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You searched for subject:(active separation control). Showing records 1 – 15 of 15 total matches.

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Georgia Tech

1. Koukpaizan, Nicholson Konrad Konrad. Improved techniques for aerodynamic flow control simulation with fluidic oscillators.

Degree: PhD, Aerospace Engineering, 2020, Georgia Tech

 High-fidelity simulations were performed to characterize the physics of jet interaction fluidic oscillators and provide a basis for the development of improved boundary conditions that… (more)

Subjects/Keywords: Fluidic oscillator; Active flow control; High-fidelity simulation; CFD; Flow separation

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APA (6th Edition):

Koukpaizan, N. K. K. (2020). Improved techniques for aerodynamic flow control simulation with fluidic oscillators. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/63604

Chicago Manual of Style (16th Edition):

Koukpaizan, Nicholson Konrad Konrad. “Improved techniques for aerodynamic flow control simulation with fluidic oscillators.” 2020. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/63604.

MLA Handbook (7th Edition):

Koukpaizan, Nicholson Konrad Konrad. “Improved techniques for aerodynamic flow control simulation with fluidic oscillators.” 2020. Web. 18 Jan 2021.

Vancouver:

Koukpaizan NKK. Improved techniques for aerodynamic flow control simulation with fluidic oscillators. [Internet] [Doctoral dissertation]. Georgia Tech; 2020. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/63604.

Council of Science Editors:

Koukpaizan NKK. Improved techniques for aerodynamic flow control simulation with fluidic oscillators. [Doctoral Dissertation]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/63604


University of Arizona

2. 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

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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 January 18, 2021. http://hdl.handle.net/10150/203475.

MLA Handbook (7th Edition):

Woszidlo, Rene. “PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS .” 2011. Web. 18 Jan 2021.

Vancouver:

Woszidlo R. PARAMETERS GOVERNING SEPARATION CONTROL WITH SWEEPING JET ACTUATORS . [Internet] [Doctoral dissertation]. University of Arizona; 2011. [cited 2021 Jan 18]. 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 Southern California

3. Yang, Shanling. Boundary layer and separation control on wings at low Reynolds numbers.

Degree: PhD, Aerospace Engineering, 2013, University of Southern California

 In the transitional chord-based Reynolds number regime for aeronautics, 10⁴ ≤ Re ≤ 10⁵, fluid flow over a surface is prone to separation followed by… (more)

Subjects/Keywords: low Reynolds numbers; separation control; acoustic excitation; active separation control; passive separation control; boundary layers; fluid dynamics; aerodynamics; Helmholtz resonance; local acoustic forcing; external acoustic excitation; internal excitation; flow control

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APA (6th Edition):

Yang, S. (2013). Boundary layer and separation control on wings at low Reynolds numbers. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/337675/rec/1157

Chicago Manual of Style (16th Edition):

Yang, Shanling. “Boundary layer and separation control on wings at low Reynolds numbers.” 2013. Doctoral Dissertation, University of Southern California. Accessed January 18, 2021. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/337675/rec/1157.

MLA Handbook (7th Edition):

Yang, Shanling. “Boundary layer and separation control on wings at low Reynolds numbers.” 2013. Web. 18 Jan 2021.

Vancouver:

Yang S. Boundary layer and separation control on wings at low Reynolds numbers. [Internet] [Doctoral dissertation]. University of Southern California; 2013. [cited 2021 Jan 18]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/337675/rec/1157.

Council of Science Editors:

Yang S. Boundary layer and separation control on wings at low Reynolds numbers. [Doctoral Dissertation]. University of Southern California; 2013. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/337675/rec/1157

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

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

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

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

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APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

Kapsalis, Panagiotis - Chrysovalantis. “Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής.” 2016. Thesis, University of Thessaly (UTH); Πανεπιστήμιο Θεσσαλίας. Accessed January 18, 2021. http://hdl.handle.net/10442/hedi/37397.

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

MLA Handbook (7th Edition):

Kapsalis, Panagiotis - Chrysovalantis. “Έλεγχος της μετάβασης και αποκόλλησης οριακού στρώματος και της απόδοσης αεροτομής με ενεργητική καθοδήγηση της ροής.” 2016. Web. 18 Jan 2021.

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 2021 Jan 18]. Available from: http://hdl.handle.net/10442/hedi/37397.

