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:(active flow control). Showing records 1 – 30 of 98 total matches.

[1] [2] [3] [4]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

▼ Search Limiters


Texas A&M University

1. Gaurav. Application of active flow control technology in an unmanned aerial vehicle.

Degree: 2009, Texas A&M University

 A low speed wind tunnel experimental investigation was conducted to determine the effectiveness of the leading edge pulsed blowing and the trailing edge jet blowing/… (more)

Subjects/Keywords: Active Flow Control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gaurav. (2009). Application of active flow control technology in an unmanned aerial vehicle. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1558

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

Chicago Manual of Style (16th Edition):

Gaurav. “Application of active flow control technology in an unmanned aerial vehicle.” 2009. Thesis, Texas A&M University. Accessed July 13, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1558.

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

MLA Handbook (7th Edition):

Gaurav. “Application of active flow control technology in an unmanned aerial vehicle.” 2009. Web. 13 Jul 2020.

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

Vancouver:

Gaurav. Application of active flow control technology in an unmanned aerial vehicle. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1558.

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

Council of Science Editors:

Gaurav. Application of active flow control technology in an unmanned aerial vehicle. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1558

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


University of Manchester

2. Marks, Aryeh. Co-Flow Studies ar Subsonic Speeds.

Degree: 2011, University of Manchester

 This report investigates the effect of a coflow on the aerodynamic performance of a flat plate. The aim is to achieve an increase in the… (more)

Subjects/Keywords: active flow control; coflow

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Marks, A. (2011). Co-Flow Studies ar Subsonic Speeds. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:106402

Chicago Manual of Style (16th Edition):

Marks, Aryeh. “Co-Flow Studies ar Subsonic Speeds.” 2011. Doctoral Dissertation, University of Manchester. Accessed July 13, 2020. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:106402.

MLA Handbook (7th Edition):

Marks, Aryeh. “Co-Flow Studies ar Subsonic Speeds.” 2011. Web. 13 Jul 2020.

Vancouver:

Marks A. Co-Flow Studies ar Subsonic Speeds. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2020 Jul 13]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:106402.

Council of Science Editors:

Marks A. Co-Flow Studies ar Subsonic Speeds. [Doctoral Dissertation]. University of Manchester; 2011. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:106402


Delft University of Technology

3. van Pelt, Timo (author). Plasma Synthetic Jet Actuator: From characterisation to separation flow control.

Degree: 2019, Delft University of Technology

 This project proposes a series of experiments that involve plasma synthetic jet actuators. The first experiment will perform a jet characterisation experiment that will research… (more)

Subjects/Keywords: Plasma actuators; Active flow control; Aerodynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

van Pelt, T. (. (2019). Plasma Synthetic Jet Actuator: From characterisation to separation flow control. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5a5627ae-63c1-459c-9a8b-cbbeb1a9625a

Chicago Manual of Style (16th Edition):

van Pelt, Timo (author). “Plasma Synthetic Jet Actuator: From characterisation to separation flow control.” 2019. Masters Thesis, Delft University of Technology. Accessed July 13, 2020. http://resolver.tudelft.nl/uuid:5a5627ae-63c1-459c-9a8b-cbbeb1a9625a.

MLA Handbook (7th Edition):

van Pelt, Timo (author). “Plasma Synthetic Jet Actuator: From characterisation to separation flow control.” 2019. Web. 13 Jul 2020.

Vancouver:

van Pelt T(. Plasma Synthetic Jet Actuator: From characterisation to separation flow control. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Jul 13]. Available from: http://resolver.tudelft.nl/uuid:5a5627ae-63c1-459c-9a8b-cbbeb1a9625a.

Council of Science Editors:

van Pelt T(. Plasma Synthetic Jet Actuator: From characterisation to separation flow control. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:5a5627ae-63c1-459c-9a8b-cbbeb1a9625a


University of Arizona

4. Kalyankar, Harshad. Re-orienting the Flow over an Inclined Cylinder of Finite Aspect Ratio .

Degree: 2019, University of Arizona

Flow around an inclined and yawed circular cylinder of finite aspect ratio, that was either swept back or swept forward, was investigated experimentally. The cylinder… (more)

Subjects/Keywords: active flow control; cylinder; sweeping jet

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kalyankar, H. (2019). Re-orienting the Flow over an Inclined Cylinder of Finite Aspect Ratio . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/636506

Chicago Manual of Style (16th Edition):

Kalyankar, Harshad. “Re-orienting the Flow over an Inclined Cylinder of Finite Aspect Ratio .” 2019. Masters Thesis, University of Arizona. Accessed July 13, 2020. http://hdl.handle.net/10150/636506.

MLA Handbook (7th Edition):

Kalyankar, Harshad. “Re-orienting the Flow over an Inclined Cylinder of Finite Aspect Ratio .” 2019. Web. 13 Jul 2020.

Vancouver:

Kalyankar H. Re-orienting the Flow over an Inclined Cylinder of Finite Aspect Ratio . [Internet] [Masters thesis]. University of Arizona; 2019. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/10150/636506.

