behaviour of circular synthetic jets for effective flow separation control.” 2010. Web. 18 Aug 2019.

Vancouver:

Zhou J. Numerical investigation of the behaviour of circular synthetic jets for effective flow separation control. [Internet] [Doctoral dissertation]. University of Manchester; 2010. [cited 2019 Aug 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-behaviour-of-circular-synthetic-jets-for-effective-flow-separation-control(6faae20e-82d6-4efb-8044-c02b089d667c).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.527192.

Council of Science Editors:

Zhou J. Numerical investigation of the behaviour of circular synthetic jets for effective flow separation control. [Doctoral Dissertation]. University of Manchester; 2010. Available from: https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-behaviour-of-circular-synthetic-jets-for-effective-flow-separation-control(6faae20e-82d6-4efb-8044-c02b089d667c).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.527192


University of Manchester

12. Zhou, Jue. Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control.

Degree: 2010, University of Manchester

 Abstract of thesis entitled "Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control" submitted to the University of Manchester for… (more)

Subjects/Keywords: Synthetic jets; Laminar boundary layer; Surface shear stress; Flow separation control; Numerical simulation

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

APA (6th Edition):

Zhou, J. (2010). Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:96786

Chicago Manual of Style (16th Edition):

Zhou, Jue. “Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control.” 2010. Doctoral Dissertation, University of Manchester. Accessed August 18, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:96786.

MLA Handbook (7th Edition):

Zhou, Jue. “Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control.” 2010. Web. 18 Aug 2019.

Vancouver:

Zhou J. Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control. [Internet] [Doctoral dissertation]. University of Manchester; 2010. [cited 2019 Aug 18]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:96786.

Council of Science Editors:

Zhou J. Numerical Investigation of the Behaviour of Circular Synthetic Jets for Effective Flow Separation Control. [Doctoral Dissertation]. University of Manchester; 2010. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:96786


University of Texas – Austin

13. Greene, Benton Robb. Control of mean separation in a compression ramp shock boundary layer interaction using pulsed plasma jets.

Degree: Aerospace Engineering, 2014, University of Texas – Austin

 Pulsed plasma jets (also called "SparkJets'") were investigated for use in controlling the mean separation location induced by shock wave-boundary layer interaction. These synthetic jet… (more)

Subjects/Keywords: Pulsed plasma jet; SWBLI; Shock wave-boundary layer interactions; Shock induced separation

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

APA (6th Edition):

Greene, B. R. (2014). Control of mean separation in a compression ramp shock boundary layer interaction using pulsed plasma jets. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/25422

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):

Greene, Benton Robb. “Control of mean separation in a compression ramp shock boundary layer interaction using pulsed plasma jets.” 2014. Thesis, University of Texas – Austin. Accessed August 18, 2019. http://hdl.handle.net/2152/25422.

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

MLA Handbook (7th Edition):

Greene, Benton Robb. “Control of mean separation in a compression ramp shock boundary layer interaction using pulsed plasma jets.” 2014. Web. 18 Aug 2019.

Vancouver:

Greene BR. Control of mean separation in a compression ramp shock boundary layer interaction using pulsed plasma jets. [Internet] [Thesis]. University of Texas – Austin; 2014. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2152/25422.

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

Council of Science Editors:

Greene BR. Control of mean separation in a compression ramp shock boundary layer interaction using pulsed plasma jets. [Thesis]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/25422

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


University of Arizona

14. Balzer, Wolfgang. Numerical Investigation of the Role of Free-Stream Turbulence on Boundary-Layer Separation and Separation Control .

Degree: 2011, University of Arizona

 The aerodynamic performance of lifting surfaces operating at low Reynolds number conditions is impaired by laminar separation. Understanding of the physical mechanisms and hydrodynamic instabilities… (more)

Subjects/Keywords: boundary-layer separation; flow control; free-stream turbulence; hydrodynamic instabilities; transition to turbulence

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APA (6th Edition):

Balzer, W. (2011). Numerical Investigation of the Role of Free-Stream Turbulence on Boundary-Layer Separation and Separation Control . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/204289

Chicago Manual of Style (16th Edition):

Balzer, Wolfgang. “Numerical Investigation of the Role of Free-Stream Turbulence on Boundary-Layer Separation and Separation Control .” 2011. Doctoral Dissertation, University of Arizona. Accessed August 18, 2019. http://hdl.handle.net/10150/204289.

