Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(laminar flow control). Showing records 1 – 30 of 33 total matches.

[1] [2]

Search Limiters

Last 2 Years | English Only

▼ Search Limiters


Brunel University

1. Hayes-McCoy, Declan. Direct computations of a synthetic jet actuator.

Degree: PhD, 2012, Brunel University

 Synthetic jet actuators have previously been defined as having potential use in both internal and external aerodynamic applications. The formation of a jet flow perpendicular… (more)

Subjects/Keywords: 533.62; Flow control; Laminar; Turbulent

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hayes-McCoy, D. (2012). Direct computations of a synthetic jet actuator. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/6454 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553641

Chicago Manual of Style (16th Edition):

Hayes-McCoy, Declan. “Direct computations of a synthetic jet actuator.” 2012. Doctoral Dissertation, Brunel University. Accessed December 08, 2019. http://bura.brunel.ac.uk/handle/2438/6454 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553641.

MLA Handbook (7th Edition):

Hayes-McCoy, Declan. “Direct computations of a synthetic jet actuator.” 2012. Web. 08 Dec 2019.

Vancouver:

Hayes-McCoy D. Direct computations of a synthetic jet actuator. [Internet] [Doctoral dissertation]. Brunel University; 2012. [cited 2019 Dec 08]. Available from: http://bura.brunel.ac.uk/handle/2438/6454 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553641.

Council of Science Editors:

Hayes-McCoy D. Direct computations of a synthetic jet actuator. [Doctoral Dissertation]. Brunel University; 2012. Available from: http://bura.brunel.ac.uk/handle/2438/6454 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.553641


University of Cambridge

2. Saeed, Tariq Issam. Conceptual design for a laminar-flying-wing aircraft.

Degree: PhD, 2012, University of Cambridge

 The laminar-flying-wing aircraft appears to be an attractive long-term prospect for reducing the environmental impact of commercial aviation. In assessing its potential, a relatively straightforward… (more)

Subjects/Keywords: 620; Laminar flow control; Flying wing aircraft

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Saeed, T. I. (2012). Conceptual design for a laminar-flying-wing aircraft. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/243926 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.559058

Chicago Manual of Style (16th Edition):

Saeed, Tariq Issam. “Conceptual design for a laminar-flying-wing aircraft.” 2012. Doctoral Dissertation, University of Cambridge. Accessed December 08, 2019. https://www.repository.cam.ac.uk/handle/1810/243926 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.559058.

MLA Handbook (7th Edition):

Saeed, Tariq Issam. “Conceptual design for a laminar-flying-wing aircraft.” 2012. Web. 08 Dec 2019.

Vancouver:

Saeed TI. Conceptual design for a laminar-flying-wing aircraft. [Internet] [Doctoral dissertation]. University of Cambridge; 2012. [cited 2019 Dec 08]. Available from: https://www.repository.cam.ac.uk/handle/1810/243926 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.559058.

Council of Science Editors:

Saeed TI. Conceptual design for a laminar-flying-wing aircraft. [Doctoral Dissertation]. University of Cambridge; 2012. Available from: https://www.repository.cam.ac.uk/handle/1810/243926 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.559058


University of Arizona

3. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 December 08, 2019. http://hdl.handle.net/10150/630146.

MLA Handbook (7th Edition):

Balthazar, Michael Aeko. “Experimental Investigation of Boundary Layer Separation .” 2018. Web. 08 Dec 2019.

Vancouver:

Balthazar MA. Experimental Investigation of Boundary Layer Separation . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2019 Dec 08]. 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


University of Illinois – Urbana-Champaign

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

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

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Thesis, University of Illinois – Urbana-Champaign. Accessed December 08, 2019. http://hdl.handle.net/2142/92747.

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

MLA Handbook (7th Edition):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Web. 08 Dec 2019.

Vancouver:

Gupta R. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2016. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2142/92747.

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

Council of Science Editors:

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

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


University of Illinois – Urbana-Champaign

5. Collazo Garcia III, Armando Rafael. Aerodynamic characterization of a Griffith-type transonic, laminar-flow airfoil.

Degree: MS, Aerospace Engineering, 2019, University of Illinois – Urbana-Champaign

 An experimental investigation was conducted at the University of Illinois’ Transonic Wind Tunnel Facility on a Griffith-type transonic airfoil to evaluate the effectiveness of its… (more)

Subjects/Keywords: transonic; laminar flow; flow control; airfoil; wind tunnel

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Collazo Garcia III, A. R. (2019). Aerodynamic characterization of a Griffith-type transonic, laminar-flow airfoil. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/104909

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):

Collazo Garcia III, Armando Rafael. “Aerodynamic characterization of a Griffith-type transonic, laminar-flow airfoil.” 2019. Thesis, University of Illinois – Urbana-Champaign. Accessed December 08, 2019. http://hdl.handle.net/2142/104909.

