Advanced search options

Advanced Search Options 🞨

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

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(COMBUSTION CHAMBERS GAS TURBINES ). Showing records 1 – 30 of 16062 total matches.

[1] [2] [3] [4] [5] … [536]

Search Limiters

Last 2 Years | English Only

Degrees

Languages

Country

▼ Search Limiters


Ryerson University

1. Larson, Levon. Numerical simulation of liquid fuel prechamber ignition.

Degree: 2014, Ryerson University

 A Computational Fluid Dynamics (CFD) model was built that simulates the transient, compressible, reacting, multi-phase environment that exists within a reciprocating engine's combustion chamber(s). ANSYS… (more)

Subjects/Keywords: Gas turbines  – Combustion chambers; Gas turbines  – Combustion

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Larson, L. (2014). Numerical simulation of liquid fuel prechamber ignition. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A3076

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):

Larson, Levon. “Numerical simulation of liquid fuel prechamber ignition.” 2014. Thesis, Ryerson University. Accessed January 17, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A3076.

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

MLA Handbook (7th Edition):

Larson, Levon. “Numerical simulation of liquid fuel prechamber ignition.” 2014. Web. 17 Jan 2020.

Vancouver:

Larson L. Numerical simulation of liquid fuel prechamber ignition. [Internet] [Thesis]. Ryerson University; 2014. [cited 2020 Jan 17]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3076.

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

Council of Science Editors:

Larson L. Numerical simulation of liquid fuel prechamber ignition. [Thesis]. Ryerson University; 2014. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3076

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


Indian Institute of Science

2. Ashirvadam, Kampa. Combustion Instability Screech In Gas Turbine Afterburner.

Degree: 2007, Indian Institute of Science

Gas turbine reheat thrust augmenters known as afterburners are used to provide additional thrust during emergencies, take off, combat, and in supersonic flight of high-performance… (more)

Subjects/Keywords: Gas Turbine; Combustion; Gas Turbines - Combustion; Gas Turbine Afterburners; Aircraft Gas Turbines - Combustion; Gas Turbines - Combustion Chambers; Gas Turbine Afterburners - Combustion Instabiltiy; Heat Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ashirvadam, K. (2007). Combustion Instability Screech In Gas Turbine Afterburner. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/581

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):

Ashirvadam, Kampa. “Combustion Instability Screech In Gas Turbine Afterburner.” 2007. Thesis, Indian Institute of Science. Accessed January 17, 2020. http://hdl.handle.net/2005/581.

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

MLA Handbook (7th Edition):

Ashirvadam, Kampa. “Combustion Instability Screech In Gas Turbine Afterburner.” 2007. Web. 17 Jan 2020.

Vancouver:

Ashirvadam K. Combustion Instability Screech In Gas Turbine Afterburner. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/2005/581.

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

Council of Science Editors:

Ashirvadam K. Combustion Instability Screech In Gas Turbine Afterburner. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/581

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


University of Florida

3. Schulze, Kurt Donald. Unified Design Methodology Based on Second Damkohler Number for Colorless Distributed Combustion and Conventional Flame Regimes.

Degree: PhD, Mechanical Engineering - Mechanical and Aerospace Engineering, 2014, University of Florida

 Colorless distributed combustion (CDC) has been of interest due to its inherent low emissions and fuel flexibility, particularity in gas turbine applications.  In the literature,… (more)

Subjects/Keywords: Analyzers; Combustion; Combustion chambers; Combustion efficiency; Combustion temperature; Diluents; Flames; Gas turbines; Inlet temperature; Pollutant emissions; colorless  – combustion  – damkohler  – distributed  – flameless  – gas  – low  – nox  – second  – turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Schulze, K. D. (2014). Unified Design Methodology Based on Second Damkohler Number for Colorless Distributed Combustion and Conventional Flame Regimes. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0046438

Chicago Manual of Style (16th Edition):

Schulze, Kurt Donald. “Unified Design Methodology Based on Second Damkohler Number for Colorless Distributed Combustion and Conventional Flame Regimes.” 2014. Doctoral Dissertation, University of Florida. Accessed January 17, 2020. http://ufdc.ufl.edu/UFE0046438.

MLA Handbook (7th Edition):

Schulze, Kurt Donald. “Unified Design Methodology Based on Second Damkohler Number for Colorless Distributed Combustion and Conventional Flame Regimes.” 2014. Web. 17 Jan 2020.

Vancouver:

Schulze KD. Unified Design Methodology Based on Second Damkohler Number for Colorless Distributed Combustion and Conventional Flame Regimes. [Internet] [Doctoral dissertation]. University of Florida; 2014. [cited 2020 Jan 17]. Available from: http://ufdc.ufl.edu/UFE0046438.

Council of Science Editors:

Schulze KD. Unified Design Methodology Based on Second Damkohler Number for Colorless Distributed Combustion and Conventional Flame Regimes. [Doctoral Dissertation]. University of Florida; 2014. Available from: http://ufdc.ufl.edu/UFE0046438


University of Cambridge

4. Quaglia, Carlo Filippo. A method for the numerical analysis of combustion instabilities with an application to afterburner screech.

Degree: PhD, 2015, University of Cambridge

 This work concerns the prediction of potentially damaging thermoacoustic oscillations in gas turbine combustion systems by computational means. A framework is laid out to predict… (more)

Subjects/Keywords: 621.43; Gas-turbines – Combustion; Afterburners

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Quaglia, C. F. (2015). A method for the numerical analysis of combustion instabilities with an application to afterburner screech. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/264444 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.708938

Chicago Manual of Style (16th Edition):

Quaglia, Carlo Filippo. “A method for the numerical analysis of combustion instabilities with an application to afterburner screech.” 2015. Doctoral Dissertation, University of Cambridge. Accessed January 17, 2020. https://www.repository.cam.ac.uk/handle/1810/264444 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.708938.

MLA Handbook (7th Edition):

Quaglia, Carlo Filippo. “A method for the numerical analysis of combustion instabilities with an application to afterburner screech.” 2015. Web. 17 Jan 2020.

Vancouver:

Quaglia CF. A method for the numerical analysis of combustion instabilities with an application to afterburner screech. [Internet] [Doctoral dissertation]. University of Cambridge; 2015. [cited 2020 Jan 17]. Available from: https://www.repository.cam.ac.uk/handle/1810/264444 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.708938.