MLA Handbook (7th Edition):

Balzer, Wolfgang. “Numerical Investigation of the Role of Free-Stream Turbulence on Boundary-Layer Separation and Separation Control .” 2011. Web. 18 Aug 2019.

Vancouver:

Balzer W. Numerical Investigation of the Role of Free-Stream Turbulence on Boundary-Layer Separation and Separation Control . [Internet] [Doctoral dissertation]. University of Arizona; 2011. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10150/204289.

Council of Science Editors:

Balzer W. Numerical Investigation of the Role of Free-Stream Turbulence on Boundary-Layer Separation and Separation Control . [Doctoral Dissertation]. University of Arizona; 2011. Available from: http://hdl.handle.net/10150/204289


Delft University of Technology

15. Michelis, Theodorus. Boundary Layer Separation: Diagnostics and Control.

Degree: 2017, Delft University of Technology

 The research presented in this thesis focuses on boundary layer separation and, more specifically, on the related physical mechanisms, such as laminar to turbulent transition,… (more)

Subjects/Keywords: Boundary layer separation; DBD plasma actuators

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APA (6th Edition):

Michelis, T. (2017). Boundary Layer Separation: Diagnostics and Control. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:isbn:978-94-92516-82-4 ; 10.4233/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53

Chicago Manual of Style (16th Edition):

Michelis, Theodorus. “Boundary Layer Separation: Diagnostics and Control.” 2017. Doctoral Dissertation, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:isbn:978-94-92516-82-4 ; 10.4233/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53.

MLA Handbook (7th Edition):

Michelis, Theodorus. “Boundary Layer Separation: Diagnostics and Control.” 2017. Web. 18 Aug 2019.

Vancouver:

Michelis T. Boundary Layer Separation: Diagnostics and Control. [Internet] [Doctoral dissertation]. Delft University of Technology; 2017. [cited 2019 Aug 18]. Available from: http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:isbn:978-94-92516-82-4 ; 10.4233/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53.

Council of Science Editors:

Michelis T. Boundary Layer Separation: Diagnostics and Control. [Doctoral Dissertation]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:isbn:978-94-92516-82-4 ; 10.4233/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; urn:NBN:nl:ui:24-uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53 ; http://resolver.tudelft.nl/uuid:f5ecca35-71f6-4c99-92e8-a3004113fa53


Cal Poly

16. Rohr, Allen R. A Computational Fluid Dynamics (CFD) Analysis of the Aerodynamic Effects of the Seams on a Two-Dimensional Representation of a Soccer Ball.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  Most major sports today use a dedicated ball or projectile with specific shape, size, and surface geometry, except for soccer. Over the history of… (more)

Subjects/Keywords: CFD; Computational Fluid Dynamics; soccer ball seams; boundary layer separation; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Rohr, A. R. (2018). A Computational Fluid Dynamics (CFD) Analysis of the Aerodynamic Effects of the Seams on a Two-Dimensional Representation of a Soccer Ball. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2013

Chicago Manual of Style (16th Edition):

Rohr, Allen R. “A Computational Fluid Dynamics (CFD) Analysis of the Aerodynamic Effects of the Seams on a Two-Dimensional Representation of a Soccer Ball.” 2018. Masters Thesis, Cal Poly. Accessed August 18, 2019. https://digitalcommons.calpoly.edu/theses/2013.

MLA Handbook (7th Edition):

Rohr, Allen R. “A Computational Fluid Dynamics (CFD) Analysis of the Aerodynamic Effects of the Seams on a Two-Dimensional Representation of a Soccer Ball.” 2018. Web. 18 Aug 2019.

Vancouver:

Rohr AR. A Computational Fluid Dynamics (CFD) Analysis of the Aerodynamic Effects of the Seams on a Two-Dimensional Representation of a Soccer Ball. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2019 Aug 18]. Available from: https://digitalcommons.calpoly.edu/theses/2013.

