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You searched for subject:(Combustor). Showing records 1 – 30 of 126 total matches.

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University of Pretoria

1. Gouws, Johannes Jacobus. Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor.

Degree: MEng, Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 Gas turbine combustion chambers were traditionally designed through trial and error which was unfortunately a time-consuming and expensive process. The development of computers, however, contributed… (more)

Subjects/Keywords: Turbine combustor; Fluid dynamics; UCTD

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APA (6th Edition):

Gouws, J. (2008). Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/24042

Chicago Manual of Style (16th Edition):

Gouws, Johannes. “Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor.” 2008. Masters Thesis, University of Pretoria. Accessed December 15, 2019. http://hdl.handle.net/2263/24042.

MLA Handbook (7th Edition):

Gouws, Johannes. “Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor.” 2008. Web. 15 Dec 2019.

Vancouver:

Gouws J. Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/2263/24042.

Council of Science Editors:

Gouws J. Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/24042


University of Pretoria

2. [No author]. Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor .

Degree: 2008, University of Pretoria

 Gas turbine combustion chambers were traditionally designed through trial and error which was unfortunately a time-consuming and expensive process. The development of computers, however, contributed… (more)

Subjects/Keywords: Turbine combustor; Fluid dynamics; UCTD

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APA (6th Edition):

author], [. (2008). Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-04212008-074344/

Chicago Manual of Style (16th Edition):

author], [No. “Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor .” 2008. Masters Thesis, University of Pretoria. Accessed December 15, 2019. http://upetd.up.ac.za/thesis/available/etd-04212008-074344/.

MLA Handbook (7th Edition):

author], [No. “Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor .” 2008. Web. 15 Dec 2019.

Vancouver:

author] [. Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2019 Dec 15]. Available from: http://upetd.up.ac.za/thesis/available/etd-04212008-074344/.

Council of Science Editors:

author] [. Combining a one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-04212008-074344/


Penn State University

3. Leonetti, Michael John. RQL Combustor Dilution Hole Placement and its Effect on the Turbine Inlet Flowfield.

Degree: MS, Mechanical Engineering, 2016, Penn State University

 Dilution jets in a gas turbine combustor are used to oxidize remaining fuel from the main flame zone in the combustor, and to homogenize the… (more)

Subjects/Keywords: combustor; dilution; piv; turbulence; turbine

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APA (6th Edition):

Leonetti, M. J. (2016). RQL Combustor Dilution Hole Placement and its Effect on the Turbine Inlet Flowfield. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/28681

Chicago Manual of Style (16th Edition):

Leonetti, Michael John. “RQL Combustor Dilution Hole Placement and its Effect on the Turbine Inlet Flowfield.” 2016. Masters Thesis, Penn State University. Accessed December 15, 2019. https://etda.libraries.psu.edu/catalog/28681.

MLA Handbook (7th Edition):

Leonetti, Michael John. “RQL Combustor Dilution Hole Placement and its Effect on the Turbine Inlet Flowfield.” 2016. Web. 15 Dec 2019.

Vancouver:

Leonetti MJ. RQL Combustor Dilution Hole Placement and its Effect on the Turbine Inlet Flowfield. [Internet] [Masters thesis]. Penn State University; 2016. [cited 2019 Dec 15]. Available from: https://etda.libraries.psu.edu/catalog/28681.

Council of Science Editors:

Leonetti MJ. RQL Combustor Dilution Hole Placement and its Effect on the Turbine Inlet Flowfield. [Masters Thesis]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/28681


NSYSU

4. Chen, Jia-Kai. Flame ignition/quenching behavior in tiny tube.

Degree: Master, Mechanical and Electro-Mechanical Engineering, 2014, NSYSU

 A new model to discuss the behavior of flame repetitive ignition/quenching spread in a tiny tube is established in this study. This new model mainly… (more)

Subjects/Keywords: micro combustor; unsteady propagation flame; Lewis number

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APA (6th Edition):

Chen, J. (2014). Flame ignition/quenching behavior in tiny tube. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0322114-201039

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):

Chen, Jia-Kai. “Flame ignition/quenching behavior in tiny tube.” 2014. Thesis, NSYSU. Accessed December 15, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0322114-201039.

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

MLA Handbook (7th Edition):

Chen, Jia-Kai. “Flame ignition/quenching behavior in tiny tube.” 2014. Web. 15 Dec 2019.

Vancouver:

Chen J. Flame ignition/quenching behavior in tiny tube. [Internet] [Thesis]. NSYSU; 2014. [cited 2019 Dec 15]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0322114-201039.

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

Council of Science Editors:

Chen J. Flame ignition/quenching behavior in tiny tube. [Thesis]. NSYSU; 2014. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0322114-201039

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

5. Xavier, Pradip. Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder : Investigation des mécanismes de stabilisation d'une flamme dans une chambre de combustion prémélangée à l'aide d'une cavité de gaz chauds.