Council of Science Editors:

Quaglia CF. A method for the numerical analysis of combustion instabilities with an application to afterburner screech. [Doctoral Dissertation]. University of Cambridge; 2015. Available from: https://www.repository.cam.ac.uk/handle/1810/264444 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.708938

5. Sjölander, Johan. Prediction of ignition limits with respect to fuel fraction of inert gases. : Evaluation of cost effective CFD-method using cold flow simulations.

Degree: Applied Physics and Electronics, 2015, Umeå University

  Improving fuel flexibility for gas turbines is one advantageous property on the market. It may lead to increased feasibility by potential customers and thereby… (more)

Subjects/Keywords: Combustion; gas turbines; CFD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sjölander, J. (2015). Prediction of ignition limits with respect to fuel fraction of inert gases. : Evaluation of cost effective CFD-method using cold flow simulations. (Thesis). Umeå University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-109094

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):

Sjölander, Johan. “Prediction of ignition limits with respect to fuel fraction of inert gases. : Evaluation of cost effective CFD-method using cold flow simulations.” 2015. Thesis, Umeå University. Accessed January 17, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-109094.

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

MLA Handbook (7th Edition):

Sjölander, Johan. “Prediction of ignition limits with respect to fuel fraction of inert gases. : Evaluation of cost effective CFD-method using cold flow simulations.” 2015. Web. 17 Jan 2020.

Vancouver:

Sjölander J. Prediction of ignition limits with respect to fuel fraction of inert gases. : Evaluation of cost effective CFD-method using cold flow simulations. [Internet] [Thesis]. Umeå University; 2015. [cited 2020 Jan 17]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-109094.

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

Council of Science Editors:

Sjölander J. Prediction of ignition limits with respect to fuel fraction of inert gases. : Evaluation of cost effective CFD-method using cold flow simulations. [Thesis]. Umeå University; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-109094

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


University of Oklahoma

6. Wicksall, Donald M. A study of lean premixed swirl-stabilized combustion of gaseous alternative fuels.

Degree: PhD, School of Aerospace and Mechanical Engineering, 2004, University of Oklahoma

 The effects of utilizing gaseous fuels with different compositions was studied for a lean premixed swirl stabilized burner typical of those used in land-based gas(more)

Subjects/Keywords: Flame.; Fuel switching.; Engineering, Mechanical.; Combustion.; Gas-turbines Combustion chambers.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wicksall, D. M. (2004). A study of lean premixed swirl-stabilized combustion of gaseous alternative fuels. (Doctoral Dissertation). University of Oklahoma. Retrieved from http://hdl.handle.net/11244/787

Chicago Manual of Style (16th Edition):

Wicksall, Donald M. “A study of lean premixed swirl-stabilized combustion of gaseous alternative fuels.” 2004. Doctoral Dissertation, University of Oklahoma. Accessed January 17, 2020. http://hdl.handle.net/11244/787.

MLA Handbook (7th Edition):

Wicksall, Donald M. “A study of lean premixed swirl-stabilized combustion of gaseous alternative fuels.” 2004. Web. 17 Jan 2020.

Vancouver:

Wicksall DM. A study of lean premixed swirl-stabilized combustion of gaseous alternative fuels. [Internet] [Doctoral dissertation]. University of Oklahoma; 2004. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/11244/787.

Council of Science Editors:

Wicksall DM. A study of lean premixed swirl-stabilized combustion of gaseous alternative fuels. [Doctoral Dissertation]. University of Oklahoma; 2004. Available from: http://hdl.handle.net/11244/787


Georgia Tech

7. Bobba, Mohan Krishna. Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor.

Degree: PhD, Aerospace Engineering, 2007, Georgia Tech

 A novel combustor design, referred to as the Stagnation Point Reverse-Flow (SPRF) combustor, was recently developed that is able to operate stably at very lean… (more)

Subjects/Keywords: Turbulent; Reverse flow combustor; NOx emissions; Stagnation; Raman scattering; Turbulence; Gas Turbines; Aircraft gas Turbines; Gas Turbines Combustion chambers; Pollution prevention

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bobba, M. K. (2007). Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/26502

Chicago Manual of Style (16th Edition):

Bobba, Mohan Krishna. “Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor.” 2007. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/26502.

MLA Handbook (7th Edition):

Bobba, Mohan Krishna. “Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor.” 2007. Web. 17 Jan 2020.

Vancouver:

Bobba MK. Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor. [Internet] [Doctoral dissertation]. Georgia Tech; 2007. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/26502.

Council of Science Editors:

Bobba MK. Flame stabilization and mixing characteristics in a stagnation point reverse flow combustor. [Doctoral Dissertation]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/26502


Texas A&M University

8. Goehring, Howard Lee. Performance of an industrial type combustor burning simulated fuels of medium BTU content.

Degree: MS, mechanical engineering, 2012, Texas A&M University

Subjects/Keywords: mechanical engineering.; Major mechanical engineering.; Gas-turbines - Combustion chambers.; Fuel - Testing.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Goehring, H. L. (2012). Performance of an industrial type combustor burning simulated fuels of medium BTU content. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1983-THESIS-G594

Chicago Manual of Style (16th Edition):

Goehring, Howard Lee. “Performance of an industrial type combustor burning simulated fuels of medium BTU content.” 2012. Masters Thesis, Texas A&M University. Accessed January 17, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1983-THESIS-G594.

MLA Handbook (7th Edition):

Goehring, Howard Lee. “Performance of an industrial type combustor burning simulated fuels of medium BTU content.” 2012. Web. 17 Jan 2020.

Vancouver:

Goehring HL. Performance of an industrial type combustor burning simulated fuels of medium BTU content. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1983-THESIS-G594.

Council of Science Editors:

Goehring HL. Performance of an industrial type combustor burning simulated fuels of medium BTU content. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1983-THESIS-G594


Georgia Tech

9. Birmaher, Shai. A method for aircraft afterburner combustion without flameholders.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 State of the art aircraft afterburners employ spray bars to inject fuel and flameholders to stabilize the combustion process. Such afterburner designs significantly increase the… (more)

Subjects/Keywords: Flameholders; Afterburner; Partial oxidation; Afterburners; Aircraft gas-turbines Combustion chambers

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Birmaher, S. (2009). A method for aircraft afterburner combustion without flameholders. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28081

Chicago Manual of Style (16th Edition):

Birmaher, Shai. “A method for aircraft afterburner combustion without flameholders.” 2009. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/28081.