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

MLA Handbook (7th Edition):

Collazo Garcia III, Armando Rafael. “Aerodynamic characterization of a Griffith-type transonic, laminar-flow airfoil.” 2019. Web. 08 Dec 2019.

Vancouver:

Collazo Garcia III AR. Aerodynamic characterization of a Griffith-type transonic, laminar-flow airfoil. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2019. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2142/104909.

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

Council of Science Editors:

Collazo Garcia III AR. Aerodynamic characterization of a Griffith-type transonic, laminar-flow airfoil. [Thesis]. University of Illinois – Urbana-Champaign; 2019. Available from: http://hdl.handle.net/2142/104909

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


Texas A&M University

6. Rhodes, Richard G. Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research.

Degree: 2010, Texas A&M University

 The high cost of energy has resulted in a renewed interest in the study of reducing skin-friction drag in aeronautical applications. Laminar Flow Control (LFC)… (more)

Subjects/Keywords: laminar; turbulence; flow; control; fluent; gambit; crossflow; lastrac

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rhodes, R. G. (2010). Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96

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):

Rhodes, Richard G. “Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research.” 2010. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96.

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

MLA Handbook (7th Edition):

Rhodes, Richard G. “Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research.” 2010. Web. 08 Dec 2019.

Vancouver:

Rhodes RG. Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96.

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

Council of Science Editors:

Rhodes RG. Computations of Laminar Flow Control on Swept Wings as a Companion to Flight Test Research. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2008-12-96

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


The Ohio State University

7. Thake, Michael Patrick, Jr. Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number.

Degree: MS, Aero/Astro Engineering, 2011, The Ohio State University

 Wind tunnel tests are performed on a NACA 643-618 airfoil at Reynolds numbers of 6.4x104, 1.8x105, 1.0x106, and 4.0x106 in order study several aspects of… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; laminar airfoil; aerodynamics; flow control; Reynolds number; separation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Thake, Michael Patrick, J. (2011). Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1292962211

Chicago Manual of Style (16th Edition):

Thake, Michael Patrick, Jr. “Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number.” 2011. Masters Thesis, The Ohio State University. Accessed December 08, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1292962211.

MLA Handbook (7th Edition):

Thake, Michael Patrick, Jr. “Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number.” 2011. Web. 08 Dec 2019.

Vancouver:

Thake, Michael Patrick J. Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number. [Internet] [Masters thesis]. The Ohio State University; 2011. [cited 2019 Dec 08]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1292962211.

Council of Science Editors:

Thake, Michael Patrick J. Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number. [Masters Thesis]. The Ohio State University; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1292962211


University of Manchester

8. Valenzuela Calva, Fernando. Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation.

Degree: 2016, University of Manchester

In 2009, based on its commitment to take action on the climate change, the aviation industry accorded a group of objectives to reduce carbon dioxide… (more)

Subjects/Keywords: synthetic jets; flow control; jet orientation; detached laminar boundary layer

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Valenzuela Calva, F. (2016). Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302245

Chicago Manual of Style (16th Edition):

Valenzuela Calva, Fernando. “Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation.” 2016. Doctoral Dissertation, University of Manchester. Accessed December 08, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302245.

MLA Handbook (7th Edition):

Valenzuela Calva, Fernando. “Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation.” 2016. Web. 08 Dec 2019.

Vancouver:

Valenzuela Calva F. Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Dec 08]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302245.

Council of Science Editors:

Valenzuela Calva F. Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:302245


North Carolina State University

9. McGowan, Gregory Zar. Computational Analysis of Circulation Control Airfoils.

Degree: MS, Aerospace Engineering, 2004, North Carolina State University

 Current projections for future aircraft concepts call for stringent requirements on high-lift and low cruise-drag. The purpose of this study is to examine the use… (more)

Subjects/Keywords: Circulation Control; airfoils; laminar flow

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

McGowan, G. Z. (2004). Computational Analysis of Circulation Control Airfoils. (Thesis). North Carolina State University. Retrieved from http://www.lib.ncsu.edu/resolver/1840.16/2508

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):

McGowan, Gregory Zar. “Computational Analysis of Circulation Control Airfoils.” 2004. Thesis, North Carolina State University. Accessed December 08, 2019. http://www.lib.ncsu.edu/resolver/1840.16/2508.

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

MLA Handbook (7th Edition):

McGowan, Gregory Zar. “Computational Analysis of Circulation Control Airfoils.” 2004. Web. 08 Dec 2019.

Vancouver:

McGowan GZ. Computational Analysis of Circulation Control Airfoils. [Internet] [Thesis]. North Carolina State University; 2004. [cited 2019 Dec 08]. Available from: http://www.lib.ncsu.edu/resolver/1840.16/2508.