Degree: Docteur es, Physique, 2014, Rouen, INSA

Cette thèse décrit l'étude d'une chambre de combustion innovante de type Trapped Vortex Combustor (TVC): ce concept utilise des cavités de gaz chauds pour stabiliser… (more)

Subjects/Keywords: Diagnostic laser rapide; Trapped Vortex Combustor

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APA (6th Edition):

Xavier, P. (2014). Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder : Investigation des mécanismes de stabilisation d'une flamme dans une chambre de combustion prémélangée à l'aide d'une cavité de gaz chauds. (Doctoral Dissertation). Rouen, INSA. Retrieved from http://www.theses.fr/2014ISAM0016

Chicago Manual of Style (16th Edition):

Xavier, Pradip. “Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder : Investigation des mécanismes de stabilisation d'une flamme dans une chambre de combustion prémélangée à l'aide d'une cavité de gaz chauds.” 2014. Doctoral Dissertation, Rouen, INSA. Accessed December 15, 2019. http://www.theses.fr/2014ISAM0016.

MLA Handbook (7th Edition):

Xavier, Pradip. “Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder : Investigation des mécanismes de stabilisation d'une flamme dans une chambre de combustion prémélangée à l'aide d'une cavité de gaz chauds.” 2014. Web. 15 Dec 2019.

Vancouver:

Xavier P. Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder : Investigation des mécanismes de stabilisation d'une flamme dans une chambre de combustion prémélangée à l'aide d'une cavité de gaz chauds. [Internet] [Doctoral dissertation]. Rouen, INSA; 2014. [cited 2019 Dec 15]. Available from: http://www.theses.fr/2014ISAM0016.

Council of Science Editors:

Xavier P. Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder : Investigation des mécanismes de stabilisation d'une flamme dans une chambre de combustion prémélangée à l'aide d'une cavité de gaz chauds. [Doctoral Dissertation]. Rouen, INSA; 2014. Available from: http://www.theses.fr/2014ISAM0016


King Abdullah University of Science and Technology

6. Qatomah, Mohammad. Experimental Investigation on The Influence of Liquid Fuels Composition on The Operational Characteristics of The Liquid Fueled Resonant Pulse Combustor.

Degree: 2018, King Abdullah University of Science and Technology

 In this study, the response of a liquid-fueled resonant pulse combustor to changes in liquid fuel composition was investigated. Experiments were performed with gasoline- ethanol,… (more)

Subjects/Keywords: Pulse combustor; Pressure gain; Liquid Fuels

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APA (6th Edition):

Qatomah, M. (2018). Experimental Investigation on The Influence of Liquid Fuels Composition on The Operational Characteristics of The Liquid Fueled Resonant Pulse Combustor. (Thesis). King Abdullah University of Science and Technology. Retrieved from http://hdl.handle.net/10754/628038

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):

Qatomah, Mohammad. “Experimental Investigation on The Influence of Liquid Fuels Composition on The Operational Characteristics of The Liquid Fueled Resonant Pulse Combustor.” 2018. Thesis, King Abdullah University of Science and Technology. Accessed December 15, 2019. http://hdl.handle.net/10754/628038.

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

MLA Handbook (7th Edition):

Qatomah, Mohammad. “Experimental Investigation on The Influence of Liquid Fuels Composition on The Operational Characteristics of The Liquid Fueled Resonant Pulse Combustor.” 2018. Web. 15 Dec 2019.

Vancouver:

Qatomah M. Experimental Investigation on The Influence of Liquid Fuels Composition on The Operational Characteristics of The Liquid Fueled Resonant Pulse Combustor. [Internet] [Thesis]. King Abdullah University of Science and Technology; 2018. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/10754/628038.

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

Council of Science Editors:

Qatomah M. Experimental Investigation on The Influence of Liquid Fuels Composition on The Operational Characteristics of The Liquid Fueled Resonant Pulse Combustor. [Thesis]. King Abdullah University of Science and Technology; 2018. Available from: http://hdl.handle.net/10754/628038

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


Cranfield University

7. Prakash, Atma. Prediction of NOX emissions for an RQL combustor using a stirred reactor modelling approach.

Degree: PhD, 2015, Cranfield University

 In an effort to reduce NOX emissions both in the landing and take-off (LTO) cycle as well as in cruise, significant research has been conducted… (more)

Subjects/Keywords: 629.134; NOX; CO; Combustor; Emission Prediction; Novel Combustor; RQL; Stirred Reactor & Shale gas

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APA (6th Edition):

Prakash, A. (2015). Prediction of NOX emissions for an RQL combustor using a stirred reactor modelling approach. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10010 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.687772

Chicago Manual of Style (16th Edition):

Prakash, Atma. “Prediction of NOX emissions for an RQL combustor using a stirred reactor modelling approach.” 2015. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/10010 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.687772.

MLA Handbook (7th Edition):

Prakash, Atma. “Prediction of NOX emissions for an RQL combustor using a stirred reactor modelling approach.” 2015. Web. 15 Dec 2019.

Vancouver:

Prakash A. Prediction of NOX emissions for an RQL combustor using a stirred reactor modelling approach. [Internet] [Doctoral dissertation]. Cranfield University; 2015. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10010 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.687772.