MLA Handbook (7th Edition):

Birmaher, Shai. “A method for aircraft afterburner combustion without flameholders.” 2009. Web. 17 Jan 2020.

Vancouver:

Birmaher S. A method for aircraft afterburner combustion without flameholders. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/28081.

Council of Science Editors:

Birmaher S. A method for aircraft afterburner combustion without flameholders. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28081

10. Acharya, Vishal Srinivas. Dynamics of premixed flames in non-axisymmetric disturbance fields.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 With strict environmental regulations, gas turbine emissions have been heavily constrained. This requires operating conditions wherein thermo-acoustic flame instabilities are prevalent. During this process the… (more)

Subjects/Keywords: Level-set; Trasverse acoustics; Helical modes; Swirling flow; Modeling; Combustion Research; Aircraft gas-turbines; Gas-turbines; Aircraft gas-turbines Combustion; Aircraft gas-turbines Combustion chambers; Flames; Combustion

…thereby leading to an unbounded growth in amplitude. Apart from gas turbines [9, 10]… …me direction for my research as well as its applicability in real-world combustion systems… …1.2 1.3 1.4 History and Motivation …..1 Combustion Instability… …Combustion Regimes ...31 Linear and Non-Linear Flame Response 32 Flame Front… …x5D;. ........................................ 2 Figure 2 : Combustion instability feedback… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Acharya, V. S. (2013). Dynamics of premixed flames in non-axisymmetric disturbance fields. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50213

Chicago Manual of Style (16th Edition):

Acharya, Vishal Srinivas. “Dynamics of premixed flames in non-axisymmetric disturbance fields.” 2013. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/50213.

MLA Handbook (7th Edition):

Acharya, Vishal Srinivas. “Dynamics of premixed flames in non-axisymmetric disturbance fields.” 2013. Web. 17 Jan 2020.

Vancouver:

Acharya VS. Dynamics of premixed flames in non-axisymmetric disturbance fields. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/50213.

Council of Science Editors:

Acharya VS. Dynamics of premixed flames in non-axisymmetric disturbance fields. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50213


Luleå University of Technology

11. Bruneflod, Simon. Flow simulations of an axisymmetric two-dimensional 3rd generation DLE burner.

Degree: 2011, Luleå University of Technology

In this thesis a parameter study of a gas turbine burner used in the Siemens Gas Turbine SGT-800 and SGT-700 has been performed using… (more)

Subjects/Keywords: Technology; CFD; Gas Turbines; Combustion; Teknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bruneflod, S. (2011). Flow simulations of an axisymmetric two-dimensional 3rd generation DLE burner. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49904

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):

Bruneflod, Simon. “Flow simulations of an axisymmetric two-dimensional 3rd generation DLE burner.” 2011. Thesis, Luleå University of Technology. Accessed January 17, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49904.

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

MLA Handbook (7th Edition):

Bruneflod, Simon. “Flow simulations of an axisymmetric two-dimensional 3rd generation DLE burner.” 2011. Web. 17 Jan 2020.

Vancouver:

Bruneflod S. Flow simulations of an axisymmetric two-dimensional 3rd generation DLE burner. [Internet] [Thesis]. Luleå University of Technology; 2011. [cited 2020 Jan 17]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49904.

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

Council of Science Editors:

Bruneflod S. Flow simulations of an axisymmetric two-dimensional 3rd generation DLE burner. [Thesis]. Luleå University of Technology; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-49904

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


INP Toulouse

12. Papadogiannis, Dimitrios. Coupled Large Eddy Simulations of combustion chamber-turbine interactions : Simulations aux Grandes Echelles couplées des interactions chambre de combustion-turbine.

Degree: Docteur es, Dynamique des fluides, 2015, INP Toulouse

Les turbines à gaz modernes deviennent de plus en plus compactes, ce qui augmente les interactions entre leurs différents composants. Les interactions chambre de combustion-turbine… (more)

Subjects/Keywords: Turbomachines; Les; Cfd; Turbines; Chambres de combustion; Couplage; Multiphysique; Turbomachinery; Les; Cfd; Turbines; Combustion chambers; Coupling; Myltiphysics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Papadogiannis, D. (2015). Coupled Large Eddy Simulations of combustion chamber-turbine interactions : Simulations aux Grandes Echelles couplées des interactions chambre de combustion-turbine. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2015INPT0049

Chicago Manual of Style (16th Edition):

Papadogiannis, Dimitrios. “Coupled Large Eddy Simulations of combustion chamber-turbine interactions : Simulations aux Grandes Echelles couplées des interactions chambre de combustion-turbine.” 2015. Doctoral Dissertation, INP Toulouse. Accessed January 17, 2020. http://www.theses.fr/2015INPT0049.

MLA Handbook (7th Edition):

Papadogiannis, Dimitrios. “Coupled Large Eddy Simulations of combustion chamber-turbine interactions : Simulations aux Grandes Echelles couplées des interactions chambre de combustion-turbine.” 2015. Web. 17 Jan 2020.

Vancouver:

Papadogiannis D. Coupled Large Eddy Simulations of combustion chamber-turbine interactions : Simulations aux Grandes Echelles couplées des interactions chambre de combustion-turbine. [Internet] [Doctoral dissertation]. INP Toulouse; 2015. [cited 2020 Jan 17]. Available from: http://www.theses.fr/2015INPT0049.