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

Council of Science Editors:

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

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


University of Alberta

5. Baugh, Aaron R. Active open-loop control of a backward-facing step flow.

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

 A robotically-controlled actuation system has been developed and built to perform active open-loop flow control experiments on transitional and turbulent backward-facing step flows in water.… (more)

Subjects/Keywords: vorticity; tuft; actuation; separation; turbulent; backward-facing step; open-loop; visualization; spanwise-varying; reattachment; shear layer; active control

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APA (6th Edition):

Baugh, A. R. (2010). Active open-loop control of a backward-facing step flow. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/3n204002v

Chicago Manual of Style (16th Edition):

Baugh, Aaron R. “Active open-loop control of a backward-facing step flow.” 2010. Masters Thesis, University of Alberta. Accessed January 18, 2021. https://era.library.ualberta.ca/files/3n204002v.

MLA Handbook (7th Edition):

Baugh, Aaron R. “Active open-loop control of a backward-facing step flow.” 2010. Web. 18 Jan 2021.

Vancouver:

Baugh AR. Active open-loop control of a backward-facing step flow. [Internet] [Masters thesis]. University of Alberta; 2010. [cited 2021 Jan 18]. Available from: https://era.library.ualberta.ca/files/3n204002v.

Council of Science Editors:

Baugh AR. Active open-loop control of a backward-facing step flow. [Masters Thesis]. University of Alberta; 2010. Available from: https://era.library.ualberta.ca/files/3n204002v


Texas A&M University

6. Balasubramanian, Ashwin Kumar. Modeling of D/C motor driven synthetic jet acutators for flow separation control.

Degree: MS, Aerospace Engineering, 2004, Texas A&M University

 The objective of this research is to present a theoretical study of the compressibility effects on the performance of an electric D/C motor driven synthetic… (more)

Subjects/Keywords: Synthetic Jet Actuators; D/C Motor; Flow separation; Active flow control

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APA (6th Edition):

Balasubramanian, A. K. (2004). Modeling of D/C motor driven synthetic jet acutators for flow separation control. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/1146

Chicago Manual of Style (16th Edition):

Balasubramanian, Ashwin Kumar. “Modeling of D/C motor driven synthetic jet acutators for flow separation control.” 2004. Masters Thesis, Texas A&M University. Accessed January 18, 2021. http://hdl.handle.net/1969.1/1146.

MLA Handbook (7th Edition):

Balasubramanian, Ashwin Kumar. “Modeling of D/C motor driven synthetic jet acutators for flow separation control.” 2004. Web. 18 Jan 2021.

Vancouver:

Balasubramanian AK. Modeling of D/C motor driven synthetic jet acutators for flow separation control. [Internet] [Masters thesis]. Texas A&M University; 2004. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1969.1/1146.

Council of Science Editors:

Balasubramanian AK. Modeling of D/C motor driven synthetic jet acutators for flow separation control. [Masters Thesis]. Texas A&M University; 2004. Available from: http://hdl.handle.net/1969.1/1146


Virginia Tech

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

Degree: MS, Mechanical Engineering, 2009, Virginia Tech

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Thompson, Andrew C. “Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade.” 2009. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/33078.

MLA Handbook (7th Edition):

Thompson, Andrew C. “Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade.” 2009. Web. 18 Jan 2021.

Vancouver:

Thompson AC. Investigation and Simulation of Ion Flow Control over a Flat Plate and Compressor Cascade. [Internet] [Masters thesis]. Virginia Tech; 2009. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/33078.

Council of Science Editors:

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


Brigham Young University

8. Reimann, Daniel D. Effects of Spanwise and Discrete Disturbances on Separating Boundary Layers on Low Pressure Turbine Blades.

Degree: MS, 2007, Brigham Young University

 Flow measurements were made on two highly loaded, low pressure turbine blade configurations in a low-speed, linear cascade facility. The L1M blade has a design… (more)

Subjects/Keywords: active flow control; VGJ; vortex generator jets; wakes; transition; hot film; separation; Mechanical Engineering

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APA (6th Edition):

Reimann, D. D. (2007). Effects of Spanwise and Discrete Disturbances on Separating Boundary Layers on Low Pressure Turbine Blades. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1882&context=etd

Chicago Manual of Style (16th Edition):

Reimann, Daniel D. “Effects of Spanwise and Discrete Disturbances on Separating Boundary Layers on Low Pressure Turbine Blades.” 2007. Masters Thesis, Brigham Young University. Accessed January 18, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1882&context=etd.

MLA Handbook (7th Edition):

Reimann, Daniel D. “Effects of Spanwise and Discrete Disturbances on Separating Boundary Layers on Low Pressure Turbine Blades.” 2007. Web. 18 Jan 2021.

Vancouver:

Reimann DD. Effects of Spanwise and Discrete Disturbances on Separating Boundary Layers on Low Pressure Turbine Blades. [Internet] [Masters thesis]. Brigham Young University; 2007. [cited 2021 Jan 18]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1882&context=etd.