Council of Science Editors:

Prakash A. Prediction of NOX emissions for an RQL combustor using a stirred reactor modelling approach. [Doctoral Dissertation]. Cranfield University; 2015. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10010 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.687772


Cranfield University

8. Khandelwal, Bhupendra. Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts.

Degree: PhD, 2012, Cranfield University

 It is widely accepted that climate change is a very serious environmental concern. Levels of carbon dioxide (CO2) and other emissions in the global atmosphere… (more)

Subjects/Keywords: 621.43; Combustor; Gas Turbine Combustor Design; Novel Combustors; Hydrogen synthesis; kerosene reforming; Hydrogen enriched combustion

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

APA (6th Edition):

Khandelwal, B. (2012). Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/9157 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.637502

Chicago Manual of Style (16th Edition):

Khandelwal, Bhupendra. “Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts.” 2012. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/9157 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.637502.

MLA Handbook (7th Edition):

Khandelwal, Bhupendra. “Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts.” 2012. Web. 15 Dec 2019.

Vancouver:

Khandelwal B. Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts. [Internet] [Doctoral dissertation]. Cranfield University; 2012. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9157 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.637502.

Council of Science Editors:

Khandelwal B. Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts. [Doctoral Dissertation]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9157 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.637502


Cranfield University

9. Khandelwal, Bhupendra. Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts.

Degree: PhD, 2012, Cranfield University

 It is widely accepted that climate change is a very serious environmental concern. Levels of carbon dioxide (CO2) and other emissions in the global atmosphere… (more)

Subjects/Keywords: Combustor; Gas Turbine Combustor Design; Novel Combustors; Hydrogen synthesis; kerosene reforming; Hydrogen enriched combustion

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

APA (6th Edition):

Khandelwal, B. (2012). Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/9157

Chicago Manual of Style (16th Edition):

Khandelwal, Bhupendra. “Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts.” 2012. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/9157.

MLA Handbook (7th Edition):

Khandelwal, Bhupendra. “Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts.” 2012. Web. 15 Dec 2019.

Vancouver:

Khandelwal B. Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts. [Internet] [Doctoral dissertation]. Cranfield University; 2012. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9157.

Council of Science Editors:

Khandelwal B. Development of gas turbine combustor preliminary design methodologies and preliminary assessments of advanced low emission combustor concepts. [Doctoral Dissertation]. Cranfield University; 2012. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9157


Indian Institute of Science

10. Sivaprakasam, M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.

Degree: 2010, Indian Institute of Science

 In the present work, two phase reacting flow in a single cavity Trapped Vortex Combustor (TVC) is studied at atmospheric conditions. KIVA-3V, numerical program for… (more)

Subjects/Keywords: Trapped Vortex Combustor (TVC); Cavity Combustor; Trapped Vortex Combustor - Flow Modelling; Ramjet Engines; Trapped Vortex Combustor - Two Phase Reacting Flow; Cavity Combustor - Reacting Flow - Numerical Simulations; Taylor Analogy Breakup (TAB); Heat Engineering

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APA (6th Edition):

Sivaprakasam, M. (2010). Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2011

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):

Sivaprakasam, M. “Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.” 2010. Thesis, Indian Institute of Science. Accessed December 15, 2019. http://hdl.handle.net/2005/2011.

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

MLA Handbook (7th Edition):

Sivaprakasam, M. “Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.” 2010. Web. 15 Dec 2019.

Vancouver:

Sivaprakasam M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/2005/2011.

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

Council of Science Editors:

Sivaprakasam M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. [Thesis]. Indian Institute of Science; 2010. Available from: http://hdl.handle.net/2005/2011

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


Indian Institute of Science

11. Sivaprakasam, M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.

Degree: 2010, Indian Institute of Science

 In the present work, two phase reacting flow in a single cavity Trapped Vortex Combustor (TVC) is studied at atmospheric conditions. KIVA-3V, numerical program for… (more)

Subjects/Keywords: Trapped Vortex Combustor (TVC); Cavity Combustor; Trapped Vortex Combustor - Flow Modelling; Ramjet Engines; Trapped Vortex Combustor - Two Phase Reacting Flow; Cavity Combustor - Reacting Flow - Numerical Simulations; Taylor Analogy Breakup (TAB); Heat Engineering

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

APA (6th Edition):

Sivaprakasam, M. (2010). Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2011 ; http://etd.ncsi.iisc.ernet.in/abstracts/2603/G24902-Abs.pdf

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

Chicago Manual of Style (16th Edition):

Sivaprakasam, M. “Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.” 2010. Thesis, Indian Institute of Science. Accessed December 15, 2019. http://etd.iisc.ernet.in/handle/2005/2011 ; http://etd.ncsi.iisc.ernet.in/abstracts/2603/G24902-Abs.pdf.

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

MLA Handbook (7th Edition):

Sivaprakasam, M. “Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor.” 2010. Web. 15 Dec 2019.

Vancouver:

Sivaprakasam M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Dec 15]. Available from: http://etd.iisc.ernet.in/handle/2005/2011 ; http://etd.ncsi.iisc.ernet.in/abstracts/2603/G24902-Abs.pdf.