Council of Science Editors:

Rohr AR. A Computational Fluid Dynamics (CFD) Analysis of the Aerodynamic Effects of the Seams on a Two-Dimensional Representation of a Soccer Ball. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/2013

17. Passaggia, Pierre-yves. Instabilités d'écoulements décollés et leur contrôle : Instabilities and control of a separated boundary-layer flow.

Degree: Docteur es, Mécanique et Physique des Fluides, 2012, Aix Marseille Université

La dynamique d'instabilité d'un écoulement laminaire décollé est étudiée expérimentalement et son contrôle par le biais de la simulation numérique. La configuration étudiée est une… (more)

Subjects/Keywords: Couche limite; Décollement; Contrôle; Réduction de modèle; Optimisation Lagrangienne; Boundary-layer flow; Separation; Control; Model reduction; Lagrangian optimisation

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

APA (6th Edition):

Passaggia, P. (2012). Instabilités d'écoulements décollés et leur contrôle : Instabilities and control of a separated boundary-layer flow. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2012AIXM4790

Chicago Manual of Style (16th Edition):

Passaggia, Pierre-yves. “Instabilités d'écoulements décollés et leur contrôle : Instabilities and control of a separated boundary-layer flow.” 2012. Doctoral Dissertation, Aix Marseille Université. Accessed August 18, 2019. http://www.theses.fr/2012AIXM4790.

MLA Handbook (7th Edition):

Passaggia, Pierre-yves. “Instabilités d'écoulements décollés et leur contrôle : Instabilities and control of a separated boundary-layer flow.” 2012. Web. 18 Aug 2019.

Vancouver:

Passaggia P. Instabilités d'écoulements décollés et leur contrôle : Instabilities and control of a separated boundary-layer flow. [Internet] [Doctoral dissertation]. Aix Marseille Université 2012. [cited 2019 Aug 18]. Available from: http://www.theses.fr/2012AIXM4790.

Council of Science Editors:

Passaggia P. Instabilités d'écoulements décollés et leur contrôle : Instabilities and control of a separated boundary-layer flow. [Doctoral Dissertation]. Aix Marseille Université 2012. Available from: http://www.theses.fr/2012AIXM4790


Virginia Tech

18. DeMoss, Joshua Andrew. Skin Friction and Cross-flow Separation on an Ellipsoidal Body During Constant Yaw Turns and a Pitch-up Maneuver with Roll Oscillation.

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

 The skin friction and cross-flow separation location on a non-body-of-revolution (non-BOR) ellipsoidal model performing constant-yaw turns and a pitch-up maneuver, each with roll oscillation were… (more)

Subjects/Keywords: Boundary Layer Measurement; Non-body-of-Revolution; Ellipsoid; Hot-film sensors; Skin Friction Measurement; Unsteady Roll Motion; Separation Location

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APA (6th Edition):

DeMoss, J. A. (2010). Skin Friction and Cross-flow Separation on an Ellipsoidal Body During Constant Yaw Turns and a Pitch-up Maneuver with Roll Oscillation. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29063

Chicago Manual of Style (16th Edition):

DeMoss, Joshua Andrew. “Skin Friction and Cross-flow Separation on an Ellipsoidal Body During Constant Yaw Turns and a Pitch-up Maneuver with Roll Oscillation.” 2010. Doctoral Dissertation, Virginia Tech. Accessed August 18, 2019. http://hdl.handle.net/10919/29063.

MLA Handbook (7th Edition):

DeMoss, Joshua Andrew. “Skin Friction and Cross-flow Separation on an Ellipsoidal Body During Constant Yaw Turns and a Pitch-up Maneuver with Roll Oscillation.” 2010. Web. 18 Aug 2019.

Vancouver:

DeMoss JA. Skin Friction and Cross-flow Separation on an Ellipsoidal Body During Constant Yaw Turns and a Pitch-up Maneuver with Roll Oscillation. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10919/29063.