Council of Science Editors:

Kalyankar H. Re-orienting the Flow over an Inclined Cylinder of Finite Aspect Ratio . [Masters Thesis]. University of Arizona; 2019. Available from: http://hdl.handle.net/10150/636506


University of Arizona

5. Beck, Stephen. Full-Scale Tilt Rotor Download Reduction .

Degree: 2013, University of Arizona

 A large-scale model of a tiltrotor wing and flap was built and tested to determine how the size and spacing of fluidic actuators for active(more)

Subjects/Keywords: scaling; Aerospace Engineering; active flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Beck, S. (2013). Full-Scale Tilt Rotor Download Reduction . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/293744

Chicago Manual of Style (16th Edition):

Beck, Stephen. “Full-Scale Tilt Rotor Download Reduction .” 2013. Masters Thesis, University of Arizona. Accessed July 13, 2020. http://hdl.handle.net/10150/293744.

MLA Handbook (7th Edition):

Beck, Stephen. “Full-Scale Tilt Rotor Download Reduction .” 2013. Web. 13 Jul 2020.

Vancouver:

Beck S. Full-Scale Tilt Rotor Download Reduction . [Internet] [Masters thesis]. University of Arizona; 2013. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/10150/293744.

Council of Science Editors:

Beck S. Full-Scale Tilt Rotor Download Reduction . [Masters Thesis]. University of Arizona; 2013. Available from: http://hdl.handle.net/10150/293744


University of Cambridge

6. Illingworth, Simon J. Feedback control of oscillations in combustion and cavity flows.

Degree: PhD, 2010, University of Cambridge

 This thesis considers the control of combustion oscillations, motivated by the susceptibility of lean premixed combustion to such oscillations, and the long and expensive development… (more)

Subjects/Keywords: Combustion oscillations; Cavity oscillations; Active flow control; Feedback flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Illingworth, S. J. (2010). Feedback control of oscillations in combustion and cavity flows. (Doctoral Dissertation). University of Cambridge. Retrieved from http://www.dspace.cam.ac.uk/handle/1810/224778https://www.repository.cam.ac.uk/bitstream/1810/224778/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/5/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/6/thesis.pdf.jpg

Chicago Manual of Style (16th Edition):

Illingworth, Simon J. “Feedback control of oscillations in combustion and cavity flows.” 2010. Doctoral Dissertation, University of Cambridge. Accessed July 13, 2020. http://www.dspace.cam.ac.uk/handle/1810/224778https://www.repository.cam.ac.uk/bitstream/1810/224778/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/5/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/6/thesis.pdf.jpg.

MLA Handbook (7th Edition):

Illingworth, Simon J. “Feedback control of oscillations in combustion and cavity flows.” 2010. Web. 13 Jul 2020.

Vancouver:

Illingworth SJ. Feedback control of oscillations in combustion and cavity flows. [Internet] [Doctoral dissertation]. University of Cambridge; 2010. [cited 2020 Jul 13]. Available from: http://www.dspace.cam.ac.uk/handle/1810/224778https://www.repository.cam.ac.uk/bitstream/1810/224778/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/5/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/6/thesis.pdf.jpg.

Council of Science Editors:

Illingworth SJ. Feedback control of oscillations in combustion and cavity flows. [Doctoral Dissertation]. University of Cambridge; 2010. Available from: http://www.dspace.cam.ac.uk/handle/1810/224778https://www.repository.cam.ac.uk/bitstream/1810/224778/2/license.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/5/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/3/thesis.pdf.txt ; https://www.repository.cam.ac.uk/bitstream/1810/224778/6/thesis.pdf.jpg


University of Miami

7. Wang, Yang. Study of Power Minimization of Co-Flow Jet Active Flow Control with Fixed Airfoil Geometry.

Degree: MS, Mechanical Engineering (Engineering), 2019, University of Miami

  The objective of this thesis is to numerically study the power minimization for subsonic Co-Flow Jet (CFJ) active flow control airfoil using fixed geometry… (more)

Subjects/Keywords: Power Minimization; Co-Flow Jet; Flow Control; Fixed Airfoil Geometry; Active Flow Control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wang, Y. (2019). Study of Power Minimization of Co-Flow Jet Active Flow Control with Fixed Airfoil Geometry. (Thesis). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_theses/765

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):

Wang, Yang. “Study of Power Minimization of Co-Flow Jet Active Flow Control with Fixed Airfoil Geometry.” 2019. Thesis, University of Miami. Accessed July 13, 2020. https://scholarlyrepository.miami.edu/oa_theses/765.

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

MLA Handbook (7th Edition):

Wang, Yang. “Study of Power Minimization of Co-Flow Jet Active Flow Control with Fixed Airfoil Geometry.” 2019. Web. 13 Jul 2020.

Vancouver:

Wang Y. Study of Power Minimization of Co-Flow Jet Active Flow Control with Fixed Airfoil Geometry. [Internet] [Thesis]. University of Miami; 2019. [cited 2020 Jul 13]. Available from: https://scholarlyrepository.miami.edu/oa_theses/765.

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

Council of Science Editors:

Wang Y. Study of Power Minimization of Co-Flow Jet Active Flow Control with Fixed Airfoil Geometry. [Thesis]. University of Miami; 2019. Available from: https://scholarlyrepository.miami.edu/oa_theses/765

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


University of Illinois – Urbana-Champaign

8. 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 July 13, 2020. http://hdl.handle.net/2142/92747.

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

MLA Handbook (7th Edition):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Web. 13 Jul 2020.