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

Council of Science Editors:

Sivaprakasam M. Numerical Simulations Of Two-Phase Reacting Flow In A Cavity Combustor. [Thesis]. Indian Institute of Science; 2010. Available from: http://etd.iisc.ernet.in/handle/2005/2011 ; http://etd.ncsi.iisc.ernet.in/abstracts/2603/G24902-Abs.pdf

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


Penn State University

12. Shrager, Adam. Effect of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner.

Degree: 2017, Penn State University

 Gas turbine engines are an important technology for power generation and aircraft propulsion due to their relatively high efficiencies compared to other methods of power… (more)

Subjects/Keywords: Combustor; Combustor Liner; Gas Turbine Engine; Effusion Cooling; Dilution Hole; Heat Transfer; Flowfield Visualization; Particle Image Velocimetry

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APA (6th Edition):

Shrager, A. (2017). Effect of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/14709acs5431

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):

Shrager, Adam. “Effect of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner.” 2017. Thesis, Penn State University. Accessed December 15, 2019. https://etda.libraries.psu.edu/catalog/14709acs5431.

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

MLA Handbook (7th Edition):

Shrager, Adam. “Effect of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner.” 2017. Web. 15 Dec 2019.

Vancouver:

Shrager A. Effect of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner. [Internet] [Thesis]. Penn State University; 2017. [cited 2019 Dec 15]. Available from: https://etda.libraries.psu.edu/catalog/14709acs5431.

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

Council of Science Editors:

Shrager A. Effect of Effusion Cooling Pattern Near the Dilution Hole for a Double-Walled Combustor Liner. [Thesis]. Penn State University; 2017. Available from: https://etda.libraries.psu.edu/catalog/14709acs5431

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


University of Minnesota

13. Ayaskanta, Arya. Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade.

Degree: MS, Mechanical Engineering, 2013, University of Minnesota

University of Minnesota M.S. thesis. May 2013. Major: Mechanical Engineering. Advisor: Terrence W. Simon. 1 computer file (PDF); xii, 123 pages.

The effects of an… (more)

Subjects/Keywords: Adiabatic effectiveness; Combustor exit profile; Contouring; Endwall heat transfer; Leakage flow

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APA (6th Edition):

Ayaskanta, A. (2013). Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/156570

Chicago Manual of Style (16th Edition):

Ayaskanta, Arya. “Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade.” 2013. Masters Thesis, University of Minnesota. Accessed December 15, 2019. http://purl.umn.edu/156570.

MLA Handbook (7th Edition):

Ayaskanta, Arya. “Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade.” 2013. Web. 15 Dec 2019.

Vancouver:

Ayaskanta A. Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade. [Internet] [Masters thesis]. University of Minnesota; 2013. [cited 2019 Dec 15]. Available from: http://purl.umn.edu/156570.

Council of Science Editors:

Ayaskanta A. Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade. [Masters Thesis]. University of Minnesota; 2013. Available from: http://purl.umn.edu/156570


Loughborough University

14. Martin, Damian. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.

Degree: PhD, 2013, Loughborough University

 Full-coverage or effusion cooling is commonly used in the thermal management of gas turbine combustion systems. The combustor environment is characterised by highly turbulent free-stream… (more)

Subjects/Keywords: 621.43; Heat transfer; Film cooling; Combustor; Turbulence; Effusion

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APA (6th Edition):

Martin, D. (2013). Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844

Chicago Manual of Style (16th Edition):

Martin, Damian. “Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.” 2013. Doctoral Dissertation, Loughborough University. Accessed December 15, 2019. https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844.

MLA Handbook (7th Edition):

Martin, Damian. “Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.” 2013. Web. 15 Dec 2019.

Vancouver:

Martin D. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2019 Dec 15]. Available from: https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844.

Council of Science Editors:

Martin D. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. [Doctoral Dissertation]. Loughborough University; 2013. Available from: https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844


Loughborough University

15. Melia, Thomas. Heat transfer characteristics of pulse combustors for gas turbine engines.

Degree: PhD, 2012, Loughborough University

 Conventional gas turbine combustors operate with a designed drop in pressure over the length of the device. This is desired in order to encourage mixing… (more)

Subjects/Keywords: 629.134; Pulse combustor; Heat transfer; Jet engines; Pressure gain combustion

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APA (6th Edition):

Melia, T. (2012). Heat transfer characteristics of pulse combustors for gas turbine engines. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/10278 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682508

Chicago Manual of Style (16th Edition):

Melia, Thomas. “Heat transfer characteristics of pulse combustors for gas turbine engines.” 2012. Doctoral Dissertation, Loughborough University. Accessed December 15, 2019. https://dspace.lboro.ac.uk/2134/10278 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682508.

MLA Handbook (7th Edition):

Melia, Thomas. “Heat transfer characteristics of pulse combustors for gas turbine engines.” 2012. Web. 15 Dec 2019.

Vancouver:

Melia T. Heat transfer characteristics of pulse combustors for gas turbine engines. [Internet] [Doctoral dissertation]. Loughborough University; 2012. [cited 2019 Dec 15]. Available from: https://dspace.lboro.ac.uk/2134/10278 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682508.