Council of Science Editors:

DeMoss JA. Skin Friction and Cross-flow Separation on an Ellipsoidal Body During Constant Yaw Turns and a Pitch-up Maneuver with Roll Oscillation. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/29063


Virginia Tech

19. Harper, David Keneda. Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet.

Degree: MS, Mechanical Engineering, 2000, Virginia Tech

 In this thesis, the benefits of boundary layer control (BLC) in improving aerodynamic performance and engine stability were examined in a compact, serpentine inlet exhibiting… (more)

Subjects/Keywords: Serpentine inlet; wall-pressure fluctuations; Boundary layer control; Separation

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

APA (6th Edition):

Harper, D. K. (2000). Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32841

Chicago Manual of Style (16th Edition):

Harper, David Keneda. “Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet.” 2000. Masters Thesis, Virginia Tech. Accessed August 18, 2019. http://hdl.handle.net/10919/32841.

MLA Handbook (7th Edition):

Harper, David Keneda. “Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet.” 2000. Web. 18 Aug 2019.

Vancouver:

Harper DK. Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10919/32841.

Council of Science Editors:

Harper DK. Boundary Layer Control and Wall-Pressure Fluctuations in a Serpentine Inlet. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/32841


KTH

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

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

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

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

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

APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

Sjöö, Filip. “Development of concept for silent UAV propulsion.” 2018. Thesis, KTH. Accessed August 18, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232450.

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

MLA Handbook (7th Edition):

Sjöö, Filip. “Development of concept for silent UAV propulsion.” 2018. Web. 18 Aug 2019.

Vancouver:

Sjöö F. Development of concept for silent UAV propulsion. [Internet] [Thesis]. KTH; 2018. [cited 2019 Aug 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-232450.

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

Council of Science Editors:

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

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

21. Fadla, Fawzi. Caractérisation expérimentale de la dynamique du décollement de couche limite induit par un gradient de pression adverse et un effet de courbure : Experimental characterization of the boundary layer separation dynamics induced by adverse pressure gradient and curvature effect.

Degree: Docteur es, Mécanique., 2014, Valenciennes

Ces travaux de recherche portent sur la caractérisation des phénomènes instationnaires associés aux écoulements décollés induits à la fois par un gradient de pression adverse… (more)

Subjects/Keywords: Décollement de couche limite; Gradient de pression adverse; Instabilités.; Boundary layer separation; Adverse pressure gradient; Instabilities.

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APA (6th Edition):

Fadla, F. (2014). Caractérisation expérimentale de la dynamique du décollement de couche limite induit par un gradient de pression adverse et un effet de courbure : Experimental characterization of the boundary layer separation dynamics induced by adverse pressure gradient and curvature effect. (Doctoral Dissertation). Valenciennes. Retrieved from http://www.theses.fr/2014VALE0022

Chicago Manual of Style (16th Edition):

Fadla, Fawzi. “Caractérisation expérimentale de la dynamique du décollement de couche limite induit par un gradient de pression adverse et un effet de courbure : Experimental characterization of the boundary layer separation dynamics induced by adverse pressure gradient and curvature effect.” 2014. Doctoral Dissertation, Valenciennes. Accessed August 18, 2019. http://www.theses.fr/2014VALE0022.

MLA Handbook (7th Edition):

Fadla, Fawzi. “Caractérisation expérimentale de la dynamique du décollement de couche limite induit par un gradient de pression adverse et un effet de courbure : Experimental characterization of the boundary layer separation dynamics induced by adverse pressure gradient and curvature effect.” 2014. Web. 18 Aug 2019.

Vancouver:

Fadla F. Caractérisation expérimentale de la dynamique du décollement de couche limite induit par un gradient de pression adverse et un effet de courbure : Experimental characterization of the boundary layer separation dynamics induced by adverse pressure gradient and curvature effect. [Internet] [Doctoral dissertation]. Valenciennes; 2014. [cited 2019 Aug 18]. Available from: http://www.theses.fr/2014VALE0022.

Council of Science Editors:

Fadla F. Caractérisation expérimentale de la dynamique du décollement de couche limite induit par un gradient de pression adverse et un effet de courbure : Experimental characterization of the boundary layer separation dynamics induced by adverse pressure gradient and curvature effect. [Doctoral Dissertation]. Valenciennes; 2014. Available from: http://www.theses.fr/2014VALE0022


University of New South Wales

22. Findanis, Nicholas. Asymmetrical localised synthetic jets in three-dimensional flows over bluff and streamlined bodies.