Vancouver:

Gupta R. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2016. [cited 2020 Jul 13]. 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


Colorado School of Mines

9. Lambie, Patrick. Concept implementation of small scale active control volumetric flow rate meter.

Degree: MS(M.S.), Petroleum Engineering, 2017, Colorado School of Mines

 Despite many shortcomings, methods claiming to measure volumetric flow rate (VFR) have been widely applied to delta flow integrated on land drilling operations. Sensors, paddles,… (more)

Subjects/Keywords: Flow rate meter; Volumetric flow meter; Kick; Active control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lambie, P. (2017). Concept implementation of small scale active control volumetric flow rate meter. (Masters Thesis). Colorado School of Mines. Retrieved from http://hdl.handle.net/11124/171191

Chicago Manual of Style (16th Edition):

Lambie, Patrick. “Concept implementation of small scale active control volumetric flow rate meter.” 2017. Masters Thesis, Colorado School of Mines. Accessed July 13, 2020. http://hdl.handle.net/11124/171191.

MLA Handbook (7th Edition):

Lambie, Patrick. “Concept implementation of small scale active control volumetric flow rate meter.” 2017. Web. 13 Jul 2020.

Vancouver:

Lambie P. Concept implementation of small scale active control volumetric flow rate meter. [Internet] [Masters thesis]. Colorado School of Mines; 2017. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/11124/171191.

Council of Science Editors:

Lambie P. Concept implementation of small scale active control volumetric flow rate meter. [Masters Thesis]. Colorado School of Mines; 2017. Available from: http://hdl.handle.net/11124/171191


University of Cincinnati

10. POONDRU, SHIRDISH. Large-Eddy Simulation and Active Flow Control of Low-Reynolds Number Flow through a Low-Pressure Turbine Cascade.

Degree: PhD, Engineering : Mechanical Engineering, 2008, University of Cincinnati

  The operating Reynolds numbers (Re) for a low-pressure turbine (LPT) in an aircraft engine can drop below 25,000 during high-altitude cruise conditions, resulting in… (more)

Subjects/Keywords: Engineering, Mechanical; Large-eddy simulation; Low-pressure turbines; Active flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

POONDRU, S. (2008). Large-Eddy Simulation and Active Flow Control of Low-Reynolds Number Flow through a Low-Pressure Turbine Cascade. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1204873699

Chicago Manual of Style (16th Edition):

POONDRU, SHIRDISH. “Large-Eddy Simulation and Active Flow Control of Low-Reynolds Number Flow through a Low-Pressure Turbine Cascade.” 2008. Doctoral Dissertation, University of Cincinnati. Accessed July 13, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1204873699.

MLA Handbook (7th Edition):

POONDRU, SHIRDISH. “Large-Eddy Simulation and Active Flow Control of Low-Reynolds Number Flow through a Low-Pressure Turbine Cascade.” 2008. Web. 13 Jul 2020.

Vancouver:

POONDRU S. Large-Eddy Simulation and Active Flow Control of Low-Reynolds Number Flow through a Low-Pressure Turbine Cascade. [Internet] [Doctoral dissertation]. University of Cincinnati; 2008. [cited 2020 Jul 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1204873699.

Council of Science Editors:

POONDRU S. Large-Eddy Simulation and Active Flow Control of Low-Reynolds Number Flow through a Low-Pressure Turbine Cascade. [Doctoral Dissertation]. University of Cincinnati; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1204873699

11. Yagiz, Bedri. Active Control of Shocks and Sonic Boom Ground Signal.

Degree: PhD, Aerospace Engineering, 2010, Old Dominion University

  The manipulation of a flow field to obtain a desired change is a much heightened subject. Active flow control has been the subject of… (more)

Subjects/Keywords: Active control; Shock waves; Sonic booms; Transonic flow; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Yagiz, B. (2010). Active Control of Shocks and Sonic Boom Ground Signal. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92

Chicago Manual of Style (16th Edition):

Yagiz, Bedri. “Active Control of Shocks and Sonic Boom Ground Signal.” 2010. Doctoral Dissertation, Old Dominion University. Accessed July 13, 2020. 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92.

MLA Handbook (7th Edition):

Yagiz, Bedri. “Active Control of Shocks and Sonic Boom Ground Signal.” 2010. Web. 13 Jul 2020.

Vancouver:

Yagiz B. Active Control of Shocks and Sonic Boom Ground Signal. [Internet] [Doctoral dissertation]. Old Dominion University; 2010. [cited 2020 Jul 13]. Available from: 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92.

Council of Science Editors:

Yagiz B. Active Control of Shocks and Sonic Boom Ground Signal. [Doctoral Dissertation]. Old Dominion University; 2010. Available from: 9781124504278 ; https://digitalcommons.odu.edu/mae_etds/92


University of New South Wales

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

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

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Wu, Chaofan. “Jet oscillation applied for aircraft cabin ventilation using active flow control actuators.” 2014. Doctoral Dissertation, University of New South Wales. Accessed July 13, 2020. http://handle.unsw.edu.au/1959.4/53544 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12239/SOURCE02?view=true.

MLA Handbook (7th Edition):

Wu, Chaofan. “Jet oscillation applied for aircraft cabin ventilation using active flow control actuators.” 2014. Web. 13 Jul 2020.