Council of Science Editors:

Melia T. Heat transfer characteristics of pulse combustors for gas turbine engines. [Doctoral Dissertation]. Loughborough University; 2012. Available from: https://dspace.lboro.ac.uk/2134/10278 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682508


Loughborough University

16. Peacock, Graham. Enhanced cold-side cooling techniques for lean burn combustor liners.

Degree: PhD, 2013, Loughborough University

 In order to meet the increasingly strict emissions targets required in modern civil aviation, lean burn combustors are being pursued as a means to reduce… (more)

Subjects/Keywords: 621.402; Cooling; Heat transfer; Impingement; Pedestal; Liquid crystal; Combustor liner

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APA (6th Edition):

Peacock, G. (2013). Enhanced cold-side cooling techniques for lean burn combustor liners. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/12329 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682516

Chicago Manual of Style (16th Edition):

Peacock, Graham. “Enhanced cold-side cooling techniques for lean burn combustor liners.” 2013. Doctoral Dissertation, Loughborough University. Accessed December 15, 2019. https://dspace.lboro.ac.uk/2134/12329 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682516.

MLA Handbook (7th Edition):

Peacock, Graham. “Enhanced cold-side cooling techniques for lean burn combustor liners.” 2013. Web. 15 Dec 2019.

Vancouver:

Peacock G. Enhanced cold-side cooling techniques for lean burn combustor liners. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2019 Dec 15]. Available from: https://dspace.lboro.ac.uk/2134/12329 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682516.

Council of Science Editors:

Peacock G. Enhanced cold-side cooling techniques for lean burn combustor liners. [Doctoral Dissertation]. Loughborough University; 2013. Available from: https://dspace.lboro.ac.uk/2134/12329 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.682516


University of Kansas

17. Tourani, Chandraprakash Chandra. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.

Degree: MS, Aerospace Engineering, 2011, University of Kansas

 1-D simulations based on the quasi-one-dimensional equations of fluid motion plus an ignition delay model and 2-D numerical simulations based on Reynolds-Averaged Navier-Stokes (RANS) equations… (more)

Subjects/Keywords: Aerospace engineering; Air-breathing propulsion; Combustor; Hypersonic; Quasi one-dimensional; Scramjet

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APA (6th Edition):

Tourani, C. C. (2011). COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7635

Chicago Manual of Style (16th Edition):

Tourani, Chandraprakash Chandra. “COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.” 2011. Masters Thesis, University of Kansas. Accessed December 15, 2019. http://hdl.handle.net/1808/7635.

MLA Handbook (7th Edition):

Tourani, Chandraprakash Chandra. “COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.” 2011. Web. 15 Dec 2019.

Vancouver:

Tourani CC. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/1808/7635.

Council of Science Editors:

Tourani CC. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7635


University of Kansas

18. Hwang, Seung-Jae. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.

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

 Numerical simulations of the scramjet combustor by using the commercial CFD code Fluent with the coupled implicit method with second-order accurate discretization have been obtained… (more)

Subjects/Keywords: Aerospace engineering; Combustor; Enhanced; Mixing; Scramjet; Suction collar; Tabs

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APA (6th Edition):

Hwang, S. (2011). Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/8080

Chicago Manual of Style (16th Edition):

Hwang, Seung-Jae. “Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.” 2011. Doctoral Dissertation, University of Kansas. Accessed December 15, 2019. http://hdl.handle.net/1808/8080.

MLA Handbook (7th Edition):

Hwang, Seung-Jae. “Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.” 2011. Web. 15 Dec 2019.

Vancouver:

Hwang S. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. [Internet] [Doctoral dissertation]. University of Kansas; 2011. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/1808/8080.

Council of Science Editors:

Hwang S. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. [Doctoral Dissertation]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/8080


NSYSU

19. Hung, Cheng-Yen. The Study of Perforated-Plate Burner and Analysis of Radiation Efficiency by Using Numerical Model.

Degree: Master, Mechanical and Electro-Mechanical Engineering, 2014, NSYSU

 In this study, established a two dimensional CFD model with orthogonal mesh to simulate the combustion phenomenon of methane-air mixture gas in the radiation combustor.… (more)

Subjects/Keywords: radiation heat efficiency; radiation combustor; excess enthalpy combustion

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APA (6th Edition):

Hung, C. (2014). The Study of Perforated-Plate Burner and Analysis of Radiation Efficiency by Using Numerical Model. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0727114-001140

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):

Hung, Cheng-Yen. “The Study of Perforated-Plate Burner and Analysis of Radiation Efficiency by Using Numerical Model.” 2014. Thesis, NSYSU. Accessed December 15, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0727114-001140.

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

MLA Handbook (7th Edition):

Hung, Cheng-Yen. “The Study of Perforated-Plate Burner and Analysis of Radiation Efficiency by Using Numerical Model.” 2014. Web. 15 Dec 2019.

Vancouver:

Hung C. The Study of Perforated-Plate Burner and Analysis of Radiation Efficiency by Using Numerical Model. [Internet] [Thesis]. NSYSU; 2014. [cited 2019 Dec 15]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0727114-001140.