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

Council of Science Editors:

McGowan GZ. Computational Analysis of Circulation Control Airfoils. [Thesis]. North Carolina State University; 2004. Available from: http://www.lib.ncsu.edu/resolver/1840.16/2508

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


University of Manchester

10. Valenzuela Calva, Fernando. Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation.

Degree: PhD, 2016, University of Manchester

 In 2009, based on its commitment to take action on the climate change, the aviation industry accorded a group of objectives to reduce carbon dioxide… (more)

Subjects/Keywords: 629.133; detached laminar boundary layer; jet orientation; synthetic jets; flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Valenzuela Calva, F. (2016). Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-interaction-of-synthetic-jets-with-a-laminar-boundary-layer-and-the-effect-of-jet-orientation(5cc80987-a9e1-48ac-9e0f-18067c5f48fe).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727917

Chicago Manual of Style (16th Edition):

Valenzuela Calva, Fernando. “Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation.” 2016. Doctoral Dissertation, University of Manchester. Accessed December 08, 2019. https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-interaction-of-synthetic-jets-with-a-laminar-boundary-layer-and-the-effect-of-jet-orientation(5cc80987-a9e1-48ac-9e0f-18067c5f48fe).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727917.

MLA Handbook (7th Edition):

Valenzuela Calva, Fernando. “Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation.” 2016. Web. 08 Dec 2019.

Vancouver:

Valenzuela Calva F. Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Dec 08]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-interaction-of-synthetic-jets-with-a-laminar-boundary-layer-and-the-effect-of-jet-orientation(5cc80987-a9e1-48ac-9e0f-18067c5f48fe).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727917.

Council of Science Editors:

Valenzuela Calva F. Numerical investigation of the interaction of synthetic jets with a laminar boundary layer and the effect of jet orientation. [Doctoral Dissertation]. University of Manchester; 2016. Available from: https://www.research.manchester.ac.uk/portal/en/theses/numerical-investigation-of-the-interaction-of-synthetic-jets-with-a-laminar-boundary-layer-and-the-effect-of-jet-orientation(5cc80987-a9e1-48ac-9e0f-18067c5f48fe).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.727917


University of Illinois – Urbana-Champaign

11. Colletti, Christopher. Investigating the frequency behavior of fluidic oscillators and their application as active flow control for an SNLF airfoil.

Degree: MS, Aerospace Engineering, 2019, University of Illinois – Urbana-Champaign

 This current study was performed to investigate the effect of geometric variation on the frequency behavior of fluidic oscillators. Fluidic oscillators are able to passively… (more)

Subjects/Keywords: Fluidic Oscillator; S414; Active Flow Control; Aerodynamics; Natural Laminar Flow; Multi Element Airfoil

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Colletti, C. (2019). Investigating the frequency behavior of fluidic oscillators and their application as active flow control for an SNLF airfoil. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/104907

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):

Colletti, Christopher. “Investigating the frequency behavior of fluidic oscillators and their application as active flow control for an SNLF airfoil.” 2019. Thesis, University of Illinois – Urbana-Champaign. Accessed December 08, 2019. http://hdl.handle.net/2142/104907.

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

MLA Handbook (7th Edition):

Colletti, Christopher. “Investigating the frequency behavior of fluidic oscillators and their application as active flow control for an SNLF airfoil.” 2019. Web. 08 Dec 2019.

Vancouver:

Colletti C. Investigating the frequency behavior of fluidic oscillators and their application as active flow control for an SNLF airfoil. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2019. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2142/104907.

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

Council of Science Editors:

Colletti C. Investigating the frequency behavior of fluidic oscillators and their application as active flow control for an SNLF airfoil. [Thesis]. University of Illinois – Urbana-Champaign; 2019. Available from: http://hdl.handle.net/2142/104907

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


University of Manchester

12. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 December 08, 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. 08 Dec 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 Dec 08]. 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

13. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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 December 08, 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. 08 Dec 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 Dec 08]. 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


Texas A&M University

14. Belisle, Michael Joseph. Aerodynamic Design for Swept-wing Laminar Flow.

Degree: 2013, Texas A&M University

 This work describes and compares processes for swept-wing laminar flow control (SWLFC) aerody-namic design. It focuses on results obtained during the preliminary outer-mold-line (OML) design… (more)

Subjects/Keywords: aircraft; aerodynamic design; boundary-layer stability; boundary-layer transition; crossflow instability; discrete roughness elements; drag reduction; flight test; laminar flow control; natural laminar flow; swept-wing laminar flow control; wing design; wing glove

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Belisle, M. J. (2013). Aerodynamic Design for Swept-wing Laminar Flow. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151655

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):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/151655.

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

MLA Handbook (7th Edition):

Belisle, Michael Joseph. “Aerodynamic Design for Swept-wing Laminar Flow.” 2013. Web. 08 Dec 2019.

Vancouver:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/151655.

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

Council of Science Editors:

Belisle MJ. Aerodynamic Design for Swept-wing Laminar Flow. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151655

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


University of Waterloo

15. Gerakopulos, Ryan. Investing Flow over an Airfoil at Low Reynolds Numbers Using Novel Time-Resolved Surface Pressure Measurements.