Council of Science Editors:

Reimann DD. Effects of Spanwise and Discrete Disturbances on Separating Boundary Layers on Low Pressure Turbine Blades. [Masters Thesis]. Brigham Young University; 2007. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1882&context=etd


Brno University of Technology

9. Daňko, Matúš. Přehled metod aktivního řízení proudu a jejich aplikací: Overview of active flow control methods and their application.

Degree: 2018, Brno University of Technology

Purpose of this study is to create an overview of currently the most used active flow control methods and their application. Thesis also contains brief historical overview of flow control development along with comparison of individual methods. Advisors/Committee Members: Dvořák, Petr (advisor), Brožek, Petr (referee).

Subjects/Keywords: metódy aktívneho riadenia prúdu; profil krídla; aktuátor; syntetizovaný prúd; vzduchový prúd; odtrhnutie vzduchového prúdu; fluidné aktuátory; plazma aktuátory; usmerňovanie ťahu; active flow control; airfoil; actuator; synthetic jet; airflow; airflow separation; fluidic actuators; plasma actuators; thrust vectoring

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APA (6th Edition):

Daňko, M. (2018). Přehled metod aktivního řízení proudu a jejich aplikací: Overview of active flow control methods and their application. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/40665

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):

Daňko, Matúš. “Přehled metod aktivního řízení proudu a jejich aplikací: Overview of active flow control methods and their application.” 2018. Thesis, Brno University of Technology. Accessed January 18, 2021. http://hdl.handle.net/11012/40665.

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

MLA Handbook (7th Edition):

Daňko, Matúš. “Přehled metod aktivního řízení proudu a jejich aplikací: Overview of active flow control methods and their application.” 2018. Web. 18 Jan 2021.

Vancouver:

Daňko M. Přehled metod aktivního řízení proudu a jejich aplikací: Overview of active flow control methods and their application. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/11012/40665.

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

Council of Science Editors:

Daňko M. Přehled metod aktivního řízení proudu a jejich aplikací: Overview of active flow control methods and their application. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/40665

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


Brigham Young University

10. Hansen, Laura C. Phase Locked Flow Measurements of Steady and Unsteady Vortex Generator Jets in a Separating Boundary Layer.

Degree: MS, 2005, Brigham Young University

  Vortex generator jets (VGJs) have been found to be an effective method of active separation control on the suction side of a low pressure… (more)

Subjects/Keywords: active flow control; boundary layer separation control; steady vortex generator jets; pulsed vortex generator jets; separation bubble analysis; low pressure turbine blade design; phase locked PIV measurements; Mechanical Engineering

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APA (6th Edition):

Hansen, L. C. (2005). Phase Locked Flow Measurements of Steady and Unsteady Vortex Generator Jets in a Separating Boundary Layer. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1267&context=etd

Chicago Manual of Style (16th Edition):

Hansen, Laura C. “Phase Locked Flow Measurements of Steady and Unsteady Vortex Generator Jets in a Separating Boundary Layer.” 2005. Masters Thesis, Brigham Young University. Accessed January 18, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1267&context=etd.

MLA Handbook (7th Edition):

Hansen, Laura C. “Phase Locked Flow Measurements of Steady and Unsteady Vortex Generator Jets in a Separating Boundary Layer.” 2005. Web. 18 Jan 2021.

Vancouver:

Hansen LC. Phase Locked Flow Measurements of Steady and Unsteady Vortex Generator Jets in a Separating Boundary Layer. [Internet] [Masters thesis]. Brigham Young University; 2005. [cited 2021 Jan 18]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1267&context=etd.

Council of Science Editors:

Hansen LC. Phase Locked Flow Measurements of Steady and Unsteady Vortex Generator Jets in a Separating Boundary Layer. [Masters Thesis]. Brigham Young University; 2005. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1267&context=etd

11. Kim, Yong Jea. Simulation of full-scale combustion instabilities in small-scale rigs using actively controlled boundary conditions.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The onset of combustion instabilities (CIs) has hindered the development and performance of combustion systems employed in industrial, power generation and propulsion systems for many… (more)

Subjects/Keywords: Active control system; Real time; Active acoustic boundary control; Impedance control; Wave separation algorithm; Small-scale rig; Sub-scale rig; Tangential combustion instability; Spinning instability; Tangential mean flow component; Mean flow; Annular combustor

Active impedance control for one-dimensional sound, from Guicking and Karcher [10]… …x28;a) experimental setup, (b) active impedance control with two feedback… …17 Figure 7. Impedance tuning of a premixed combustor using active control, from Bothien… …test rig, (b) application of the active control scheme… …19 Figure 8. A schematic of the active control system used by previous investigators (… 

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APA (6th Edition):

Kim, Y. J. (2017). Simulation of full-scale combustion instabilities in small-scale rigs using actively controlled boundary conditions. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59255

Chicago Manual of Style (16th Edition):

Kim, Yong Jea. “Simulation of full-scale combustion instabilities in small-scale rigs using actively controlled boundary conditions.” 2017. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/59255.