Vancouver:

Wu C. Jet oscillation applied for aircraft cabin ventilation using active flow control actuators. [Internet] [Doctoral dissertation]. University of New South Wales; 2014. [cited 2020 Jul 13]. Available from: http://handle.unsw.edu.au/1959.4/53544 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:12239/SOURCE02?view=true.

Council of Science Editors:

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


Brunel University

13. Jeyalingam, Jonne. Towards the noise reduction of synthetic jet actuators using lobed orifices.

Degree: PhD, 2018, Brunel University

 With increasing strain on the civil aviation industry to meet strict targets to reduce the adverse effects aviation has on the environment by 2050, significant… (more)

Subjects/Keywords: Fluid mechanics; Active flow control; Aeroacoustics; Axis-switching

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jeyalingam, J. (2018). Towards the noise reduction of synthetic jet actuators using lobed orifices. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048

Chicago Manual of Style (16th Edition):

Jeyalingam, Jonne. “Towards the noise reduction of synthetic jet actuators using lobed orifices.” 2018. Doctoral Dissertation, Brunel University. Accessed July 13, 2020. http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048.

MLA Handbook (7th Edition):

Jeyalingam, Jonne. “Towards the noise reduction of synthetic jet actuators using lobed orifices.” 2018. Web. 13 Jul 2020.

Vancouver:

Jeyalingam J. Towards the noise reduction of synthetic jet actuators using lobed orifices. [Internet] [Doctoral dissertation]. Brunel University; 2018. [cited 2020 Jul 13]. Available from: http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048.

Council of Science Editors:

Jeyalingam J. Towards the noise reduction of synthetic jet actuators using lobed orifices. [Doctoral Dissertation]. Brunel University; 2018. Available from: http://bura.brunel.ac.uk/handle/2438/17118 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.765048

14. Ring, Emma. Modelling a piezoelectric-driven actuator for active flow control.

Degree: The Institute of Technology, 2014, Linköping UniversityLinköping University

Flow control is an area of research of particular interest within automotive and aerospace industries since methods used to affect the fluid flow around… (more)

Subjects/Keywords: Piezoelectric actuator; Lumped Element Modelling; Equivalent circuits; Active Flow Control; Simulink

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ring, E. (2014). Modelling a piezoelectric-driven actuator for active flow control. (Thesis). Linköping UniversityLinköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-114957

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):

Ring, Emma. “Modelling a piezoelectric-driven actuator for active flow control.” 2014. Thesis, Linköping UniversityLinköping University. Accessed July 13, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-114957.

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

MLA Handbook (7th Edition):

Ring, Emma. “Modelling a piezoelectric-driven actuator for active flow control.” 2014. Web. 13 Jul 2020.

Vancouver:

Ring E. Modelling a piezoelectric-driven actuator for active flow control. [Internet] [Thesis]. Linköping UniversityLinköping University; 2014. [cited 2020 Jul 13]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-114957.

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

Council of Science Editors:

Ring E. Modelling a piezoelectric-driven actuator for active flow control. [Thesis]. Linköping UniversityLinköping University; 2014. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-114957

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


University of Arizona

15. Wu, Luhong. Receptivity to Energy Deposition in Compressible Mixing Layers .

Degree: 2020, University of Arizona

 Better understanding of the behavior of compressible turbulent mixing layer is desirable for its active flow control by actuators which can be applied in many… (more)

Subjects/Keywords: Active Flow Control; Compressible Mixing Layer; Instability; Receptivity; Turbulence

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wu, L. (2020). Receptivity to Energy Deposition in Compressible Mixing Layers . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/641369

Chicago Manual of Style (16th Edition):

Wu, Luhong. “Receptivity to Energy Deposition in Compressible Mixing Layers .” 2020. Masters Thesis, University of Arizona. Accessed July 13, 2020. http://hdl.handle.net/10150/641369.

MLA Handbook (7th Edition):

Wu, Luhong. “Receptivity to Energy Deposition in Compressible Mixing Layers .” 2020. Web. 13 Jul 2020.

Vancouver:

Wu L. Receptivity to Energy Deposition in Compressible Mixing Layers . [Internet] [Masters thesis]. University of Arizona; 2020. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/10150/641369.

Council of Science Editors:

Wu L. Receptivity to Energy Deposition in Compressible Mixing Layers . [Masters Thesis]. University of Arizona; 2020. Available from: http://hdl.handle.net/10150/641369


Delft University of Technology

16. Bal, S.R. (author). Investigating the Influence of DBD Plasma Actuators on Skin Friction: Application to Integral Boundary Layer Formulation.

Degree: 2015, Delft University of Technology

The main driver of developments in the wind energy sector is not the absolute maximization of energy capture, but the reduction of the Cost of… (more)

Subjects/Keywords: Windenergy; skin friction; active flow control; DBD plasma actuation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bal, S. R. (. (2015). Investigating the Influence of DBD Plasma Actuators on Skin Friction: Application to Integral Boundary Layer Formulation. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8c723c77-3f7c-4ca1-899b-169207c0666a

Chicago Manual of Style (16th Edition):

Bal, S R (author). “Investigating the Influence of DBD Plasma Actuators on Skin Friction: Application to Integral Boundary Layer Formulation.” 2015. Masters Thesis, Delft University of Technology. Accessed July 13, 2020. http://resolver.tudelft.nl/uuid:8c723c77-3f7c-4ca1-899b-169207c0666a.

