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You searched for subject:(GAS TURBINES COMBUSTION TURBINES INTERNAL COMBUSTION ENGINES ). Showing records 1 – 30 of 22988 total matches.

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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

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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 19, 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. 19 Jan 2020.

Vancouver:

Larson L. Numerical simulation of liquid fuel prechamber ignition. [Internet] [Thesis]. Ryerson University; 2014. [cited 2020 Jan 19]. 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


University of Cambridge

2. 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

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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 19, 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. 19 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 19]. 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

3. 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

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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 19, 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. 19 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 19]. 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


Northeastern University

4. Yang, Fan. Experimental investigation of heat transfer performance in turbine airfoil cooling channels roughened with wrap-around ribs.

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

Gas turbine is a type of internal combustion engine. Cooling of turbine airfoils is one useful way to obtain higher thermal efficiency and lower fuel… (more)

Subjects/Keywords: cooling channels; turbine airfoil; wrap-around ribs; Gas-turbines; Thermodynamics; Heat; Transmission; Aerofoils; Cooling; Internal combustion engines

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APA (6th Edition):

Yang, F. (2016). Experimental investigation of heat transfer performance in turbine airfoil cooling channels roughened with wrap-around ribs. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20213264

Chicago Manual of Style (16th Edition):

Yang, Fan. “Experimental investigation of heat transfer performance in turbine airfoil cooling channels roughened with wrap-around ribs.” 2016. Masters Thesis, Northeastern University. Accessed January 19, 2020. http://hdl.handle.net/2047/D20213264.

MLA Handbook (7th Edition):

Yang, Fan. “Experimental investigation of heat transfer performance in turbine airfoil cooling channels roughened with wrap-around ribs.” 2016. Web. 19 Jan 2020.

Vancouver:

Yang F. Experimental investigation of heat transfer performance in turbine airfoil cooling channels roughened with wrap-around ribs. [Internet] [Masters thesis]. Northeastern University; 2016. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/2047/D20213264.

Council of Science Editors:

Yang F. Experimental investigation of heat transfer performance in turbine airfoil cooling channels roughened with wrap-around ribs. [Masters Thesis]. Northeastern University; 2016. Available from: http://hdl.handle.net/2047/D20213264


Texas A&M University

5. Ford, David Bruce. An investigation into the feasibility of an external combustion, steam injected gas turbine.

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

Subjects/Keywords: mechanical engineering.; Major mechanical engineering.; Gas-turbines.; Gas-turbines - Combustion.; Internal combustion engines - Combustion.

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APA (6th Edition):

Ford, D. B. (2012). An investigation into the feasibility of an external combustion, steam injected gas turbine. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-F699

Chicago Manual of Style (16th Edition):

Ford, David Bruce. “An investigation into the feasibility of an external combustion, steam injected gas turbine.” 2012. Masters Thesis, Texas A&M University. Accessed January 19, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-F699.

MLA Handbook (7th Edition):

Ford, David Bruce. “An investigation into the feasibility of an external combustion, steam injected gas turbine.” 2012. Web. 19 Jan 2020.

Vancouver:

Ford DB. An investigation into the feasibility of an external combustion, steam injected gas turbine. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-F699.

Council of Science Editors:

Ford DB. An investigation into the feasibility of an external combustion, steam injected gas turbine. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-F699


Indian Institute of Science

6. 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

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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 19, 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. 19 Jan 2020.

Vancouver:

Ashirvadam K. Combustion Instability Screech In Gas Turbine Afterburner. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2020 Jan 19]. 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


Luleå University of Technology

7. 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

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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 19, 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. 19 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 19]. 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


ETH Zürich

8. Jaggi, Hans. Stationäres Betriebsverhalten von Gasturbinen mit verstellbaren Leitapparaten.

Degree: 1964, ETH Zürich

Subjects/Keywords: GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6th Edition):

Jaggi, H. (1964). Stationäres Betriebsverhalten von Gasturbinen mit verstellbaren Leitapparaten. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/132752

Chicago Manual of Style (16th Edition):

Jaggi, Hans. “Stationäres Betriebsverhalten von Gasturbinen mit verstellbaren Leitapparaten.” 1964. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/132752.

MLA Handbook (7th Edition):

Jaggi, Hans. “Stationäres Betriebsverhalten von Gasturbinen mit verstellbaren Leitapparaten.” 1964. Web. 19 Jan 2020.

Vancouver:

Jaggi H. Stationäres Betriebsverhalten von Gasturbinen mit verstellbaren Leitapparaten. [Internet] [Doctoral dissertation]. ETH Zürich; 1964. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/132752.

Council of Science Editors:

Jaggi H. Stationäres Betriebsverhalten von Gasturbinen mit verstellbaren Leitapparaten. [Doctoral Dissertation]. ETH Zürich; 1964. Available from: http://hdl.handle.net/20.500.11850/132752


ETH Zürich

9. Calder, James Wilson. Compressible potential flow through a thermal turbine.

Degree: 1962, ETH Zürich

Subjects/Keywords: GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); FLUIDDYNAMIK; GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); FLUID DYNAMICS; info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6th Edition):

Calder, J. W. (1962). Compressible potential flow through a thermal turbine. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/131809

Chicago Manual of Style (16th Edition):

Calder, James Wilson. “Compressible potential flow through a thermal turbine.” 1962. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/131809.