Degree: Mechanical & Manufacturing Engineering, 2012, University of New South Wales

 Synthetic jet, a turbulent shear flow generated from an oscillating train of coalescing vortex rings having a time-averaged zero net mass flow rate, is generally… (more)

Subjects/Keywords: Boundary layer; Synthetic jet; Flow separation; Wake; Three-dimensional; Drag; Flow reversal; Aerodynamics; Bluff body; Streamlined body

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APA (6th Edition):

Findanis, N. (2012). Asymmetrical localised synthetic jets in three-dimensional flows over bluff and streamlined bodies. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/51833 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10500/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Findanis, Nicholas. “Asymmetrical localised synthetic jets in three-dimensional flows over bluff and streamlined bodies.” 2012. Doctoral Dissertation, University of New South Wales. Accessed August 18, 2019. http://handle.unsw.edu.au/1959.4/51833 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10500/SOURCE02?view=true.

MLA Handbook (7th Edition):

Findanis, Nicholas. “Asymmetrical localised synthetic jets in three-dimensional flows over bluff and streamlined bodies.” 2012. Web. 18 Aug 2019.

Vancouver:

Findanis N. Asymmetrical localised synthetic jets in three-dimensional flows over bluff and streamlined bodies. [Internet] [Doctoral dissertation]. University of New South Wales; 2012. [cited 2019 Aug 18]. Available from: http://handle.unsw.edu.au/1959.4/51833 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10500/SOURCE02?view=true.

Council of Science Editors:

Findanis N. Asymmetrical localised synthetic jets in three-dimensional flows over bluff and streamlined bodies. [Doctoral Dissertation]. University of New South Wales; 2012. Available from: http://handle.unsw.edu.au/1959.4/51833 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:10500/SOURCE02?view=true

23. Bonne, Nicolas. Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction.

Degree: Docteur es, Mécanique des fluides, 2018, Paris Saclay

 Le phénomène d’interaction onde de choc/couche limite (CL) est omniprésent en aérodynamique. De manière générale, il génère des oscillations basses fréquences qui peuvent être néfastes… (more)

Subjects/Keywords: Stabilité globale; Choc; Couche limite; Transition; Séparation; RANS; Global stability; Shock; Boundary layer; Transition; Separation; RANS; 532.059 3

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APA (6th Edition):

Bonne, N. (2018). Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction. (Doctoral Dissertation). Paris Saclay. Retrieved from http://www.theses.fr/2018SACLX025

Chicago Manual of Style (16th Edition):

Bonne, Nicolas. “Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction.” 2018. Doctoral Dissertation, Paris Saclay. Accessed August 18, 2019. http://www.theses.fr/2018SACLX025.

MLA Handbook (7th Edition):

Bonne, Nicolas. “Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction.” 2018. Web. 18 Aug 2019.

Vancouver:

Bonne N. Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction. [Internet] [Doctoral dissertation]. Paris Saclay; 2018. [cited 2019 Aug 18]. Available from: http://www.theses.fr/2018SACLX025.

Council of Science Editors:

Bonne N. Stabilité de l'intéraction onde de choc/ couche limite laminaire : Stability of the shock wave/ laminar boundary layer interaction. [Doctoral Dissertation]. Paris Saclay; 2018. Available from: http://www.theses.fr/2018SACLX025


Indian Institute of Science

24. Das, Shyama Prasad. An Experimental Study Of Instabilities In Unsteady Separation Bubbles.

Degree: 2006, Indian Institute of Science

 The present thesis is an experimental study of some aspects of unsteady two dimensional boundary layers subject to adverse pressure gradient. An adverse pressure gradient… (more)

Subjects/Keywords: Boundary Layer Problems; Mechanical Engineering; Bubbles - Instability; Unsteady Flows; Particle Image Velocimetry (PIV); Unsteady Two Dimensional Boundary Layers; Flow Visualization; Particle Visualization; LIF Visualization; Unsteady Separation; Unsteady Boundary Layer; Applied Mechanics

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APA (6th Edition):

Das, S. P. (2006). An Experimental Study Of Instabilities In Unsteady Separation Bubbles. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/290

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):

Das, Shyama Prasad. “An Experimental Study Of Instabilities In Unsteady Separation Bubbles.” 2006. Thesis, Indian Institute of Science. Accessed August 18, 2019. http://hdl.handle.net/2005/290.