MLA Handbook (7th Edition):

Bal, S R (author). “Investigating the Influence of DBD Plasma Actuators on Skin Friction: Application to Integral Boundary Layer Formulation.” 2015. Web. 13 Jul 2020.

Vancouver:

Bal SR(. Investigating the Influence of DBD Plasma Actuators on Skin Friction: Application to Integral Boundary Layer Formulation. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Jul 13]. Available from: http://resolver.tudelft.nl/uuid:8c723c77-3f7c-4ca1-899b-169207c0666a.

Council of Science Editors:

Bal SR(. Investigating the Influence of DBD Plasma Actuators on Skin Friction: Application to Integral Boundary Layer Formulation. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:8c723c77-3f7c-4ca1-899b-169207c0666a


University of Arizona

17. Jentzsch, Marvin Patrick. On the Use of Active Flow Control to Trim and Control a Tailles Aircraft Model .

Degree: 2017, University of Arizona

 The Stability And Control CONfiguration (SACCON) model represents an emerging trend in airplane design where the classical tube, wing and empennage are replaced by a… (more)

Subjects/Keywords: Active Flow Control; Oscillating Jet; SACCON; Sweeping Jet; Tailles Aircraft; Trim

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jentzsch, M. P. (2017). On the Use of Active Flow Control to Trim and Control a Tailles Aircraft Model . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/625917

Chicago Manual of Style (16th Edition):

Jentzsch, Marvin Patrick. “On the Use of Active Flow Control to Trim and Control a Tailles Aircraft Model .” 2017. Masters Thesis, University of Arizona. Accessed July 13, 2020. http://hdl.handle.net/10150/625917.

MLA Handbook (7th Edition):

Jentzsch, Marvin Patrick. “On the Use of Active Flow Control to Trim and Control a Tailles Aircraft Model .” 2017. Web. 13 Jul 2020.

Vancouver:

Jentzsch MP. On the Use of Active Flow Control to Trim and Control a Tailles Aircraft Model . [Internet] [Masters thesis]. University of Arizona; 2017. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/10150/625917.

Council of Science Editors:

Jentzsch MP. On the Use of Active Flow Control to Trim and Control a Tailles Aircraft Model . [Masters Thesis]. University of Arizona; 2017. Available from: http://hdl.handle.net/10150/625917


Missouri University of Science and Technology

18. Aholt, Justin Roger. Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles.

Degree: M.S. in Aerospace Engineering, Aerospace Engineering, Missouri University of Science and Technology

 "A parametric computational study designed to examine the plausibility of an external body force generated by active means, such as a plasma actuator, as a… (more)

Subjects/Keywords: Active flow control; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Aholt, J. R. (n.d.). Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles. (Masters Thesis). Missouri University of Science and Technology. Retrieved from https://scholarsmine.mst.edu/masters_theses/4977

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Chicago Manual of Style (16th Edition):

Aholt, Justin Roger. “Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles.” Masters Thesis, Missouri University of Science and Technology. Accessed July 13, 2020. https://scholarsmine.mst.edu/masters_theses/4977.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

MLA Handbook (7th Edition):

Aholt, Justin Roger. “Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles.” Web. 13 Jul 2020.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Aholt JR. Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles. [Internet] [Masters thesis]. Missouri University of Science and Technology; [cited 2020 Jul 13]. Available from: https://scholarsmine.mst.edu/masters_theses/4977.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Council of Science Editors:

Aholt JR. Computational investigation of plasma actuator as an active flow control strategy of laminar separation bubbles. [Masters Thesis]. Missouri University of Science and Technology; Available from: https://scholarsmine.mst.edu/masters_theses/4977

Note: this citation may be lacking information needed for this citation format:
No year of publication.


University of Cincinnati

19. Gan, Subhadeep. Active Separation Control of High-Re Turbulent Separated Flow over a Wall-Mounted Hump using RANS, DES, and LES Turbulence Modeling Approaches.

Degree: PhD, Engineering : Mechanical Engineering, 2010, University of Cincinnati

 Most practical flows in engineering applications are turbulent, and exhibit separation which is generally undesirable because of its adverse effects on performance and efficiency. Therefore,… (more)

Subjects/Keywords: Mechanical Engineering; CFD; Separated flow; Active flow control; Steady Suction; Synthetic Jet

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gan, S. (2010). Active Separation Control of High-Re Turbulent Separated Flow over a Wall-Mounted Hump using RANS, DES, and LES Turbulence Modeling Approaches. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1275924069

Chicago Manual of Style (16th Edition):

Gan, Subhadeep. “Active Separation Control of High-Re Turbulent Separated Flow over a Wall-Mounted Hump using RANS, DES, and LES Turbulence Modeling Approaches.” 2010. Doctoral Dissertation, University of Cincinnati. Accessed July 13, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1275924069.

MLA Handbook (7th Edition):

Gan, Subhadeep. “Active Separation Control of High-Re Turbulent Separated Flow over a Wall-Mounted Hump using RANS, DES, and LES Turbulence Modeling Approaches.” 2010. Web. 13 Jul 2020.