Council of Science Editors:

Papadogiannis D. Coupled Large Eddy Simulations of combustion chamber-turbine interactions : Simulations aux Grandes Echelles couplées des interactions chambre de combustion-turbine. [Doctoral Dissertation]. INP Toulouse; 2015. Available from: http://www.theses.fr/2015INPT0049

13. Crawford, Jackie H., III. Factors that limit control effectiveness in self-excited noise driven combustors.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 A full Strouhal number thermo-acoustic model is purposed for the feedback control of self excited noise driven combustors. The inclusion of time delays in the… (more)

Subjects/Keywords: Combustion instability; Feedback control; Time delay; Laminar premixed flame; Fundamental limitations; Thermo-acoustic model; Aircraft gas-turbines Combustion chambers; Gas-turbines Combustion chambers; Combustion engineering

…instability problem. A key contribution from this collaboration on combustion instabilities in gas… …27 Figure 2-3: Borghi diagram depicting possible combustion regimes. … 33 Figure 2-4… …control of combustion instabilities. The inclusion of time delays in the volumetric heat release… …introduced to the combustion community. These new analysis tools can be used to extend sensitivity… …feedback control. xvii CHAPTER 1 INTRODUCTION Design of gas turbine combustors for propulsion… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Crawford, Jackie H., I. (2012). Factors that limit control effectiveness in self-excited noise driven combustors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43647

Chicago Manual of Style (16th Edition):

Crawford, Jackie H., III. “Factors that limit control effectiveness in self-excited noise driven combustors.” 2012. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/43647.

MLA Handbook (7th Edition):

Crawford, Jackie H., III. “Factors that limit control effectiveness in self-excited noise driven combustors.” 2012. Web. 17 Jan 2020.

Vancouver:

Crawford, Jackie H. I. Factors that limit control effectiveness in self-excited noise driven combustors. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/43647.

Council of Science Editors:

Crawford, Jackie H. I. Factors that limit control effectiveness in self-excited noise driven combustors. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/43647


Northeastern University

14. Ahlholm, Alden William. An investigation of the flame structures and burning speeds of H2/CO/air mixtures.

Degree: MS, Department of Mechanical and Industrial Engineering, 2015, Northeastern University

 With the potential of synthetic gas to be used as a replacement for natural gas in the gas turbine industry the knowledge of its fundamental… (more)

Subjects/Keywords: combustion; thermodynamics; Mechanical Engineering; Flame; Combustion; Synthesis gas; Combustion chambers; Thermodynamics; Carbon monoxide; Hydrogen

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ahlholm, A. W. (2015). An investigation of the flame structures and burning speeds of H2/CO/air mixtures. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/d20128901

Chicago Manual of Style (16th Edition):

Ahlholm, Alden William. “An investigation of the flame structures and burning speeds of H2/CO/air mixtures.” 2015. Masters Thesis, Northeastern University. Accessed January 17, 2020. http://hdl.handle.net/2047/d20128901.

MLA Handbook (7th Edition):

Ahlholm, Alden William. “An investigation of the flame structures and burning speeds of H2/CO/air mixtures.” 2015. Web. 17 Jan 2020.

Vancouver:

Ahlholm AW. An investigation of the flame structures and burning speeds of H2/CO/air mixtures. [Internet] [Masters thesis]. Northeastern University; 2015. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/2047/d20128901.

Council of Science Editors:

Ahlholm AW. An investigation of the flame structures and burning speeds of H2/CO/air mixtures. [Masters Thesis]. Northeastern University; 2015. Available from: http://hdl.handle.net/2047/d20128901

15. Rehayem, Elias. Modélisation des turbomachines : Dérivation d’un modèle phénoménologique de combustion pour la simulation de transitoires sur hélicoptères : Gas Turbine Modelling : Combustion Model Derivation for Rotorcraft Transient Operation.

Degree: Docteur es, Combustion, 2017, Paris Saclay

Ce travail propose l’investigation d’une approche physique 0D/1D modélisant les brûleurs de turbines à gaz, prenant en compte l’évaporation du carburant, la turbulence, la combustion,… (more)

Subjects/Keywords: Turbines à gaz; Combustion,; Simulation système; CFD; Gas turbines; Combustion,; System simulation; CFD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rehayem, E. (2017). Modélisation des turbomachines : Dérivation d’un modèle phénoménologique de combustion pour la simulation de transitoires sur hélicoptères : Gas Turbine Modelling : Combustion Model Derivation for Rotorcraft Transient Operation. (Doctoral Dissertation). Paris Saclay. Retrieved from http://www.theses.fr/2017SACLC056

Chicago Manual of Style (16th Edition):

Rehayem, Elias. “Modélisation des turbomachines : Dérivation d’un modèle phénoménologique de combustion pour la simulation de transitoires sur hélicoptères : Gas Turbine Modelling : Combustion Model Derivation for Rotorcraft Transient Operation.” 2017. Doctoral Dissertation, Paris Saclay. Accessed January 17, 2020. http://www.theses.fr/2017SACLC056.

MLA Handbook (7th Edition):

Rehayem, Elias. “Modélisation des turbomachines : Dérivation d’un modèle phénoménologique de combustion pour la simulation de transitoires sur hélicoptères : Gas Turbine Modelling : Combustion Model Derivation for Rotorcraft Transient Operation.” 2017. Web. 17 Jan 2020.

Vancouver:

Rehayem E. Modélisation des turbomachines : Dérivation d’un modèle phénoménologique de combustion pour la simulation de transitoires sur hélicoptères : Gas Turbine Modelling : Combustion Model Derivation for Rotorcraft Transient Operation. [Internet] [Doctoral dissertation]. Paris Saclay; 2017. [cited 2020 Jan 17]. Available from: http://www.theses.fr/2017SACLC056.

Council of Science Editors:

Rehayem E. Modélisation des turbomachines : Dérivation d’un modèle phénoménologique de combustion pour la simulation de transitoires sur hélicoptères : Gas Turbine Modelling : Combustion Model Derivation for Rotorcraft Transient Operation. [Doctoral Dissertation]. Paris Saclay; 2017. Available from: http://www.theses.fr/2017SACLC056


Michigan State University

16. Hicks, Yolanda R. (Yolanda Royce). Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors.

Degree: PhD, Department of Mechanical Engineering, 1996, Michigan State University

Subjects/Keywords: Combustion engineering; Gas-turbines – Combustion

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hicks, Y. R. (. R. (1996). Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. (Doctoral Dissertation). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:25405

Chicago Manual of Style (16th Edition):

Hicks, Yolanda R (Yolanda Royce). “Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors.” 1996. Doctoral Dissertation, Michigan State University. Accessed January 17, 2020. http://etd.lib.msu.edu/islandora/object/etd:25405.