MLA Handbook (7th Edition):

Kim, Yong Jea. “Simulation of full-scale combustion instabilities in small-scale rigs using actively controlled boundary conditions.” 2017. Web. 18 Jan 2021.

Vancouver:

Kim YJ. Simulation of full-scale combustion instabilities in small-scale rigs using actively controlled boundary conditions. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/59255.

Council of Science Editors:

Kim YJ. Simulation of full-scale combustion instabilities in small-scale rigs using actively controlled boundary conditions. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59255

12. Metka, Matthew. Application of Fluidic Oscillator Separation Control to a Square-back Vehicle Model.

Degree: MS, Mechanical Engineering, 2015, The Ohio State University

 Aerodynamic drag is an increasingly important factor in ground vehicle design due to its large impact on overall fuel economy. The average vehicle drag coefficient… (more)

Subjects/Keywords: Aerospace Engineering; Automotive Engineering; Mechanical Engineering; separation control; aerodynamics; drag reduction; bluff body; Ahmed model; fluidic oscillator; bluff body wake; active flow control

…oscillators are increasingly recognized as efficient active separation control devices, with a… …9 1.4.2 Semi-Active Flow Control… …10 viii 1.4.3 Active Flow Control… …31 3.1. Local Effects of Fluidic Oscillator Separation Control… …31 3.2. Global Effects of Separation Control on the Wake… 

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APA (6th Edition):

Metka, M. (2015). Application of Fluidic Oscillator Separation Control to a Square-back Vehicle Model. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1439205355

Chicago Manual of Style (16th Edition):

Metka, Matthew. “Application of Fluidic Oscillator Separation Control to a Square-back Vehicle Model.” 2015. Masters Thesis, The Ohio State University. Accessed January 18, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=osu1439205355.

MLA Handbook (7th Edition):

Metka, Matthew. “Application of Fluidic Oscillator Separation Control to a Square-back Vehicle Model.” 2015. Web. 18 Jan 2021.

Vancouver:

Metka M. Application of Fluidic Oscillator Separation Control to a Square-back Vehicle Model. [Internet] [Masters thesis]. The Ohio State University; 2015. [cited 2021 Jan 18]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1439205355.

Council of Science Editors:

Metka M. Application of Fluidic Oscillator Separation Control to a Square-back Vehicle Model. [Masters Thesis]. The Ohio State University; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1439205355

13. Mello, Hilton Carlos de Miranda. Estudo dos efeitos de um jato sintético simulado numericamente no atraso da separação de uma camada limite sobre um aerofólio hipotético.

Degree: PhD, Engenharia Mecânica, 2005, University of São Paulo

A realização deste trabalho tem como objetivo fundamental estudar os efeitos dos atuadores de jato sintético no escoamento de uma camada limite desenvolvida sobre uma… (more)

Subjects/Keywords: active flow control; atraso da separação; Blasius boundary layer; camada limite de Blasius; camada limite de Falkner-Skan; controle ativo de escoamento; delay of separation; Falkner-Skan boundary layer; jato sintético; synthetic jet

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APA (6th Edition):

Mello, H. C. d. M. (2005). Estudo dos efeitos de um jato sintético simulado numericamente no atraso da separação de uma camada limite sobre um aerofólio hipotético. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18135/tde-26022006-111816/ ;

Chicago Manual of Style (16th Edition):

Mello, Hilton Carlos de Miranda. “Estudo dos efeitos de um jato sintético simulado numericamente no atraso da separação de uma camada limite sobre um aerofólio hipotético.” 2005. Doctoral Dissertation, University of São Paulo. Accessed January 18, 2021. http://www.teses.usp.br/teses/disponiveis/18/18135/tde-26022006-111816/ ;.

MLA Handbook (7th Edition):

Mello, Hilton Carlos de Miranda. “Estudo dos efeitos de um jato sintético simulado numericamente no atraso da separação de uma camada limite sobre um aerofólio hipotético.” 2005. Web. 18 Jan 2021.