Vancouver:

Gan S. Active Separation Control of High-Re Turbulent Separated Flow over a Wall-Mounted Hump using RANS, DES, and LES Turbulence Modeling Approaches. [Internet] [Doctoral dissertation]. University of Cincinnati; 2010. [cited 2020 Jul 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1275924069.

Council of Science Editors:

Gan S. Active Separation Control of High-Re Turbulent Separated Flow over a Wall-Mounted Hump using RANS, DES, and LES Turbulence Modeling Approaches. [Doctoral Dissertation]. University of Cincinnati; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1275924069


University of Arizona

20. Woszidlo, Rene. PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS .

Degree: 2011, University of Arizona

 Parameters governing separation control with sweeping jet actuators over a deflected flap are investigated experimentally on a generic "Multiple Flap Airfoil" (MFA). The model enables… (more)

Subjects/Keywords: fluidic oscillators; separation control; streamwise vortices; sweeping jets; Aerospace Engineering; active flow control; aerodynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Woszidlo, R. (2011). PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/203475

Chicago Manual of Style (16th Edition):

Woszidlo, Rene. “PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS .” 2011. Doctoral Dissertation, University of Arizona. Accessed July 13, 2020. http://hdl.handle.net/10150/203475.

MLA Handbook (7th Edition):

Woszidlo, Rene. “PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS .” 2011. Web. 13 Jul 2020.

Vancouver:

Woszidlo R. PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS . [Internet] [Doctoral dissertation]. University of Arizona; 2011. [cited 2020 Jul 13]. Available from: http://hdl.handle.net/10150/203475.

Council of Science Editors:

Woszidlo R. PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS . [Doctoral Dissertation]. University of Arizona; 2011. Available from: http://hdl.handle.net/10150/203475


University of Notre Dame

21. Ahmed Eltaweel. Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>.

Degree: Aerospace and Mechanical Engineering, 2013, University of Notre Dame

  Prediction and reduction of airframe noise are critically important to the development of quieter civil transport aircraft. The key to noise reduction is a… (more)

Subjects/Keywords: Hybrid Acoustic Approach; Plasma Flow Control; Landing Gear Noise; Active Flow and Noise Control; Tandem Cylinders; Rod-Airfoil Wake Interaction

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Eltaweel, A. (2013). Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/tq57np21m1v

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):

Eltaweel, Ahmed. “Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>.” 2013. Thesis, University of Notre Dame. Accessed July 13, 2020. https://curate.nd.edu/show/tq57np21m1v.

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

MLA Handbook (7th Edition):

Eltaweel, Ahmed. “Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>.” 2013. Web. 13 Jul 2020.

Vancouver:

Eltaweel A. Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>. [Internet] [Thesis]. University of Notre Dame; 2013. [cited 2020 Jul 13]. Available from: https://curate.nd.edu/show/tq57np21m1v.

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

Council of Science Editors:

Eltaweel A. Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>. [Thesis]. University of Notre Dame; 2013. Available from: https://curate.nd.edu/show/tq57np21m1v

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

22. Baiense, Jr., Joao C. Vortex Generator Jet Flow Control in Highly Loaded Compressors.

Degree: MS, 2014, Worcester Polytechnic Institute

 "A flow control method for minimizing losses in a highly loaded compressor blade was analyzed. Passive and active flow control experiments with vortex generator jets… (more)

Subjects/Keywords: highly loaded blades; linear compressor cascade; gas turbines; vortex generator jet; active flow control; passive flow control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Baiense, Jr., J. C. (2014). Vortex Generator Jet Flow Control in Highly Loaded Compressors. (Thesis). Worcester Polytechnic Institute. Retrieved from etd-072814-063700 ; https://digitalcommons.wpi.edu/etd-theses/916

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):

Baiense, Jr., Joao C. “Vortex Generator Jet Flow Control in Highly Loaded Compressors.” 2014. Thesis, Worcester Polytechnic Institute. Accessed July 13, 2020. etd-072814-063700 ; https://digitalcommons.wpi.edu/etd-theses/916.

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

MLA Handbook (7th Edition):

Baiense, Jr., Joao C. “Vortex Generator Jet Flow Control in Highly Loaded Compressors.” 2014. Web. 13 Jul 2020.

Vancouver:

Baiense, Jr. JC. Vortex Generator Jet Flow Control in Highly Loaded Compressors. [Internet] [Thesis]. Worcester Polytechnic Institute; 2014. [cited 2020 Jul 13]. Available from: etd-072814-063700 ; https://digitalcommons.wpi.edu/etd-theses/916.

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

Council of Science Editors:

Baiense, Jr. JC. Vortex Generator Jet Flow Control in Highly Loaded Compressors. [Thesis]. Worcester Polytechnic Institute; 2014. Available from: etd-072814-063700 ; https://digitalcommons.wpi.edu/etd-theses/916

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


University of Toledo

23. Lopera, Javier. Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation.

Degree: PhD, Mechanical Engineering, 2007, University of Toledo

 This dissertation presents experimental investigations of several novel active flow control methodologies that have been implemented for aerodynamic control and maneuvering of slender bodies at… (more)

Subjects/Keywords: active flow control; aerodynamic control; slender bodies; blunt bodies; high angle of attack; forebody vortex control; coning motion; strakes; flowfield

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lopera, J. (2007). Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation. (Doctoral Dissertation). University of Toledo. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=toledo1177504352

Chicago Manual of Style (16th Edition):

Lopera, Javier. “Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation.” 2007. Doctoral Dissertation, University of Toledo. Accessed July 13, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1177504352.