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

MLA Handbook (7th Edition):

Das, Shyama Prasad. “An Experimental Study Of Instabilities In Unsteady Separation Bubbles.” 2006. Web. 18 Aug 2019.

Vancouver:

Das SP. An Experimental Study Of Instabilities In Unsteady Separation Bubbles. [Internet] [Thesis]. Indian Institute of Science; 2006. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2005/290.

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

Council of Science Editors:

Das SP. An Experimental Study Of Instabilities In Unsteady Separation Bubbles. [Thesis]. Indian Institute of Science; 2006. Available from: http://hdl.handle.net/2005/290

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

25. Cuvier, Christophe. Contrôle actif du décollement d’une couche limite turbulente en gradient de pression adverse : Active control of a separated turbulent boundary layer in adverse pressure gradient.

Degree: Docteur es, Mécanique, 2012, Ecole centrale de Lille

Le contrôle d’écoulement permet d’éliminer le phénomène de décollement de couches limites, très néfaste pour les performances des machines interagissant avec un fluide (avions, voitures,… (more)

Subjects/Keywords: Couche limite; Turbulence; Gradient de pression adverse; PIV; Contrôle d'écoulements; Décollement; Générateurs de vortex; Boundary layer; Turbulence; Adverse pressure gradient; PIV; Flow control; Flow separation; Vortex generators

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

APA (6th Edition):

Cuvier, C. (2012). Contrôle actif du décollement d’une couche limite turbulente en gradient de pression adverse : Active control of a separated turbulent boundary layer in adverse pressure gradient. (Doctoral Dissertation). Ecole centrale de Lille. Retrieved from http://www.theses.fr/2012ECLI0015

Chicago Manual of Style (16th Edition):

Cuvier, Christophe. “Contrôle actif du décollement d’une couche limite turbulente en gradient de pression adverse : Active control of a separated turbulent boundary layer in adverse pressure gradient.” 2012. Doctoral Dissertation, Ecole centrale de Lille. Accessed August 18, 2019. http://www.theses.fr/2012ECLI0015.

MLA Handbook (7th Edition):

Cuvier, Christophe. “Contrôle actif du décollement d’une couche limite turbulente en gradient de pression adverse : Active control of a separated turbulent boundary layer in adverse pressure gradient.” 2012. Web. 18 Aug 2019.

Vancouver:

Cuvier C. Contrôle actif du décollement d’une couche limite turbulente en gradient de pression adverse : Active control of a separated turbulent boundary layer in adverse pressure gradient. [Internet] [Doctoral dissertation]. Ecole centrale de Lille; 2012. [cited 2019 Aug 18]. Available from: http://www.theses.fr/2012ECLI0015.

Council of Science Editors:

Cuvier C. Contrôle actif du décollement d’une couche limite turbulente en gradient de pression adverse : Active control of a separated turbulent boundary layer in adverse pressure gradient. [Doctoral Dissertation]. Ecole centrale de Lille; 2012. Available from: http://www.theses.fr/2012ECLI0015

26. Ahmed, Ishtiaq. The interaction of synthetic jets with attached and separating turbulent boundary layer.

Degree: PhD, 2014, University of Manchester

 Like virtually every other human activity, air transport has an impact on the environment and similar to all other industries environmental impacts and economic issues… (more)

Subjects/Keywords: 629.132; Flow separation, Boundary layer, Synthetic jet actuator, vortical structures

boundary layer upstream of the separation line. The effectiveness of each type of vortices has… …undesirable from a control point of view. Separation resulting from shock wave/boundary-layer… …environment are explained. 2.1 Flow separation 2.1.1 Boundary layer separation The present… …region is termed as the boundary layer. Furthermore Prandtl concluded that the flow separation… …89 Figure 3.19 Schematic of the Boundary Layer triggered by a circular round wire94… 