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

Council of Science Editors:

Hung C. The Study of Perforated-Plate Burner and Analysis of Radiation Efficiency by Using Numerical Model. [Thesis]. NSYSU; 2014. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0727114-001140

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


University of Cincinnati

20. Endicott, Derick S. Experimental Development of a Lean Direct Injection Combustor Utilizing High-Low Swirl Intensity Combinations.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2014, University of Cincinnati

 The focus of this research is to investigate the isothermal aerodynamic behavior of three LDI configurations utilizing a 3 x 3 array of radial-radial swirlers.… (more)

Subjects/Keywords: Aerospace Materials; lean; direct; injection; swirler; combustor; NOx

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APA (6th Edition):

Endicott, D. S. (2014). Experimental Development of a Lean Direct Injection Combustor Utilizing High-Low Swirl Intensity Combinations. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1416231599

Chicago Manual of Style (16th Edition):

Endicott, Derick S. “Experimental Development of a Lean Direct Injection Combustor Utilizing High-Low Swirl Intensity Combinations.” 2014. Masters Thesis, University of Cincinnati. Accessed December 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1416231599.

MLA Handbook (7th Edition):

Endicott, Derick S. “Experimental Development of a Lean Direct Injection Combustor Utilizing High-Low Swirl Intensity Combinations.” 2014. Web. 15 Dec 2019.

Vancouver:

Endicott DS. Experimental Development of a Lean Direct Injection Combustor Utilizing High-Low Swirl Intensity Combinations. [Internet] [Masters thesis]. University of Cincinnati; 2014. [cited 2019 Dec 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1416231599.

Council of Science Editors:

Endicott DS. Experimental Development of a Lean Direct Injection Combustor Utilizing High-Low Swirl Intensity Combinations. [Masters Thesis]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1416231599


Penn State University

21. Kalaskar, Vickey Baliram. EMISSION CHARACTERISTICS OF JP-8, JP-900, FISCHER-TROPSCH (FT) AND JP-8/FT BLENDS IN A MODEL GAS TURBINE COMBUSTOR.

Degree: MS, Mechanical Engineering, 2009, Penn State University

 The increasing usage of coal-based fuels in aviation turbines and fluctuating prices of the crude oil imports emphasizes the need to study and analyze alternate… (more)

Subjects/Keywords: jet fuels; coal-based; gas turbine; model combustor

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APA (6th Edition):

Kalaskar, V. B. (2009). EMISSION CHARACTERISTICS OF JP-8, JP-900, FISCHER-TROPSCH (FT) AND JP-8/FT BLENDS IN A MODEL GAS TURBINE COMBUSTOR. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10080

Chicago Manual of Style (16th Edition):

Kalaskar, Vickey Baliram. “EMISSION CHARACTERISTICS OF JP-8, JP-900, FISCHER-TROPSCH (FT) AND JP-8/FT BLENDS IN A MODEL GAS TURBINE COMBUSTOR.” 2009. Masters Thesis, Penn State University. Accessed December 15, 2019. https://etda.libraries.psu.edu/catalog/10080.

MLA Handbook (7th Edition):

Kalaskar, Vickey Baliram. “EMISSION CHARACTERISTICS OF JP-8, JP-900, FISCHER-TROPSCH (FT) AND JP-8/FT BLENDS IN A MODEL GAS TURBINE COMBUSTOR.” 2009. Web. 15 Dec 2019.

Vancouver:

Kalaskar VB. EMISSION CHARACTERISTICS OF JP-8, JP-900, FISCHER-TROPSCH (FT) AND JP-8/FT BLENDS IN A MODEL GAS TURBINE COMBUSTOR. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Dec 15]. Available from: https://etda.libraries.psu.edu/catalog/10080.

Council of Science Editors:

Kalaskar VB. EMISSION CHARACTERISTICS OF JP-8, JP-900, FISCHER-TROPSCH (FT) AND JP-8/FT BLENDS IN A MODEL GAS TURBINE COMBUSTOR. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/10080


University of Southern California

22. Chen, Chien-Hua. Geometrical effects on Swiss-roll heat-recirculating combustors.

Degree: PhD, Mechanical Engineering, 2011, University of Southern California

 A 3D numerical model of Swiss-roll combustor with considering heat loss to environment, turbulence, radiation, and simplified reaction mechanism (1-step and 4-step) was built. Comparisons… (more)

Subjects/Keywords: Swiss roll combustor; heat recirculating combustion; gas mask

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APA (6th Edition):

Chen, C. (2011). Geometrical effects on Swiss-roll heat-recirculating combustors. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/644689/rec/3031

Chicago Manual of Style (16th Edition):

Chen, Chien-Hua. “Geometrical effects on Swiss-roll heat-recirculating combustors.” 2011. Doctoral Dissertation, University of Southern California. Accessed December 15, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/644689/rec/3031.

MLA Handbook (7th Edition):

Chen, Chien-Hua. “Geometrical effects on Swiss-roll heat-recirculating combustors.” 2011. Web. 15 Dec 2019.

Vancouver:

Chen C. Geometrical effects on Swiss-roll heat-recirculating combustors. [Internet] [Doctoral dissertation]. University of Southern California; 2011. [cited 2019 Dec 15]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/644689/rec/3031.