MLA Handbook (7th Edition):

Lopera, Javier. “Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation.” 2007. Web. 13 Jul 2020.

Vancouver:

Lopera J. Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation. [Internet] [Doctoral dissertation]. University of Toledo; 2007. [cited 2020 Jul 13]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=toledo1177504352.

Council of Science Editors:

Lopera J. Aerodynamic Control of Slender Bodies from Low to High Angles of Attack through Flow Manipulation. [Doctoral Dissertation]. University of Toledo; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=toledo1177504352


Penn State University

24. Sikarwar, Nidhi. The Development of Three-dimensional Adjoint Method for Flow Control with Blowing in Convergent-Divergent Nozzle Flows.

Degree: PhD, Aerospace Engineering, 2014, Penn State University

 The noise produced by the low bypass ratio turbofan engines used to power fighter aircraft is a problem for communities near military bases and for… (more)

Subjects/Keywords: Adjoint method; noise reduction; active flow control; adjoint boundary conditions; optimization; computational fluid dynamics.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sikarwar, N. (2014). The Development of Three-dimensional Adjoint Method for Flow Control with Blowing in Convergent-Divergent Nozzle Flows. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/24885

Chicago Manual of Style (16th Edition):

Sikarwar, Nidhi. “The Development of Three-dimensional Adjoint Method for Flow Control with Blowing in Convergent-Divergent Nozzle Flows.” 2014. Doctoral Dissertation, Penn State University. Accessed July 13, 2020. https://etda.libraries.psu.edu/catalog/24885.

MLA Handbook (7th Edition):

Sikarwar, Nidhi. “The Development of Three-dimensional Adjoint Method for Flow Control with Blowing in Convergent-Divergent Nozzle Flows.” 2014. Web. 13 Jul 2020.

Vancouver:

Sikarwar N. The Development of Three-dimensional Adjoint Method for Flow Control with Blowing in Convergent-Divergent Nozzle Flows. [Internet] [Doctoral dissertation]. Penn State University; 2014. [cited 2020 Jul 13]. Available from: https://etda.libraries.psu.edu/catalog/24885.

Council of Science Editors:

Sikarwar N. The Development of Three-dimensional Adjoint Method for Flow Control with Blowing in Convergent-Divergent Nozzle Flows. [Doctoral Dissertation]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/24885


University of Alberta

25. Babazadeh, Hamed. Active flow control of a precessing jet.

Degree: MS, Department of Mechanical Engineering, 2010, University of Alberta

Active flow control of a precessing jet is the focus of this work. A round jet confined by a round cavity exhibits a self-excited rotational… (more)

Subjects/Keywords: Jet actuation; Active flow control; Real time monitoring; Stereoscopic PIV; Phase plane; Precessing jet

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Babazadeh, H. (2010). Active flow control of a precessing jet. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/br86b3944

Chicago Manual of Style (16th Edition):

Babazadeh, Hamed. “Active flow control of a precessing jet.” 2010. Masters Thesis, University of Alberta. Accessed July 13, 2020. https://era.library.ualberta.ca/files/br86b3944.

MLA Handbook (7th Edition):

Babazadeh, Hamed. “Active flow control of a precessing jet.” 2010. Web. 13 Jul 2020.

Vancouver:

Babazadeh H. Active flow control of a precessing jet. [Internet] [Masters thesis]. University of Alberta; 2010. [cited 2020 Jul 13]. Available from: https://era.library.ualberta.ca/files/br86b3944.

Council of Science Editors:

Babazadeh H. Active flow control of a precessing jet. [Masters Thesis]. University of Alberta; 2010. Available from: https://era.library.ualberta.ca/files/br86b3944


Rochester Institute of Technology

26. Gomez, Arnold David. Control of a magnetically levitated ventricular assist device.

Degree: Mechanical Engineering, 2009, Rochester Institute of Technology

 This work presents theoretical and experimental means for achieving impeller stability in a magnetically levitated left ventricular assist device (LVAD). These types of medical devices… (more)

Subjects/Keywords: Active magnetic bearing; Axial flow; Blood pump; Control system; Hall effect position sensing; Magnetic levitation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gomez, A. D. (2009). Control of a magnetically levitated ventricular assist device. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/5821

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):

Gomez, Arnold David. “Control of a magnetically levitated ventricular assist device.” 2009. Thesis, Rochester Institute of Technology. Accessed July 13, 2020. https://scholarworks.rit.edu/theses/5821.

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

MLA Handbook (7th Edition):

Gomez, Arnold David. “Control of a magnetically levitated ventricular assist device.” 2009. Web. 13 Jul 2020.

Vancouver:

Gomez AD. Control of a magnetically levitated ventricular assist device. [Internet] [Thesis]. Rochester Institute of Technology; 2009. [cited 2020 Jul 13]. Available from: https://scholarworks.rit.edu/theses/5821.

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

Council of Science Editors:

Gomez AD. Control of a magnetically levitated ventricular assist device. [Thesis]. Rochester Institute of Technology; 2009. Available from: https://scholarworks.rit.edu/theses/5821

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

27. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 July 13, 2020. 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. 13 Jul 2020.