Vancouver:

Mello HCdM. Estudo dos efeitos de um jato sintético simulado numericamente no atraso da separação de uma camada limite sobre um aerofólio hipotético. [Internet] [Doctoral dissertation]. University of São Paulo; 2005. [cited 2021 Jan 18]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18135/tde-26022006-111816/ ;.

Council of Science Editors:

Mello HCdM. Estudo dos efeitos de um jato sintético simulado numericamente no atraso da separação de uma camada limite sobre um aerofólio hipotético. [Doctoral Dissertation]. University of São Paulo; 2005. Available from: http://www.teses.usp.br/teses/disponiveis/18/18135/tde-26022006-111816/ ;

14. Jhaveri, Viyat Viral. Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator.

Degree: MS, Mechanical Engineering, 2017, Georgia Tech

 The use of active flow control (AFC) on civil transport aircraft flaps can delay stall at low aircraft speeds. This can lead to reducing the… (more)

Subjects/Keywords: AFC; FO; Fluidic oscillator; Active flow control; Flaps; Boundary layer; Separation; Low speed lift; Coefficient of momentum; Manufacturing; Materials; Oscillation frequency; Fluidic power

…114 x LIST OF SYMBOLS AND ABBREVIATIONS A Area AFC Active Flow Control ANOVA Analysis of… …𝜈 Kinematic Viscosity xii SUMMARY The use of active flow control (AFC) on… …Recently, active flow control (AFC) devices have gained popularity due to the potential… …of Active Flow Control, the different types of AFC devices, how they operate, and how they… …knowledge gaps and challenges in integrating active flow control devices into aircraft, it is… 

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

APA (6th Edition):

Jhaveri, V. V. (2017). Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58221

Chicago Manual of Style (16th Edition):

Jhaveri, Viyat Viral. “Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator.” 2017. Masters Thesis, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/58221.

MLA Handbook (7th Edition):

Jhaveri, Viyat Viral. “Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator.” 2017. Web. 18 Jan 2021.

Vancouver:

Jhaveri VV. Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator. [Internet] [Masters thesis]. Georgia Tech; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/58221.

Council of Science Editors:

Jhaveri VV. Effect of dimensional variation, manufacturing process, and material on performance of fluidic oscillator. [Masters Thesis]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58221

15. Ebrahiminejad Rafsanjani, Amin. Towards small scale sensors for turbulent flows and for rarefied gas damping.

Degree: Department of Mechanical Engineering, 2018, University of Victoria

 This thesis makes contributions towards the development of two different small-scale sensing systems which show promise for measurements in fluid mechanics. Well-resolved turbulent Wall Shear… (more)

Subjects/Keywords: turbulence fluctuations; Wall shear stress; Thermal sensors; Thermal anemometry; Large eddy simulations; Wind turbine control systems; Active flow control; Separation of nanoparticles; electrodeposition in templates; Rhodium nanowires; bidisperse suspension; Nanowire fabrication

…of this thesis that is focused on this topic is called “nanowire separation”. 1.1 Thesis… …applications of thermal WSS sensors in wind turbine control systems –how the information that a… …capable thermal WSS sensor provides for the control system of wind turbines can be used to avoid… …flow separation, and consequently, prolong the life span of wind turbine blades, is discussed… …turbulent structures, as well as being helpful field instruments for flow control system input. In… 

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

APA (6th Edition):

Ebrahiminejad Rafsanjani, A. (2018). Towards small scale sensors for turbulent flows and for rarefied gas damping. (Masters Thesis). University of Victoria. Retrieved from https://dspace.library.uvic.ca//handle/1828/8929

Chicago Manual of Style (16th Edition):

Ebrahiminejad Rafsanjani, Amin. “Towards small scale sensors for turbulent flows and for rarefied gas damping.” 2018. Masters Thesis, University of Victoria. Accessed January 18, 2021. https://dspace.library.uvic.ca//handle/1828/8929.

MLA Handbook (7th Edition):

Ebrahiminejad Rafsanjani, Amin. “Towards small scale sensors for turbulent flows and for rarefied gas damping.” 2018. Web. 18 Jan 2021.

Vancouver:

Ebrahiminejad Rafsanjani A. Towards small scale sensors for turbulent flows and for rarefied gas damping. [Internet] [Masters thesis]. University of Victoria; 2018. [cited 2021 Jan 18]. Available from: https://dspace.library.uvic.ca//handle/1828/8929.

Council of Science Editors:

Ebrahiminejad Rafsanjani A. Towards small scale sensors for turbulent flows and for rarefied gas damping. [Masters Thesis]. University of Victoria; 2018. Available from: https://dspace.library.uvic.ca//handle/1828/8929

.