Degree: 2011, University of Waterloo

 An aluminum NACA 0018 airfoil testbed was constructed with 95 static pressure taps and 25 embedded microphones to enable novel time-resolved measurements of surface pressure.… (more)

Subjects/Keywords: aerodynamics; flow control; low Reynolds number; laminar; transition; airfoil; flow development; embedded microphones; aerospace; wind turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gerakopulos, R. (2011). Investing Flow over an Airfoil at Low Reynolds Numbers Using Novel Time-Resolved Surface Pressure Measurements. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/5832

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):

Gerakopulos, Ryan. “Investing Flow over an Airfoil at Low Reynolds Numbers Using Novel Time-Resolved Surface Pressure Measurements.” 2011. Thesis, University of Waterloo. Accessed December 08, 2019. http://hdl.handle.net/10012/5832.

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

MLA Handbook (7th Edition):

Gerakopulos, Ryan. “Investing Flow over an Airfoil at Low Reynolds Numbers Using Novel Time-Resolved Surface Pressure Measurements.” 2011. Web. 08 Dec 2019.

Vancouver:

Gerakopulos R. Investing Flow over an Airfoil at Low Reynolds Numbers Using Novel Time-Resolved Surface Pressure Measurements. [Internet] [Thesis]. University of Waterloo; 2011. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/10012/5832.

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

Council of Science Editors:

Gerakopulos R. Investing Flow over an Airfoil at Low Reynolds Numbers Using Novel Time-Resolved Surface Pressure Measurements. [Thesis]. University of Waterloo; 2011. Available from: http://hdl.handle.net/10012/5832

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


KTH

16. Roy, Arijit Sinha. Analysis and control of boundary layer transition on a NACA 0008 wing profile.

Degree: Mechanics, 2018, KTH

  The main aim of this thesis was to understand the mechanism behind the classical transition scenario inside the boundary layer over an airfoil and… (more)

Subjects/Keywords: boundary layer stability; laminar - turbulent transition; laminar flow control; Tollmien-Schlichting waves; streaky boundary layers; miniature vortex generators; Falkner-Skan boundary layer.; Engineering and Technology; Teknik och teknologier

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Roy, A. S. (2018). Analysis and control of boundary layer transition on a NACA 0008 wing profile. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931

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):

Roy, Arijit Sinha. “Analysis and control of boundary layer transition on a NACA 0008 wing profile.” 2018. Thesis, KTH. Accessed December 08, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931.

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

MLA Handbook (7th Edition):

Roy, Arijit Sinha. “Analysis and control of boundary layer transition on a NACA 0008 wing profile.” 2018. Web. 08 Dec 2019.

Vancouver:

Roy AS. Analysis and control of boundary layer transition on a NACA 0008 wing profile. [Internet] [Thesis]. KTH; 2018. [cited 2019 Dec 08]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931.

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

Council of Science Editors:

Roy AS. Analysis and control of boundary layer transition on a NACA 0008 wing profile. [Thesis]. KTH; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-239931

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


University of Adelaide

17. Choudhry, Amanullah. Unsteady separation control on wind turbine blades.

Degree: 2015, University of Adelaide

 Dynamic stall is one of the primary causes of unsteady loads on wind turbine blades. The process can be instigated by a multitude of factors,… (more)

Subjects/Keywords: dynamic stall; wind turbines; unsteady separation; passive flow control; dynamic stall prediction; laminar separation bubble; airfoil; lift

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Choudhry, A. (2015). Unsteady separation control on wind turbine blades. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/101653

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):

Choudhry, Amanullah. “Unsteady separation control on wind turbine blades.” 2015. Thesis, University of Adelaide. Accessed December 08, 2019. http://hdl.handle.net/2440/101653.

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

MLA Handbook (7th Edition):

Choudhry, Amanullah. “Unsteady separation control on wind turbine blades.” 2015. Web. 08 Dec 2019.

Vancouver:

Choudhry A. Unsteady separation control on wind turbine blades. [Internet] [Thesis]. University of Adelaide; 2015. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2440/101653.

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

Council of Science Editors:

Choudhry A. Unsteady separation control on wind turbine blades. [Thesis]. University of Adelaide; 2015. Available from: http://hdl.handle.net/2440/101653

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

18. Saeed, Tariq Issam. Conceptual design for a laminar-flying-wing aircraft .

Degree: 2012, University of Cambridge

 The laminar-flying-wing aircraft appears to be an attractive long-term prospect for reducing the environmental impact of commercial aviation. In assessing its potential, a relatively straightforward… (more)

Subjects/Keywords: Laminar flow control; Flying wing aircraft

…Nomenclature xxix 1 Introduction 1 2 Literature Review 7 2.1 Laminar Flow Control… …18 2.11 Outline for a laminar flow control system (from Edwards (1977))… …suction pump LCV = low calorific value te = trailing edge LFC = laminar flow control th… …open literature on laminar flow control, flying wing aircraft, and studies which combine the… …this research aims to: provide insight into the parameters affecting practical laminar-flow… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Saeed, T. I. (2012). Conceptual design for a laminar-flying-wing aircraft . (Thesis). University of Cambridge. Retrieved from http://www.dspace.cam.ac.uk/handle/1810/243926

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):

Saeed, Tariq Issam. “Conceptual design for a laminar-flying-wing aircraft .” 2012. Thesis, University of Cambridge. Accessed December 08, 2019. http://www.dspace.cam.ac.uk/handle/1810/243926.