MLA Handbook (7th Edition):

Hicks, Yolanda R (Yolanda Royce). “Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors.” 1996. Web. 17 Jan 2020.

Vancouver:

Hicks YR(R. Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Internet] [Doctoral dissertation]. Michigan State University; 1996. [cited 2020 Jan 17]. Available from: http://etd.lib.msu.edu/islandora/object/etd:25405.

Council of Science Editors:

Hicks YR(R. Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Doctoral Dissertation]. Michigan State University; 1996. Available from: http://etd.lib.msu.edu/islandora/object/etd:25405


ETH Zürich

17. Baumann, Michael. Stability Analysis of Thermoacoustic Coupling in Damper-Equipped Combustion Chambers Including Nonlinearities.

Degree: 2013, ETH Zürich

Combustion chambers of gas turbines can be viewed as organ pipes in which acoustic pressure and velocity oscillations can be sustained. Thermoacoustic instabilities can occur… (more)

Subjects/Keywords: COMBUSTION CHAMBERS (GAS TURBINES); THERMISCHE SCHWINGUNGSERREGUNG (AKUSTIK); KELVIN-HELMHOLTZ INSTABILITY (FLUID DYNAMICS); DAMPING OF MECHANICAL OSCILLATIONS (ACOUSTICS); KELVIN-HELMHOLTZ INSTABILITÄT (FLUIDDYNAMIK); BRENNKAMMERN (GASTURBINEN); DÄMPFUNG MECHANISCHER SCHWINGUNGEN (AKUSTIK); THERMAL EXCITATION OF VIBRATIONS (ACOUSTICS); info:eu-repo/classification/ddc/620; Engineering & allied operations

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Baumann, M. (2013). Stability Analysis of Thermoacoustic Coupling in Damper-Equipped Combustion Chambers Including Nonlinearities. (Thesis). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/65599

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):

Baumann, Michael. “Stability Analysis of Thermoacoustic Coupling in Damper-Equipped Combustion Chambers Including Nonlinearities.” 2013. Thesis, ETH Zürich. Accessed January 17, 2020. http://hdl.handle.net/20.500.11850/65599.

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

MLA Handbook (7th Edition):

Baumann, Michael. “Stability Analysis of Thermoacoustic Coupling in Damper-Equipped Combustion Chambers Including Nonlinearities.” 2013. Web. 17 Jan 2020.

Vancouver:

Baumann M. Stability Analysis of Thermoacoustic Coupling in Damper-Equipped Combustion Chambers Including Nonlinearities. [Internet] [Thesis]. ETH Zürich; 2013. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/20.500.11850/65599.

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

Council of Science Editors:

Baumann M. Stability Analysis of Thermoacoustic Coupling in Damper-Equipped Combustion Chambers Including Nonlinearities. [Thesis]. ETH Zürich; 2013. Available from: http://hdl.handle.net/20.500.11850/65599

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


Georgia Tech

18. Zhang, Qingguo. Lean blowoff characteristics of swirling H2/CO/CH4 Flames.

Degree: PhD, Aerospace Engineering, 2008, Georgia Tech

 This thesis describes an experimental investigation of lean blowoff for H2/CO/CH4 mixtures in a swirling combustor. This investigation consisted of three thrusts. The first thrust… (more)

Subjects/Keywords: Swirling flames; Lean blowout; Hydrogen; Syngas; Combustion chambers; Gas-turbines; Pollution prevention; Fuel switching; Gasoline, Synthetic

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zhang, Q. (2008). Lean blowoff characteristics of swirling H2/CO/CH4 Flames. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/22641

Chicago Manual of Style (16th Edition):

Zhang, Qingguo. “Lean blowoff characteristics of swirling H2/CO/CH4 Flames.” 2008. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/22641.

MLA Handbook (7th Edition):

Zhang, Qingguo. “Lean blowoff characteristics of swirling H2/CO/CH4 Flames.” 2008. Web. 17 Jan 2020.

Vancouver:

Zhang Q. Lean blowoff characteristics of swirling H2/CO/CH4 Flames. [Internet] [Doctoral dissertation]. Georgia Tech; 2008. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/22641.

Council of Science Editors:

Zhang Q. Lean blowoff characteristics of swirling H2/CO/CH4 Flames. [Doctoral Dissertation]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/22641


Georgia Tech

19. Natarajan, Jayaprakash. Experimental and numerical investigation of laminar flame speeds of H₂/CO/CO₂/N₂ mixtures.

Degree: PhD, Aerospace Engineering, 2008, Georgia Tech

 Coal derived synthetic gas (syngas) fuel is a promising solution for today s increasing demand for clean and reliable power. Syngas fuels are primarily mixtures… (more)

Subjects/Keywords: CO₂ dilution; Preheat; High pressure; Laminar flame speed; Syngas; N₂ dilution; Gasoline, Synthetic; Combustion chambers; Flame; Gas-turbines

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Natarajan, J. (2008). Experimental and numerical investigation of laminar flame speeds of H₂/CO/CO₂/N₂ mixtures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/22685

Chicago Manual of Style (16th Edition):

Natarajan, Jayaprakash. “Experimental and numerical investigation of laminar flame speeds of H₂/CO/CO₂/N₂ mixtures.” 2008. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2020. http://hdl.handle.net/1853/22685.

MLA Handbook (7th Edition):

Natarajan, Jayaprakash. “Experimental and numerical investigation of laminar flame speeds of H₂/CO/CO₂/N₂ mixtures.” 2008. Web. 17 Jan 2020.

Vancouver:

Natarajan J. Experimental and numerical investigation of laminar flame speeds of H₂/CO/CO₂/N₂ mixtures. [Internet] [Doctoral dissertation]. Georgia Tech; 2008. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1853/22685.

Council of Science Editors:

Natarajan J. Experimental and numerical investigation of laminar flame speeds of H₂/CO/CO₂/N₂ mixtures. [Doctoral Dissertation]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/22685


University of Toronto

20. Passarelli, Mitchell Louis. An Investigation of Cross-frequency Interactions in a Gas Turbine Combustor at Flight-relevant Conditions.