MLA Handbook (7th Edition):

Calder, James Wilson. “Compressible potential flow through a thermal turbine.” 1962. Web. 19 Jan 2020.

Vancouver:

Calder JW. Compressible potential flow through a thermal turbine. [Internet] [Doctoral dissertation]. ETH Zürich; 1962. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/131809.

Council of Science Editors:

Calder JW. Compressible potential flow through a thermal turbine. [Doctoral Dissertation]. ETH Zürich; 1962. Available from: http://hdl.handle.net/20.500.11850/131809

10. 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

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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 19, 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. 19 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 19]. 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

11. 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

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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 19, 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. 19 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 19]. 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

12. Oprecht, Ulrich. Regeneratoren für Kleingasturbinen.

Degree: 1957, ETH Zürich

Subjects/Keywords: GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6th Edition):

Oprecht, U. (1957). Regeneratoren für Kleingasturbinen. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/134996

Chicago Manual of Style (16th Edition):

Oprecht, Ulrich. “Regeneratoren für Kleingasturbinen.” 1957. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/134996.

MLA Handbook (7th Edition):

Oprecht, Ulrich. “Regeneratoren für Kleingasturbinen.” 1957. Web. 19 Jan 2020.

Vancouver:

Oprecht U. Regeneratoren für Kleingasturbinen. [Internet] [Doctoral dissertation]. ETH Zürich; 1957. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/134996.

Council of Science Editors:

Oprecht U. Regeneratoren für Kleingasturbinen. [Doctoral Dissertation]. ETH Zürich; 1957. Available from: http://hdl.handle.net/20.500.11850/134996


ETH Zürich

13. Nussbaumer, Ernst. Analyse des Betriebsverhaltens von Gasturbinen mit der Analogrechenmaschine.

Degree: 1963, ETH Zürich

Subjects/Keywords: ANALOGCOMPUTER (COMPUTERSYSTEME); GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); ANALOG COMPUTERS (COMPUTER SYSTEMS); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6th Edition):

Nussbaumer, E. (1963). Analyse des Betriebsverhaltens von Gasturbinen mit der Analogrechenmaschine. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/135387

Chicago Manual of Style (16th Edition):

Nussbaumer, Ernst. “Analyse des Betriebsverhaltens von Gasturbinen mit der Analogrechenmaschine.” 1963. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/135387.

MLA Handbook (7th Edition):

Nussbaumer, Ernst. “Analyse des Betriebsverhaltens von Gasturbinen mit der Analogrechenmaschine.” 1963. Web. 19 Jan 2020.

Vancouver:

Nussbaumer E. Analyse des Betriebsverhaltens von Gasturbinen mit der Analogrechenmaschine. [Internet] [Doctoral dissertation]. ETH Zürich; 1963. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/135387.

Council of Science Editors:

Nussbaumer E. Analyse des Betriebsverhaltens von Gasturbinen mit der Analogrechenmaschine. [Doctoral Dissertation]. ETH Zürich; 1963. Available from: http://hdl.handle.net/20.500.11850/135387


University of Miami

14. Chen, Shanghua. An Investigation of The New High Efficiency 3 Cylinders Internal Combustion Engine.

Degree: MS, Mechanical Engineering (Engineering), 2016, University of Miami

  The thesis is an initial study of a unique 3 cylinder geometry for naturally aspired piston type internal combustion engines (ICE). The advantages of… (more)

Subjects/Keywords: internal combustion engines

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APA (6th Edition):

Chen, S. (2016). An Investigation of The New High Efficiency 3 Cylinders Internal Combustion Engine. (Thesis). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_theses/601

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, Shanghua. “An Investigation of The New High Efficiency 3 Cylinders Internal Combustion Engine.” 2016. Thesis, University of Miami. Accessed January 19, 2020. https://scholarlyrepository.miami.edu/oa_theses/601.

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

MLA Handbook (7th Edition):

Chen, Shanghua. “An Investigation of The New High Efficiency 3 Cylinders Internal Combustion Engine.” 2016. Web. 19 Jan 2020.

Vancouver:

Chen S. An Investigation of The New High Efficiency 3 Cylinders Internal Combustion Engine. [Internet] [Thesis]. University of Miami; 2016. [cited 2020 Jan 19]. Available from: https://scholarlyrepository.miami.edu/oa_theses/601.