Council of Science Editors:

Chen C. Geometrical effects on Swiss-roll heat-recirculating combustors. [Doctoral Dissertation]. University of Southern California; 2011. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll127/id/644689/rec/3031


Virginia Tech

23. Scrittore, Joseph. Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor.

Degree: PhD, Mechanical Engineering, 2008, Virginia Tech

 Cooling combustor chambers for gas turbine engines is challenging because of the complex flow fields inherent to this engine component. This complexity, in part, arises… (more)

Subjects/Keywords: Gas turbine; combustor; film cooling

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APA (6th Edition):

Scrittore, J. (2008). Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28171

Chicago Manual of Style (16th Edition):

Scrittore, Joseph. “Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor.” 2008. Doctoral Dissertation, Virginia Tech. Accessed December 15, 2019. http://hdl.handle.net/10919/28171.

MLA Handbook (7th Edition):

Scrittore, Joseph. “Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor.” 2008. Web. 15 Dec 2019.

Vancouver:

Scrittore J. Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor. [Internet] [Doctoral dissertation]. Virginia Tech; 2008. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/10919/28171.

Council of Science Editors:

Scrittore J. Experimental Study of the Effect of Dilution Jets on Film Cooling Flow in a Gas Turbine Combustor. [Doctoral Dissertation]. Virginia Tech; 2008. Available from: http://hdl.handle.net/10919/28171


University of Minnesota

24. Ayaskanta, Arya. Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade.

Degree: MS, Mechanical Engineering, 2013, University of Minnesota

 The effects of an engine representative combustor exit temperature profile on the adiabatic effectiveness values on a contoured turbine hub endwall at different disc cavity… (more)

Subjects/Keywords: Adiabatic effectiveness; Combustor exit profile; Contouring; Endwall heat transfer; Leakage flow

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APA (6th Edition):

Ayaskanta, A. (2013). Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade. (Masters Thesis). University of Minnesota. Retrieved from http://purl.umn.edu/156570

Chicago Manual of Style (16th Edition):

Ayaskanta, Arya. “Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade.” 2013. Masters Thesis, University of Minnesota. Accessed December 15, 2019. http://purl.umn.edu/156570.

MLA Handbook (7th Edition):

Ayaskanta, Arya. “Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade.” 2013. Web. 15 Dec 2019.

Vancouver:

Ayaskanta A. Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade. [Internet] [Masters thesis]. University of Minnesota; 2013. [cited 2019 Dec 15]. Available from: http://purl.umn.edu/156570.

Council of Science Editors:

Ayaskanta A. Experimental investigation of the effect of engine representative combustor exit temperature profile and disc cavity leakage flow on the film cooling of contoured Hub Endwall of a high pressure gas turbine rotor cascade. [Masters Thesis]. University of Minnesota; 2013. Available from: http://purl.umn.edu/156570


University of Cincinnati

25. Stoddard, William A. Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2018, University of Cincinnati

 PDE's (Pulse Detonation Engines) and RDE's (Rotating Detonation Engines) utilize a shock coupled burning wave to combust fuel and oxidizer or air at a near… (more)

Subjects/Keywords: Aerospace Materials; Detonation; PDE; RDE; CFD; Experimental; Combustor

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APA (6th Edition):

Stoddard, W. A. (2018). Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073

Chicago Manual of Style (16th Edition):

Stoddard, William A. “Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors.” 2018. Doctoral Dissertation, University of Cincinnati. Accessed December 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073.

MLA Handbook (7th Edition):

Stoddard, William A. “Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors.” 2018. Web. 15 Dec 2019.

Vancouver:

Stoddard WA. Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors. [Internet] [Doctoral dissertation]. University of Cincinnati; 2018. [cited 2019 Dec 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073.

Council of Science Editors:

Stoddard WA. Use of Computational Fluid Dynamics in Conjunction with Experimental Methods to Improve Designs of Detonation-Based Combustors. [Doctoral Dissertation]. University of Cincinnati; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1543921268222073


University of Cambridge

26. Valreau, Audrey Sophie Lisa. Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors .

Degree: 2019, University of Cambridge

 The drive towards environmentally-friendly gas turbine engines imposes strict design constraints on combustion chambers to minimise harmful pollutant emission. Measures employed to counter this issue… (more)

Subjects/Keywords: Combustion; Combustion Instability; CFD; Annular Combustor; Oscillatory Behaviour

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APA (6th Edition):

Valreau, A. S. L. (2019). Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors . (Thesis). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/292285

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):

Valreau, Audrey Sophie Lisa. “Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors .” 2019. Thesis, University of Cambridge. Accessed December 15, 2019. https://www.repository.cam.ac.uk/handle/1810/292285.

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

MLA Handbook (7th Edition):

Valreau, Audrey Sophie Lisa. “Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors .” 2019. Web. 15 Dec 2019.

Vancouver:

Valreau ASL. Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors . [Internet] [Thesis]. University of Cambridge; 2019. [cited 2019 Dec 15]. Available from: https://www.repository.cam.ac.uk/handle/1810/292285.