Degree: 2019, University of Toronto

This thesis presents the analysis of experimental thermoacoustic data obtained from experiments on an optically accessible aeronautical gas turbine combustor operating at elevated pressures to… (more)

Subjects/Keywords: Combustion; Cross-frequency interactions; Experimental; Gas turbines; Modal decompositions; Thermoacoustics; 0538

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Passarelli, M. L. (2019). An Investigation of Cross-frequency Interactions in a Gas Turbine Combustor at Flight-relevant Conditions. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/98305

Chicago Manual of Style (16th Edition):

Passarelli, Mitchell Louis. “An Investigation of Cross-frequency Interactions in a Gas Turbine Combustor at Flight-relevant Conditions.” 2019. Masters Thesis, University of Toronto. Accessed January 17, 2020. http://hdl.handle.net/1807/98305.

MLA Handbook (7th Edition):

Passarelli, Mitchell Louis. “An Investigation of Cross-frequency Interactions in a Gas Turbine Combustor at Flight-relevant Conditions.” 2019. Web. 17 Jan 2020.

Vancouver:

Passarelli ML. An Investigation of Cross-frequency Interactions in a Gas Turbine Combustor at Flight-relevant Conditions. [Internet] [Masters thesis]. University of Toronto; 2019. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/1807/98305.

Council of Science Editors:

Passarelli ML. An Investigation of Cross-frequency Interactions in a Gas Turbine Combustor at Flight-relevant Conditions. [Masters Thesis]. University of Toronto; 2019. Available from: http://hdl.handle.net/1807/98305


Virginia Tech

21. Farina, Jordan T. Application of Multi-Port Mixing for Passive Suppression of Thermo-Acoustic Instabilities in Premixed Combustors.

Degree: PhD, Mechanical Engineering, 2013, Virginia Tech

 The utilization of lean premixed combustors has become attractive to designers of industrial gas turbines as a means of meeting strict emissions standards without compromising… (more)

Subjects/Keywords: lean premixed; gas turbines; combustion; thermo-acoustic instabilities; passive control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Farina, J. T. (2013). Application of Multi-Port Mixing for Passive Suppression of Thermo-Acoustic Instabilities in Premixed Combustors. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/50533

Chicago Manual of Style (16th Edition):

Farina, Jordan T. “Application of Multi-Port Mixing for Passive Suppression of Thermo-Acoustic Instabilities in Premixed Combustors.” 2013. Doctoral Dissertation, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/50533.

MLA Handbook (7th Edition):

Farina, Jordan T. “Application of Multi-Port Mixing for Passive Suppression of Thermo-Acoustic Instabilities in Premixed Combustors.” 2013. Web. 17 Jan 2020.

Vancouver:

Farina JT. Application of Multi-Port Mixing for Passive Suppression of Thermo-Acoustic Instabilities in Premixed Combustors. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/50533.

Council of Science Editors:

Farina JT. Application of Multi-Port Mixing for Passive Suppression of Thermo-Acoustic Instabilities in Premixed Combustors. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/50533


Virginia Tech

22. Barringer, Michael David. Design and Benchmarking of a Combustor Simulator Relevant to Gas Turbine Engines.

Degree: MS, Mechanical Engineering, 2001, Virginia Tech

 An experimental facility was designed and benchmarked that could simulate the non-uniformities in the flow and thermal fields exiting real gas-turbine combustors. The design of… (more)

Subjects/Keywords: combustion chamber; gas turbines

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Barringer, M. D. (2001). Design and Benchmarking of a Combustor Simulator Relevant to Gas Turbine Engines. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35519

Chicago Manual of Style (16th Edition):

Barringer, Michael David. “Design and Benchmarking of a Combustor Simulator Relevant to Gas Turbine Engines.” 2001. Masters Thesis, Virginia Tech. Accessed January 17, 2020. http://hdl.handle.net/10919/35519.

MLA Handbook (7th Edition):

Barringer, Michael David. “Design and Benchmarking of a Combustor Simulator Relevant to Gas Turbine Engines.” 2001. Web. 17 Jan 2020.

Vancouver:

Barringer MD. Design and Benchmarking of a Combustor Simulator Relevant to Gas Turbine Engines. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/10919/35519.

Council of Science Editors:

Barringer MD. Design and Benchmarking of a Combustor Simulator Relevant to Gas Turbine Engines. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/35519


University of New South Wales

23. Ahn, Thomas Wha Seung. Catalytic combustion of gas turbines: process modelling and kinetic study of iso-octane oxidation.

Degree: Chemical Engineering and Industrial Chemistry :, 1983, University of New South Wales

Subjects/Keywords: Gas-turbines; Combustion of gas-turbines; Thesis Digitisation Program

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ahn, T. W. S. (1983). Catalytic combustion of gas turbines: process modelling and kinetic study of iso-octane oxidation. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/55832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:39499/SOURCE01?view=true

Chicago Manual of Style (16th Edition):

Ahn, Thomas Wha Seung. “Catalytic combustion of gas turbines: process modelling and kinetic study of iso-octane oxidation.” 1983. Doctoral Dissertation, University of New South Wales. Accessed January 17, 2020. http://handle.unsw.edu.au/1959.4/55832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:39499/SOURCE01?view=true.

MLA Handbook (7th Edition):

Ahn, Thomas Wha Seung. “Catalytic combustion of gas turbines: process modelling and kinetic study of iso-octane oxidation.” 1983. Web. 17 Jan 2020.

Vancouver:

Ahn TWS. Catalytic combustion of gas turbines: process modelling and kinetic study of iso-octane oxidation. [Internet] [Doctoral dissertation]. University of New South Wales; 1983. [cited 2020 Jan 17]. Available from: http://handle.unsw.edu.au/1959.4/55832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:39499/SOURCE01?view=true.

Council of Science Editors:

Ahn TWS. Catalytic combustion of gas turbines: process modelling and kinetic study of iso-octane oxidation. [Doctoral Dissertation]. University of New South Wales; 1983. Available from: http://handle.unsw.edu.au/1959.4/55832 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:39499/SOURCE01?view=true


INP Toulouse

24. Felden, Anne. Development of Analytically Reduced Chemistries (ARC) and applications in Large Eddy Simulations (LES) of turbulent combustion : Développement de Chimies Analytiquement Réduites (CAR) et applications à la Simulation aux Grandes Échelles (SGE) de la combustion turbulente.