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

MLA Handbook (7th Edition):

Saeed, Tariq Issam. “Conceptual design for a laminar-flying-wing aircraft .” 2012. Web. 08 Dec 2019.

Vancouver:

Saeed TI. Conceptual design for a laminar-flying-wing aircraft . [Internet] [Thesis]. University of Cambridge; 2012. [cited 2019 Dec 08]. Available from: http://www.dspace.cam.ac.uk/handle/1810/243926.

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

Council of Science Editors:

Saeed TI. Conceptual design for a laminar-flying-wing aircraft . [Thesis]. University of Cambridge; 2012. Available from: http://www.dspace.cam.ac.uk/handle/1810/243926

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

19. Woodruff, Matthew Jeffery. Receptivity Studies on a Swept-Wing Model.

Degree: 2012, Texas A&M University

 A series of flight tests was performed using a swept-wing model mounted on a Cessna O-2 aircraft. The crossflow waves on the airfoil were excited… (more)

Subjects/Keywords: laminar flow control; laminar to turbulent transition; swept wing flow control

…the last major hurdle in swept-wing laminar flow control (SWLFC) (Saric… …for this series of tests, and a painted leading edge that is used for laminar flow control… …design natural laminar flow airfoils. While both the linear Orr-Sommerfeld equation and linear… …linear solvers compared to experimental results It is well known that laminar flow over a wing… …variations from crossflow in the saturated region of a laminar flow airfoil, and a calibration… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Woodruff, M. J. (2012). Receptivity Studies on a Swept-Wing Model. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119

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):

Woodruff, Matthew Jeffery. “Receptivity Studies on a Swept-Wing Model.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119.

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

MLA Handbook (7th Edition):

Woodruff, Matthew Jeffery. “Receptivity Studies on a Swept-Wing Model.” 2012. Web. 08 Dec 2019.

Vancouver:

Woodruff MJ. Receptivity Studies on a Swept-Wing Model. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119.

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

Council of Science Editors:

Woodruff MJ. Receptivity Studies on a Swept-Wing Model. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2011-05-9119

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

20. Fanning, Joshua 1987-. In-Flight Measurements of Freestream Atmospheric Turbulence Intensities.

Degree: 2012, Texas A&M University

 The last key to implementing laminar flow control on swept-wings is controlling the crossflow instability. One promising technology is spanwise-periodic discrete roughness elements (DREs). Previous… (more)

Subjects/Keywords: Laminar Flow Control; DRE; Turbulence; Flight Test; Hotwire

…effectiveness and knowledge of Laminar Flow Control (LFC). Receptivity is the process by… …boundary layer, delaying transition, and increasing the extent of laminar flow over a wing the… …x29; plasma actuators. DBDs have been used in the past for different types of flow control… …and cause the transition from laminar to turbulent [1]. By stabilizing the… …encompasses techniques to control the instabilities that occur on swept-wings. Multiple… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Fanning, J. 1. (2012). In-Flight Measurements of Freestream Atmospheric Turbulence Intensities. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148376

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):

Fanning, Joshua 1987-. “In-Flight Measurements of Freestream Atmospheric Turbulence Intensities.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/148376.

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

MLA Handbook (7th Edition):

Fanning, Joshua 1987-. “In-Flight Measurements of Freestream Atmospheric Turbulence Intensities.” 2012. Web. 08 Dec 2019.

Vancouver:

Fanning J1. In-Flight Measurements of Freestream Atmospheric Turbulence Intensities. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/148376.

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

Council of Science Editors:

Fanning J1. In-Flight Measurements of Freestream Atmospheric Turbulence Intensities. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148376

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

21. Szulga, Natacha. Étude expérimentale et numérique du contrôle de transition de couche limite par actionneurs à plasma froid surfacique : Experimental and numerical study of boundary layer transition control by means of cold surface plasma actuators.