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 2020 Jul 13]. 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

28. Barry, Gillian. The effects of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in a healthy young subject population.

Degree: PhD, 2014, Teesside University

 This thesis investigated the effect of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in… (more)

Subjects/Keywords: 613.7; Exergaming; Active Video Gaming; Technology Acceptance; Flow state; Postural control; Balance

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Barry, G. (2014). The effects of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in a healthy young subject population. (Doctoral Dissertation). Teesside University. Retrieved from https://research.tees.ac.uk/en/studentTheses/30f40710-31f2-4104-b207-8cc8483215bb ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.632798

Chicago Manual of Style (16th Edition):

Barry, Gillian. “The effects of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in a healthy young subject population.” 2014. Doctoral Dissertation, Teesside University. Accessed July 13, 2020. https://research.tees.ac.uk/en/studentTheses/30f40710-31f2-4104-b207-8cc8483215bb ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.632798.

MLA Handbook (7th Edition):

Barry, Gillian. “The effects of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in a healthy young subject population.” 2014. Web. 13 Jul 2020.

Vancouver:

Barry G. The effects of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in a healthy young subject population. [Internet] [Doctoral dissertation]. Teesside University; 2014. [cited 2020 Jul 13]. Available from: https://research.tees.ac.uk/en/studentTheses/30f40710-31f2-4104-b207-8cc8483215bb ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.632798.

Council of Science Editors:

Barry G. The effects of exergaming versus mirror matched gym based exercise with no virtual stimuli on technology acceptance, flow and postural control in a healthy young subject population. [Doctoral Dissertation]. Teesside University; 2014. Available from: https://research.tees.ac.uk/en/studentTheses/30f40710-31f2-4104-b207-8cc8483215bb ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.632798


Syracuse University

29. Berger, Zachary P. The Effects of Active Flow Control on High-Speed Jet Flow Physics and Noise.

Degree: PhD, Mechanical and Aerospace Engineering, 2014, Syracuse University

  The work to be presented focuses on the noise generation of a fully turbulent, compressible jet flow within a large scale anechoic chamber. The… (more)

Subjects/Keywords: Active Flow Control; Aeroacoustics; Jet Noise; Particle Image Velocimetry; Reduced-Order Modeling; Turbulence; Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Berger, Z. P. (2014). The Effects of Active Flow Control on High-Speed Jet Flow Physics and Noise. (Doctoral Dissertation). Syracuse University. Retrieved from https://surface.syr.edu/etd/107

Chicago Manual of Style (16th Edition):

Berger, Zachary P. “The Effects of Active Flow Control on High-Speed Jet Flow Physics and Noise.” 2014. Doctoral Dissertation, Syracuse University. Accessed July 13, 2020. https://surface.syr.edu/etd/107.

MLA Handbook (7th Edition):

Berger, Zachary P. “The Effects of Active Flow Control on High-Speed Jet Flow Physics and Noise.” 2014. Web. 13 Jul 2020.

Vancouver:

Berger ZP. The Effects of Active Flow Control on High-Speed Jet Flow Physics and Noise. [Internet] [Doctoral dissertation]. Syracuse University; 2014. [cited 2020 Jul 13]. Available from: https://surface.syr.edu/etd/107.

Council of Science Editors:

Berger ZP. The Effects of Active Flow Control on High-Speed Jet Flow Physics and Noise. [Doctoral Dissertation]. Syracuse University; 2014. Available from: https://surface.syr.edu/etd/107


Delft University of Technology

30. Crespo Pradell, Oriol (author). Study of the bifurcation behavior of the flow around a 2D Ahmed body applied to active flow control systems.

Degree: 2018, Delft University of Technology

 This master thesis focuses in the study of the application of active flow control in the transitional regime (Re ≈ 3E3) at the rear part… (more)

Subjects/Keywords: Aerodynamics; Stability Analysis; Low Reynolds number; Ahmed body; Active flow control; Bifurcation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Crespo Pradell, O. (. (2018). Study of the bifurcation behavior of the flow around a 2D Ahmed body applied to active flow control systems. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:853cb59d-9c14-45ae-ba19-5edf57f65575

Chicago Manual of Style (16th Edition):

Crespo Pradell, Oriol (author). “Study of the bifurcation behavior of the flow around a 2D Ahmed body applied to active flow control systems.” 2018. Masters Thesis, Delft University of Technology. Accessed July 13, 2020. http://resolver.tudelft.nl/uuid:853cb59d-9c14-45ae-ba19-5edf57f65575.

MLA Handbook (7th Edition):

Crespo Pradell, Oriol (author). “Study of the bifurcation behavior of the flow around a 2D Ahmed body applied to active flow control systems.” 2018. Web. 13 Jul 2020.

Vancouver:

Crespo Pradell O(. Study of the bifurcation behavior of the flow around a 2D Ahmed body applied to active flow control systems. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2020 Jul 13]. Available from: http://resolver.tudelft.nl/uuid:853cb59d-9c14-45ae-ba19-5edf57f65575.

Council of Science Editors:

Crespo Pradell O(. Study of the bifurcation behavior of the flow around a 2D Ahmed body applied to active flow control systems. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:853cb59d-9c14-45ae-ba19-5edf57f65575

[1] [2] [3] [4]

.