Degree: Docteur es, Dynamique des fluides, 2017, INP Toulouse

L'impact environnemental du trafic aérien fait maintenant l'objet d'une réglementation qui tend à se sévériser. Dans ce contexte, les industriels misent sur l'amélioration des technologies… (more)

Subjects/Keywords: Chimie de la combustion; Chimies réduites; Combustion turbulente; Turbines à gaz; Simulations aux Grandes Échelles; Prédiction des polluants; Combustion chemistry; Reduced chemistry; Turbulent combustion; Gas turbines; Large Eddy Simulations; Pollutants

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Felden, A. (2017). Development of Analytically Reduced Chemistries (ARC) and applications in Large Eddy Simulations (LES) of turbulent combustion : Développement de Chimies Analytiquement Réduites (CAR) et applications à la Simulation aux Grandes Échelles (SGE) de la combustion turbulente. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2017INPT0063

Chicago Manual of Style (16th Edition):

Felden, Anne. “Development of Analytically Reduced Chemistries (ARC) and applications in Large Eddy Simulations (LES) of turbulent combustion : Développement de Chimies Analytiquement Réduites (CAR) et applications à la Simulation aux Grandes Échelles (SGE) de la combustion turbulente.” 2017. Doctoral Dissertation, INP Toulouse. Accessed January 17, 2020. http://www.theses.fr/2017INPT0063.

MLA Handbook (7th Edition):

Felden, Anne. “Development of Analytically Reduced Chemistries (ARC) and applications in Large Eddy Simulations (LES) of turbulent combustion : Développement de Chimies Analytiquement Réduites (CAR) et applications à la Simulation aux Grandes Échelles (SGE) de la combustion turbulente.” 2017. Web. 17 Jan 2020.

Vancouver:

Felden A. Development of Analytically Reduced Chemistries (ARC) and applications in Large Eddy Simulations (LES) of turbulent combustion : Développement de Chimies Analytiquement Réduites (CAR) et applications à la Simulation aux Grandes Échelles (SGE) de la combustion turbulente. [Internet] [Doctoral dissertation]. INP Toulouse; 2017. [cited 2020 Jan 17]. Available from: http://www.theses.fr/2017INPT0063.

Council of Science Editors:

Felden A. Development of Analytically Reduced Chemistries (ARC) and applications in Large Eddy Simulations (LES) of turbulent combustion : Développement de Chimies Analytiquement Réduites (CAR) et applications à la Simulation aux Grandes Échelles (SGE) de la combustion turbulente. [Doctoral Dissertation]. INP Toulouse; 2017. Available from: http://www.theses.fr/2017INPT0063


ETH Zürich

25. Büche, Dirk. Multi-objective evolutionary optimization of gas turbine components.

Degree: 2003, ETH Zürich

Subjects/Keywords: DESIGN + GESTALTUNG + FORMGEBUNG; PRODUKTENTWICKLUNG; PARETO-OPTIMUM; TURBOMASCHINENSCHAUFELN (TURBOMASCHINEN); MACHINE COMPONENTS (MECHANICAL ENGINEERING); STRUCTURAL OPTIMIZATION (ENGINEERING); BRENNKAMMERN (GASTURBINEN); PARETO OPTIMALITY; NEW PRODUCT DEVELOPMENT; COMBUSTION CHAMBERS (GAS TURBINES); STRUKTUROPTIMIERUNG (INGENIEURWESEN); TURBOMACHINE BLADES (TURBOMACHINES); DESIGN + PRESENTATION; GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); MASCHINENELEMENTE (MASCHINENBAU); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; Engineering & allied operations

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Büche, D. (2003). Multi-objective evolutionary optimization of gas turbine components. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/72761

Chicago Manual of Style (16th Edition):

Büche, Dirk. “Multi-objective evolutionary optimization of gas turbine components.” 2003. Doctoral Dissertation, ETH Zürich. Accessed January 17, 2020. http://hdl.handle.net/20.500.11850/72761.

MLA Handbook (7th Edition):

Büche, Dirk. “Multi-objective evolutionary optimization of gas turbine components.” 2003. Web. 17 Jan 2020.

Vancouver:

Büche D. Multi-objective evolutionary optimization of gas turbine components. [Internet] [Doctoral dissertation]. ETH Zürich; 2003. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/20.500.11850/72761.

Council of Science Editors:

Büche D. Multi-objective evolutionary optimization of gas turbine components. [Doctoral Dissertation]. ETH Zürich; 2003. Available from: http://hdl.handle.net/20.500.11850/72761


ETH Zürich

26. Becerra Sagredo, Julián Tercero. High-order semi-Lagrangian numerical method for large-eddy simulations of reacting flows.

Degree: 2007, ETH Zürich

Subjects/Keywords: GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); BRENNKAMMERN (GASTURBINEN); FLAMMENCHEMIE; REAKTIVE STRÖMUNG (CHEMISCHE VERFAHRENSTECHNIK); METHAN (BRENNSTOFFTECHNOLOGIE); LARGE-EDDY-SIMULATION (FLUIDDYNAMIK); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); COMBUSTION CHAMBERS (GAS TURBINES); FLAME CHEMISTRY; REACTIVE FLOW (CHEMICAL ENGINEERING); METHANE (FUEL TECHNOLOGY); LARGE-EDDY SIMULATION (FLUID DYNAMICS); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Becerra Sagredo, J. T. (2007). High-order semi-Lagrangian numerical method for large-eddy simulations of reacting flows. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/150248

Chicago Manual of Style (16th Edition):

Becerra Sagredo, Julián Tercero. “High-order semi-Lagrangian numerical method for large-eddy simulations of reacting flows.” 2007. Doctoral Dissertation, ETH Zürich. Accessed January 17, 2020. http://hdl.handle.net/20.500.11850/150248.

MLA Handbook (7th Edition):

Becerra Sagredo, Julián Tercero. “High-order semi-Lagrangian numerical method for large-eddy simulations of reacting flows.” 2007. Web. 17 Jan 2020.

Vancouver:

Becerra Sagredo JT. High-order semi-Lagrangian numerical method for large-eddy simulations of reacting flows. [Internet] [Doctoral dissertation]. ETH Zürich; 2007. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/20.500.11850/150248.