Degree: Docteur es, Dynamique des fluides, 2016, Toulouse, ISAE

La transition laminaire-turbulent au sein de la couche limite qui se développesur les parois des aéronefs augmente fortement la traînée de frottement. Ainsi, afin derépondre… (more)

Subjects/Keywords: Transition laminaire/turbulent; Couche limite; Actionneurs à plasma; Contrôle d’écoulement; Ondes de Tollmien-Schlichting; Laminar/turbulent transition; Boundary layer; Plasma actuators; Flow control; Tollmien-Schlichting waves; 532

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Szulga, N. (2016). Étude expérimentale et numérique du contrôle de transition de couche limite par actionneurs à plasma froid surfacique : Experimental and numerical study of boundary layer transition control by means of cold surface plasma actuators. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2016ESAE0032

Chicago Manual of Style (16th Edition):

Szulga, Natacha. “Étude expérimentale et numérique du contrôle de transition de couche limite par actionneurs à plasma froid surfacique : Experimental and numerical study of boundary layer transition control by means of cold surface plasma actuators.” 2016. Doctoral Dissertation, Toulouse, ISAE. Accessed December 08, 2019. http://www.theses.fr/2016ESAE0032.

MLA Handbook (7th Edition):

Szulga, Natacha. “Étude expérimentale et numérique du contrôle de transition de couche limite par actionneurs à plasma froid surfacique : Experimental and numerical study of boundary layer transition control by means of cold surface plasma actuators.” 2016. Web. 08 Dec 2019.

Vancouver:

Szulga N. Étude expérimentale et numérique du contrôle de transition de couche limite par actionneurs à plasma froid surfacique : Experimental and numerical study of boundary layer transition control by means of cold surface plasma actuators. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2016. [cited 2019 Dec 08]. Available from: http://www.theses.fr/2016ESAE0032.

Council of Science Editors:

Szulga N. Étude expérimentale et numérique du contrôle de transition de couche limite par actionneurs à plasma froid surfacique : Experimental and numerical study of boundary layer transition control by means of cold surface plasma actuators. [Doctoral Dissertation]. Toulouse, ISAE; 2016. Available from: http://www.theses.fr/2016ESAE0032


Loughborough University

22. Mistry, Vinan I. Simulation and control of stationary crossflow vortices.

Degree: Thesis (Eng.D.), 2014, Loughborough University

 Turbulent flow and transition are some of the most important phenomena of fluid mechanics and aerodynamics and represent a challenging engineering problem for aircraft manufacturers… (more)

Subjects/Keywords: Large eddy simulation; Fluid mechanics; Computational fluid dynamics; Crossflow instability; Transition; Turbulence; Laminar; Turbulent; WALE; Synthetic eddy method; Distributed roughness elements; Flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mistry, V. I. (2014). Simulation and control of stationary crossflow vortices. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/16323 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756457

Chicago Manual of Style (16th Edition):

Mistry, Vinan I. “Simulation and control of stationary crossflow vortices.” 2014. Doctoral Dissertation, Loughborough University. Accessed December 08, 2019. https://dspace.lboro.ac.uk/2134/16323 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756457.

MLA Handbook (7th Edition):

Mistry, Vinan I. “Simulation and control of stationary crossflow vortices.” 2014. Web. 08 Dec 2019.

Vancouver:

Mistry VI. Simulation and control of stationary crossflow vortices. [Internet] [Doctoral dissertation]. Loughborough University; 2014. [cited 2019 Dec 08]. Available from: https://dspace.lboro.ac.uk/2134/16323 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756457.

Council of Science Editors:

Mistry VI. Simulation and control of stationary crossflow vortices. [Doctoral Dissertation]. Loughborough University; 2014. Available from: https://dspace.lboro.ac.uk/2134/16323 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.756457


Loughborough University

23. Mistry, Vinan I. Simulation and control of stationary crossflow vortices.

Degree: Thesis (Eng.D.), 2014, Loughborough University

 Turbulent flow and transition are some of the most important phenomena of fluid mechanics and aerodynamics and represent a challenging engineering problem for aircraft manufacturers… (more)

Subjects/Keywords: Large eddy simulation; Fluid mechanics; Computational fluid dynamics; Crossflow instability; Transition; Turbulence; Laminar; Turbulent; WALE; Synthetic eddy method; Distributed roughness elements; Flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mistry, V. I. (2014). Simulation and control of stationary crossflow vortices. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/16323

Chicago Manual of Style (16th Edition):

Mistry, Vinan I. “Simulation and control of stationary crossflow vortices.” 2014. Doctoral Dissertation, Loughborough University. Accessed December 08, 2019. http://hdl.handle.net/2134/16323.

MLA Handbook (7th Edition):

Mistry, Vinan I. “Simulation and control of stationary crossflow vortices.” 2014. Web. 08 Dec 2019.

Vancouver:

Mistry VI. Simulation and control of stationary crossflow vortices. [Internet] [Doctoral dissertation]. Loughborough University; 2014. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/2134/16323.