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APA (6th Edition):

Ahmed, I. (2014). The interaction of synthetic jets with attached and separating turbulent boundary layer. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/the-interaction-of-synthetic-jets-with-attached-and-separating-turbulent-boundary-layer(1c09d1b2-ca0f-4e60-afc9-8279d879747b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617971

Chicago Manual of Style (16th Edition):

Ahmed, Ishtiaq. “The interaction of synthetic jets with attached and separating turbulent boundary layer.” 2014. Doctoral Dissertation, University of Manchester. Accessed August 18, 2019. https://www.research.manchester.ac.uk/portal/en/theses/the-interaction-of-synthetic-jets-with-attached-and-separating-turbulent-boundary-layer(1c09d1b2-ca0f-4e60-afc9-8279d879747b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617971.

MLA Handbook (7th Edition):

Ahmed, Ishtiaq. “The interaction of synthetic jets with attached and separating turbulent boundary layer.” 2014. Web. 18 Aug 2019.

Vancouver:

Ahmed I. The interaction of synthetic jets with attached and separating turbulent boundary layer. [Internet] [Doctoral dissertation]. University of Manchester; 2014. [cited 2019 Aug 18]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/the-interaction-of-synthetic-jets-with-attached-and-separating-turbulent-boundary-layer(1c09d1b2-ca0f-4e60-afc9-8279d879747b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617971.

Council of Science Editors:

Ahmed I. The interaction of synthetic jets with attached and separating turbulent boundary layer. [Doctoral Dissertation]. University of Manchester; 2014. Available from: https://www.research.manchester.ac.uk/portal/en/theses/the-interaction-of-synthetic-jets-with-attached-and-separating-turbulent-boundary-layer(1c09d1b2-ca0f-4e60-afc9-8279d879747b).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617971


University of Florida

27. Innocent, Douglas G. Design of a High Capacity Breakaway Connection for Multi-Post Ground Signs.

Degree: M.E., Civil Engineering - Civil and Coastal Engineering, 2016, University of Florida

 The primary objective of this study was to develop a high capacity breakaway connection, with the capacity to resist 150 mph design wind loads with… (more)

Subjects/Keywords: Acceleration; Accelerometers; Boundary layer separation; Breakaway supports; Impact tests; Impact velocity; Posts; Simulations; Statics; Steels; acceleration  – breakaway  – engineering  – hardware  – impact  – occupant  – ridedown  – roadside  – safety  – structural  – velocity

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

APA (6th Edition):

Innocent, D. G. (2016). Design of a High Capacity Breakaway Connection for Multi-Post Ground Signs. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0050496

Chicago Manual of Style (16th Edition):

Innocent, Douglas G. “Design of a High Capacity Breakaway Connection for Multi-Post Ground Signs.” 2016. Masters Thesis, University of Florida. Accessed August 18, 2019. http://ufdc.ufl.edu/UFE0050496.

MLA Handbook (7th Edition):

Innocent, Douglas G. “Design of a High Capacity Breakaway Connection for Multi-Post Ground Signs.” 2016. Web. 18 Aug 2019.

Vancouver:

Innocent DG. Design of a High Capacity Breakaway Connection for Multi-Post Ground Signs. [Internet] [Masters thesis]. University of Florida; 2016. [cited 2019 Aug 18]. Available from: http://ufdc.ufl.edu/UFE0050496.

Council of Science Editors:

Innocent DG. Design of a High Capacity Breakaway Connection for Multi-Post Ground Signs. [Masters Thesis]. University of Florida; 2016. Available from: http://ufdc.ufl.edu/UFE0050496


Virginia Tech

28. Thompson, Andrew Capers. Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade.

Degree: MS, Mechanical Engineering, 2009, Virginia Tech

 An investigation of ion flow control was performed to determine the effect of a positive, DC corona discharge on the boundary layer profile along a… (more)

Subjects/Keywords: active flow control; plasma; corona discharge; separation; compressor cascade; boundary layer transition

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APA (6th Edition):

Thompson, A. C. (2009). Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/33078

Chicago Manual of Style (16th Edition):

Thompson, Andrew Capers. “Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade.” 2009. Masters Thesis, Virginia Tech. Accessed August 18, 2019. http://hdl.handle.net/10919/33078.