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

Council of Science Editors:

Valreau ASL. Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors . [Thesis]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/292285

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


Virginia Tech

27. Park, Suhyeon. Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows.

Degree: PhD, Mechanical Engineering, 2018, Virginia Tech

 The study of flow fields and heat transfer characteristics inside a gas turbine combustor provides one of the most serious challenges for gas turbine researchers… (more)

Subjects/Keywords: Heat transfer; gas turbine combustor; particle image velocimetry; infrared thermography

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

APA (6th Edition):

Park, S. (2018). Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/82349

Chicago Manual of Style (16th Edition):

Park, Suhyeon. “Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows.” 2018. Doctoral Dissertation, Virginia Tech. Accessed December 15, 2019. http://hdl.handle.net/10919/82349.

MLA Handbook (7th Edition):

Park, Suhyeon. “Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows.” 2018. Web. 15 Dec 2019.

Vancouver:

Park S. Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows. [Internet] [Doctoral dissertation]. Virginia Tech; 2018. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/10919/82349.

Council of Science Editors:

Park S. Experimental Investigation of Flow and Wall Heat Transfer in an Optical Combustor for Reacting Swirl Flows. [Doctoral Dissertation]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/82349


University of Cambridge

28. Valreau, Audrey Sophie Lisa. Computational fluid dynamics investigation of oscillatory behaviour in annular combustors.

Degree: PhD, 2019, University of Cambridge

 The drive towards environmentally-friendly gas turbine engines imposes strict design constraints on combustion chambers to minimise harmful pollutant emission. Measures employed to counter this issue… (more)

Subjects/Keywords: Combustion; Combustion Instability; CFD; Annular Combustor; Oscillatory Behaviour

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

APA (6th Edition):

Valreau, A. S. L. (2019). Computational fluid dynamics investigation of oscillatory behaviour in annular combustors. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/292285 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774780

Chicago Manual of Style (16th Edition):

Valreau, Audrey Sophie Lisa. “Computational fluid dynamics investigation of oscillatory behaviour in annular combustors.” 2019. Doctoral Dissertation, University of Cambridge. Accessed December 15, 2019. https://www.repository.cam.ac.uk/handle/1810/292285 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774780.

MLA Handbook (7th Edition):

Valreau, Audrey Sophie Lisa. “Computational fluid dynamics investigation of oscillatory behaviour in annular combustors.” 2019. Web. 15 Dec 2019.

Vancouver:

Valreau ASL. Computational fluid dynamics investigation of oscillatory behaviour in annular combustors. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2019 Dec 15]. Available from: https://www.repository.cam.ac.uk/handle/1810/292285 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774780.

Council of Science Editors:

Valreau ASL. Computational fluid dynamics investigation of oscillatory behaviour in annular combustors. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/292285 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774780


Loughborough University

29. Melia, Thomas. Heat transfer characteristics of pulse combustors for gas turbine engines.

Degree: PhD, 2012, Loughborough University

 Conventional gas turbine combustors operate with a designed drop in pressure over the length of the device. This is desired in order to encourage mixing… (more)

Subjects/Keywords: 629.134; Pulse combustor; Heat transfer; Jet engines; Pressure gain combustion

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

APA (6th Edition):

Melia, T. (2012). Heat transfer characteristics of pulse combustors for gas turbine engines. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/10278

Chicago Manual of Style (16th Edition):

Melia, Thomas. “Heat transfer characteristics of pulse combustors for gas turbine engines.” 2012. Doctoral Dissertation, Loughborough University. Accessed December 15, 2019. http://hdl.handle.net/2134/10278.

MLA Handbook (7th Edition):

Melia, Thomas. “Heat transfer characteristics of pulse combustors for gas turbine engines.” 2012. Web. 15 Dec 2019.

Vancouver:

Melia T. Heat transfer characteristics of pulse combustors for gas turbine engines. [Internet] [Doctoral dissertation]. Loughborough University; 2012. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/2134/10278.

Council of Science Editors:

Melia T. Heat transfer characteristics of pulse combustors for gas turbine engines. [Doctoral Dissertation]. Loughborough University; 2012. Available from: http://hdl.handle.net/2134/10278


Loughborough University

30. Martin, Damian. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.

Degree: PhD, 2013, Loughborough University

 Full-coverage or effusion cooling is commonly used in the thermal management of gas turbine combustion systems. The combustor environment is characterised by highly turbulent free-stream… (more)

Subjects/Keywords: 621.43; Heat transfer; Film cooling; Combustor; Turbulence; Effusion

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

APA (6th Edition):

Martin, D. (2013). Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/14725

Chicago Manual of Style (16th Edition):

Martin, Damian. “Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.” 2013. Doctoral Dissertation, Loughborough University. Accessed December 15, 2019. http://hdl.handle.net/2134/14725.

MLA Handbook (7th Edition):

Martin, Damian. “Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.” 2013. Web. 15 Dec 2019.

Vancouver:

Martin D. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/2134/14725.

Council of Science Editors:

Martin D. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. [Doctoral Dissertation]. Loughborough University; 2013. Available from: http://hdl.handle.net/2134/14725

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