Council of Science Editors:

Mistry VI. Simulation and control of stationary crossflow vortices. [Doctoral Dissertation]. Loughborough University; 2014. Available from: http://hdl.handle.net/2134/16323

24. Roberts, Matthew William. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design.

Degree: 2012, Texas A&M University

 The aerodynamic benefits of laminar flow have long made it a sought-after attribute in aircraft design. By laminarizing portions of an aircraft, such as the… (more)

Subjects/Keywords: computational fluid dynamics; transonic; laminar flow; wing glove; boundary-layer stability; boundary-layer transition; laminar flow control; discrete roughness elements

…3 C. Laminar Flow Control… …further destabilized by a favorable pressure gradient. C. Laminar Flow Control By understanding… …x5B;10]. Laminar Flow Control and Hybrid Laminar Flow Control Active systems using wall… …Laminar flow control (LFC) describes the use of an active control system over the… …whole-wing chord. Hybrid laminar flow control (HLFC) employs a LFC system near the… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Roberts, M. W. (2012). Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857

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):

Roberts, Matthew William. “Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857.

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

MLA Handbook (7th Edition):

Roberts, Matthew William. “Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design.” 2012. Web. 08 Dec 2019.

Vancouver:

Roberts MW. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857.

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

Council of Science Editors:

Roberts MW. Computational Evaluation of a Transonic Laminar-Flow Wing Glove Design. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-05-10857

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

25. Neale, Tyler P. CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment.

Degree: 2011, Texas A&M University

Laminar flow control has been studied for several decades in an effort to achieve higher efficiencies for aircraft. Successful implementation of laminar flow control technology… (more)

Subjects/Keywords: Laminar flow control; crossflow; discrete roughness elements; aircraft CFD; turbofan simulation; airframe and turbofan integration

…1.1 1.2 1.3 1.4 1.5 2 Background in Laminar Flow Control… …Laminar Flow Control Techniques… …laminar flow control study. 1.1 Background in Laminar Flow Control The study of laminar flow… …breakdown in the boundary layer and eventually transition to turbulence. 1.3 Laminar Flow Control… …Techniques The challenge in achieving laminar flow for an aircraft comes from attempting to control… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Neale, T. P. (2011). CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889

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):

Neale, Tyler P. “CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment.” 2011. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889.

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

MLA Handbook (7th Edition):

Neale, Tyler P. “CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment.” 2011. Web. 08 Dec 2019.

Vancouver:

Neale TP. CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889.

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

Council of Science Editors:

Neale TP. CFD Investigations of a Transonic Swept-Wing Laminar Flow Control Flight Experiment. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7889

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

26. Tucker, Aaron 1975-. Laminar Flow Control Flight Experiment Design.

Degree: 2012, Texas A&M University

 Demonstration of spanwise-periodic discrete roughness element laminar flow control (DRE LFC) technology at operationally relevant flight regimes requires extremely stable flow conditions in flight. A… (more)

Subjects/Keywords: design of experiments; wing glove; flight test technique; flight test; flight research; laminar flow control

…11 Figure 7. X-21 laminar flow control aircraft… …28 Figure 16. Laminar flow control test flow… …periodic discrete roughness element laminar flow control (DRE LFC) technology at… …flight experiment. While these factors are applied to a laminar flow control flight experiment… …experience in laminar flow control flight research will be covered as it relates to the present… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Tucker, A. 1. (2012). Laminar Flow Control Flight Experiment Design. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/148399

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):

Tucker, Aaron 1975-. “Laminar Flow Control Flight Experiment Design.” 2012. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/148399.

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

MLA Handbook (7th Edition):

Tucker, Aaron 1975-. “Laminar Flow Control Flight Experiment Design.” 2012. Web. 08 Dec 2019.

Vancouver:

Tucker A1. Laminar Flow Control Flight Experiment Design. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/148399.

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

Council of Science Editors:

Tucker A1. Laminar Flow Control Flight Experiment Design. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/148399

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


University of Cincinnati

27. You, Lishan. Computational Modeling of Laminar Swirl Flows and Heat Transfer in Circular Tubes with Twisted-Tape Inserts.

Degree: MS, Engineering : Mechanical Engineering, 2002, University of Cincinnati

  A numerical study is carried out to predict the velocity and temperature distributions in fully developed, constant property, laminar flows in tubes containing twisted-tape… (more)

Subjects/Keywords: Engineering, Mechanical; swirl flow; twisted-tape insert; laminar; finite control volume method; heat transfer

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

You, L. (2002). Computational Modeling of Laminar Swirl Flows and Heat Transfer in Circular Tubes with Twisted-Tape Inserts. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1029525889

Chicago Manual of Style (16th Edition):

You, Lishan. “Computational Modeling of Laminar Swirl Flows and Heat Transfer in Circular Tubes with Twisted-Tape Inserts.” 2002. Masters Thesis, University of Cincinnati. Accessed December 08, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1029525889.

MLA Handbook (7th Edition):

You, Lishan. “Computational Modeling of Laminar Swirl Flows and Heat Transfer in Circular Tubes with Twisted-Tape Inserts.” 2002. Web. 08 Dec 2019.