Council of Science Editors:

Becerra Sagredo JT. High-order semi-Lagrangian numerical method for large-eddy simulations of reacting flows. [Doctoral Dissertation]. ETH Zürich; 2007. Available from: http://hdl.handle.net/20.500.11850/150248


Northeastern University

27. Nongsaeng, Amornrat. Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes.

Degree: MS, Department of Mechanical and Industrial Engineering, 2009, Northeastern University

 Trailing edge cooling cavities in modern gas turbine airfoils play an important role in maintaining the trailing edge temperature at levels consistent with airfoil design… (more)

Subjects/Keywords: Cooling of Turbine Blades in Gas Turbines; Cross Flow Effects; Trailing Edge Cooling; Turbine Blade Cooling; Aerofoils – Design and construction; Trailing edges (Aerodynamics) – Cooling; Gas-turbines – Combustion chambers; Mechanical Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Nongsaeng, A. (2009). Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/d20000061

Chicago Manual of Style (16th Edition):

Nongsaeng, Amornrat. “Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes.” 2009. Masters Thesis, Northeastern University. Accessed January 17, 2020. http://hdl.handle.net/2047/d20000061.

MLA Handbook (7th Edition):

Nongsaeng, Amornrat. “Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes.” 2009. Web. 17 Jan 2020.

Vancouver:

Nongsaeng A. Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes. [Internet] [Masters thesis]. Northeastern University; 2009. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/2047/d20000061.

Council of Science Editors:

Nongsaeng A. Experimental impingement heat transfer in a smooth channel with cross over jets and bleed holes. [Masters Thesis]. Northeastern University; 2009. Available from: http://hdl.handle.net/2047/d20000061


Northeastern University

28. Elia, Mimmo. Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of N-heptane and gas to liquid fuel.

Degree: PhD, Department of Mechanical and Industrial Engineering, 2016, Northeastern University

 Research studies into understanding the fundamental thermodynamic properties of Syngas are extremely relevant in engineering combustion modelling for stationary turbine based power plants and for… (more)

Subjects/Keywords: auto-ignition; GTL; laminar burning speed; mass burning speed; S8; syngas; Synthesis gas; Combustion; Combustion; Combustion chambers; Gas as fuel; Flame; Chemical kinetics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Elia, M. (2016). Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of N-heptane and gas to liquid fuel. (Doctoral Dissertation). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20211318

Chicago Manual of Style (16th Edition):

Elia, Mimmo. “Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of N-heptane and gas to liquid fuel.” 2016. Doctoral Dissertation, Northeastern University. Accessed January 17, 2020. http://hdl.handle.net/2047/D20211318.

MLA Handbook (7th Edition):

Elia, Mimmo. “Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of N-heptane and gas to liquid fuel.” 2016. Web. 17 Jan 2020.

Vancouver:

Elia M. Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of N-heptane and gas to liquid fuel. [Internet] [Doctoral dissertation]. Northeastern University; 2016. [cited 2020 Jan 17]. Available from: http://hdl.handle.net/2047/D20211318.

Council of Science Editors:

Elia M. Measurement apparatus and modelling of laminar burning speed and mass burning rate of syngas and onset of auto-ignition of N-heptane and gas to liquid fuel. [Doctoral Dissertation]. Northeastern University; 2016. Available from: http://hdl.handle.net/2047/D20211318

29. Flynt, Guy Austin. Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators.

Degree: 2013, University of Tennessee – Chattanooga

 The effects of rotation and Reynolds number on heat transfer in rotating two-pass square and rectangular channels with smooth walls and walls with 45 degree… (more)

Subjects/Keywords: Gas-Turbines

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Flynt, G. A. (2013). Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators. (Masters Thesis). University of Tennessee – Chattanooga. Retrieved from https://scholar.utc.edu/theses/265

Chicago Manual of Style (16th Edition):

Flynt, Guy Austin. “Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators.” 2013. Masters Thesis, University of Tennessee – Chattanooga. Accessed January 17, 2020. https://scholar.utc.edu/theses/265.

MLA Handbook (7th Edition):

Flynt, Guy Austin. “Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators.” 2013. Web. 17 Jan 2020.

Vancouver:

Flynt GA. Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators. [Internet] [Masters thesis]. University of Tennessee – Chattanooga; 2013. [cited 2020 Jan 17]. Available from: https://scholar.utc.edu/theses/265.

Council of Science Editors:

Flynt GA. Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators. [Masters Thesis]. University of Tennessee – Chattanooga; 2013. Available from: https://scholar.utc.edu/theses/265


Cranfield University

30. Anosike, Nnamdi Benedict. Technoeconomic evaluation of flared natural gas reduction and energy recovery using gas-to-wire scheme.

Degree: PhD, 2013, Cranfield University

 Most mature oil reservoirs or fields tend to perform below expectations, owing to high level of associated gas production. This creates a sub-optimal performance of… (more)

Subjects/Keywords: 621.43; small-scaled flared associated gas utilization; combustion gas turbines; onsite power generation; associated gas production decline; power plant operations alternatives; gas turbines unit divestment; makeup –fuel; uncertainty analysis

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Anosike, N. B. (2013). Technoeconomic evaluation of flared natural gas reduction and energy recovery using gas-to-wire scheme. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/8625 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.613517

Chicago Manual of Style (16th Edition):

Anosike, Nnamdi Benedict. “Technoeconomic evaluation of flared natural gas reduction and energy recovery using gas-to-wire scheme.” 2013. Doctoral Dissertation, Cranfield University. Accessed January 17, 2020. http://dspace.lib.cranfield.ac.uk/handle/1826/8625 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.613517.

MLA Handbook (7th Edition):

Anosike, Nnamdi Benedict. “Technoeconomic evaluation of flared natural gas reduction and energy recovery using gas-to-wire scheme.” 2013. Web. 17 Jan 2020.

Vancouver:

Anosike NB. Technoeconomic evaluation of flared natural gas reduction and energy recovery using gas-to-wire scheme. [Internet] [Doctoral dissertation]. Cranfield University; 2013. [cited 2020 Jan 17]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8625 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.613517.

Council of Science Editors:

Anosike NB. Technoeconomic evaluation of flared natural gas reduction and energy recovery using gas-to-wire scheme. [Doctoral Dissertation]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8625 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.613517

[1] [2] [3] [4] [5] … [536]

.