MLA Handbook (7th Edition):

Thompson, Andrew Capers. “Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade.” 2009. Web. 18 Aug 2019.

Vancouver:

Thompson AC. Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade. [Internet] [Masters thesis]. Virginia Tech; 2009. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10919/33078.

Council of Science Editors:

Thompson AC. Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade. [Masters Thesis]. Virginia Tech; 2009. Available from: http://hdl.handle.net/10919/33078

29. Ma, Wei. Experimental investigation of corner stall in a linear compressor cascade : Etude expérimentale et numérique du décollement de coin dans une grille d'aubes de compresseur.

Degree: Docteur es, Mécanique, Energétique, Génie Civil et Acoustique, 2012, Ecully, Ecole centrale de Lyon

 Dans le domaine de la recherche appliquée, les turbomachinistes sont confrontés à un manque de compréhension de la physique du décollement de coin. Ce décollement… (more)

Subjects/Keywords: Grilles d'aubes de compresseur; Décollement de coin; Bases de données expérimentale; Couche limite turbulente; Histogrammes bimodaux; Compressor cascade; Corner stall; Corner separation; Experimental data; Turbulent boundary layer; Bimodal histograms

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

APA (6th Edition):

Ma, W. (2012). Experimental investigation of corner stall in a linear compressor cascade : Etude expérimentale et numérique du décollement de coin dans une grille d'aubes de compresseur. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon. Retrieved from http://www.theses.fr/2012ECDL0002

Chicago Manual of Style (16th Edition):

Ma, Wei. “Experimental investigation of corner stall in a linear compressor cascade : Etude expérimentale et numérique du décollement de coin dans une grille d'aubes de compresseur.” 2012. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed August 18, 2019. http://www.theses.fr/2012ECDL0002.

MLA Handbook (7th Edition):

Ma, Wei. “Experimental investigation of corner stall in a linear compressor cascade : Etude expérimentale et numérique du décollement de coin dans une grille d'aubes de compresseur.” 2012. Web. 18 Aug 2019.

Vancouver:

Ma W. Experimental investigation of corner stall in a linear compressor cascade : Etude expérimentale et numérique du décollement de coin dans une grille d'aubes de compresseur. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2012. [cited 2019 Aug 18]. Available from: http://www.theses.fr/2012ECDL0002.

Council of Science Editors:

Ma W. Experimental investigation of corner stall in a linear compressor cascade : Etude expérimentale et numérique du décollement de coin dans une grille d'aubes de compresseur. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; 2012. Available from: http://www.theses.fr/2012ECDL0002


University of Texas – Austin

30. Narayanaswamy, Venkateswa. Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control.

Degree: Aerospace Engineering and Engineering Mechanics, 2010, University of Texas – Austin

 A pulsed-plasma jet (called a "spark-jet" by other researchers), is a high-speed synthetic jet that is generated by striking an electrical discharge in a small… (more)

Subjects/Keywords: Shock wave boundary layer interaction; Plasma flow control; Pulsed jets; Spark-jet; Pulsed-plasma jet; Supersonic flow control; Flow control; Separation shock

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

APA (6th Edition):

Narayanaswamy, V. (2010). Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2010-05-1400

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):

Narayanaswamy, Venkateswa. “Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control.” 2010. Thesis, University of Texas – Austin. Accessed August 18, 2019. http://hdl.handle.net/2152/ETD-UT-2010-05-1400.

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

MLA Handbook (7th Edition):

Narayanaswamy, Venkateswa. “Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control.” 2010. Web. 18 Aug 2019.

Vancouver:

Narayanaswamy V. Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. [Internet] [Thesis]. University of Texas – Austin; 2010. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1400.

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

Council of Science Editors:

Narayanaswamy V. Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. [Thesis]. University of Texas – Austin; 2010. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1400

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

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