Vancouver:

You L. Computational Modeling of Laminar Swirl Flows and Heat Transfer in Circular Tubes with Twisted-Tape Inserts. [Internet] [Masters thesis]. University of Cincinnati; 2002. [cited 2019 Dec 08]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1029525889.

Council of Science Editors:

You L. Computational Modeling of Laminar Swirl Flows and Heat Transfer in Circular Tubes with Twisted-Tape Inserts. [Masters Thesis]. University of Cincinnati; 2002. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1029525889

28. Clayton, Patrick. Development of high-lift laminar wing using steady active flow control.

Degree: 2013, Iowa State University

 Fuel costs represent a large fraction of aircraft operating costs. Increased aircraft fuel efficiency is thus desirable. Laminar airfoils have the advantage of reduced cruise… (more)

Subjects/Keywords: Active Flow Control; deflected flap; high-lift; laminar airfoil; multiple slot blowing; steady; Aerospace Engineering

…develop high-lift technology for laminar airfoils by using active flow control. 2 Flow… …flow control AoA – angle of attack BL – boundary layer PFC – passive flow control psf… …flow control has shown the ability to prevent or mitigate separation effects, and increase… …investigating the effects of steady active flow control from three slots, located at 1%, 10%, and 80… …Control Flow control can be described as altering an airfoil’s natural flow state and… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Clayton, P. (2013). Development of high-lift laminar wing using steady active flow control. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/13561

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):

Clayton, Patrick. “Development of high-lift laminar wing using steady active flow control.” 2013. Thesis, Iowa State University. Accessed December 08, 2019. https://lib.dr.iastate.edu/etd/13561.

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

MLA Handbook (7th Edition):

Clayton, Patrick. “Development of high-lift laminar wing using steady active flow control.” 2013. Web. 08 Dec 2019.

Vancouver:

Clayton P. Development of high-lift laminar wing using steady active flow control. [Internet] [Thesis]. Iowa State University; 2013. [cited 2019 Dec 08]. Available from: https://lib.dr.iastate.edu/etd/13561.

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

Council of Science Editors:

Clayton P. Development of high-lift laminar wing using steady active flow control. [Thesis]. Iowa State University; 2013. Available from: https://lib.dr.iastate.edu/etd/13561

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

29. West, David Edward. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.

Degree: 2014, Texas A&M University

 Micron-sized, spanwise-periodic, discrete roughness elements (DREs) were applied to and tested on a 30? swept-wing model in order to study their effects on boundary-layer transition… (more)

Subjects/Keywords: discrete roughness elements; DRE; laminar flow control; transition; laminar-turbulent; experiment; flight; swept wing; sensitivity; spanwise-periodic; Texas A&M; Flight Research Lab

…x28;DREs) as a reliable and consistent means of swept-wing laminar flow control in the… …FRL). This introduction encapsulates the motivation for laminar-flow control, the… …through laminar flow control (LFC) or more specifically the delaying of laminar… …particular control strategy for increasing laminar flow on a crossflow dominated swept wing. In… …effective DRE 13 configuration for laminar flow control. Recommendations will be made on the… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

West, D. E. (2014). Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154330

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):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/154330.

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

MLA Handbook (7th Edition):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Web. 08 Dec 2019.

Vancouver:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/154330.

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

Council of Science Editors:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154330

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

30. West, David Edward. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.

Degree: 2014, Texas A&M University

 Micron-sized, spanwise-periodic, discrete roughness elements (DREs) were applied to and tested on a 30? swept-wing model in order to study their effects on boundary-layer transition… (more)

Subjects/Keywords: discrete roughness elements; DRE; laminar flow control; transition; laminar-turbulent; experiment; flight; swept wing; sensitivity; spanwise-periodic; Texas A&M; Flight Research Lab

…x28;DREs) as a reliable and consistent means of swept-wing laminar flow control in the… …FRL). This introduction encapsulates the motivation for laminar-flow control, the… …through laminar flow control (LFC) or more specifically the delaying of laminar… …particular control strategy for increasing laminar flow on a crossflow dominated swept wing. In… …effective DRE 13 configuration for laminar flow control. Recommendations will be made on the… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

West, D. E. (2014). Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/154230

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):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Thesis, Texas A&M University. Accessed December 08, 2019. http://hdl.handle.net/1969.1/154230.

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

MLA Handbook (7th Edition):

West, David Edward. “Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements.” 2014. Web. 08 Dec 2019.

Vancouver:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Internet] [Thesis]. Texas A&M University; 2014. [cited 2019 Dec 08]. Available from: http://hdl.handle.net/1969.1/154230.

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

Council of Science Editors:

West DE. Sensitivity of Swept-Wing, Boundary-Layer Transition to Spanwise-Periodic Discrete Roughness Elements. [Thesis]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/154230

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

[1] [2]

.