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

Council of Science Editors:

Chen S. An Investigation of The New High Efficiency 3 Cylinders Internal Combustion Engine. [Thesis]. University of Miami; 2016. Available from: https://scholarlyrepository.miami.edu/oa_theses/601

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


ETH Zürich

15. Mills, Robert Glenn. A thermodynamic analysis of the combined steam turbine-gas turbine power cycle.

Degree: 1957, ETH Zürich

Subjects/Keywords: GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); DAMPFTURBINEN (WÄRMEKRAFTMASCHINEN); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); STEAM TURBINES (HEAT ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6th Edition):

Mills, R. G. (1957). A thermodynamic analysis of the combined steam turbine-gas turbine power cycle. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/133487

Chicago Manual of Style (16th Edition):

Mills, Robert Glenn. “A thermodynamic analysis of the combined steam turbine-gas turbine power cycle.” 1957. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/133487.

MLA Handbook (7th Edition):

Mills, Robert Glenn. “A thermodynamic analysis of the combined steam turbine-gas turbine power cycle.” 1957. Web. 19 Jan 2020.

Vancouver:

Mills RG. A thermodynamic analysis of the combined steam turbine-gas turbine power cycle. [Internet] [Doctoral dissertation]. ETH Zürich; 1957. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/133487.

Council of Science Editors:

Mills RG. A thermodynamic analysis of the combined steam turbine-gas turbine power cycle. [Doctoral Dissertation]. ETH Zürich; 1957. Available from: http://hdl.handle.net/20.500.11850/133487


ETH Zürich

16. Traupel, Walter. Neue allgemeine Theorie der mehrstufigen axialen Turbomaschine.

Degree: 1942, ETH Zürich

Subjects/Keywords: AXIALTURBOMASCHINEN (MASCHINENBAU); DAMPFTURBINEN (WÄRMEKRAFTMASCHINEN); GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); AXIAL TURBOMACHINES (MECHANICAL ENGINEERING); STEAM TURBINES (HEAT ENGINES); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6th Edition):

Traupel, W. (1942). Neue allgemeine Theorie der mehrstufigen axialen Turbomaschine. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/135369

Chicago Manual of Style (16th Edition):

Traupel, Walter. “Neue allgemeine Theorie der mehrstufigen axialen Turbomaschine.” 1942. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/135369.

MLA Handbook (7th Edition):

Traupel, Walter. “Neue allgemeine Theorie der mehrstufigen axialen Turbomaschine.” 1942. Web. 19 Jan 2020.

Vancouver:

Traupel W. Neue allgemeine Theorie der mehrstufigen axialen Turbomaschine. [Internet] [Doctoral dissertation]. ETH Zürich; 1942. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/135369.

Council of Science Editors:

Traupel W. Neue allgemeine Theorie der mehrstufigen axialen Turbomaschine. [Doctoral Dissertation]. ETH Zürich; 1942. Available from: http://hdl.handle.net/20.500.11850/135369


Indian Institute of Science

17. Santhosh, R. Transition and Acoustic Response of Vortex Breakdown Modes in Unconfined Coaxial Swirling Flow and Flame.

Degree: 2015, Indian Institute of Science

 The efficient and enhanced mixing of heat and incoming reactants is achieved in modern gas turbine systems by employing swirling flows. This is realized by… (more)

Subjects/Keywords: Coaxial Isothermal Swirling Jet; Gas Turbines; Internal Combustion Engines; Swirling Flow Jets; Swirling Flow/Flame; Thermo-Acoustic Combustion Instability; Vortex Breakdown; Jets-Fluid Dynamics; Combustion; Co-axial Isothermal Swirling Flow; Vortex Breakdown Modes; Swirling Flame; Isothermal Swirling Flow Field; Isothermal Swirling Co-axial Jet; Co-axial Isothermal Swirling Jet; Isothermal Coaxial Swirling Jet; Mechanical Engineering

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APA (6th Edition):

Santhosh, R. (2015). Transition and Acoustic Response of Vortex Breakdown Modes in Unconfined Coaxial Swirling Flow and Flame. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3856 ; http://etd.iisc.ernet.in/abstracts/4728/G27131-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):

Santhosh, R. “Transition and Acoustic Response of Vortex Breakdown Modes in Unconfined Coaxial Swirling Flow and Flame.” 2015. Thesis, Indian Institute of Science. Accessed January 19, 2020. http://etd.iisc.ernet.in/2005/3856 ; http://etd.iisc.ernet.in/abstracts/4728/G27131-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):

Santhosh, R. “Transition and Acoustic Response of Vortex Breakdown Modes in Unconfined Coaxial Swirling Flow and Flame.” 2015. Web. 19 Jan 2020.

Vancouver:

Santhosh R. Transition and Acoustic Response of Vortex Breakdown Modes in Unconfined Coaxial Swirling Flow and Flame. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2020 Jan 19]. Available from: http://etd.iisc.ernet.in/2005/3856 ; http://etd.iisc.ernet.in/abstracts/4728/G27131-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:

Santhosh R. Transition and Acoustic Response of Vortex Breakdown Modes in Unconfined Coaxial Swirling Flow and Flame. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3856 ; http://etd.iisc.ernet.in/abstracts/4728/G27131-Abs.pdf

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


University of Toronto

18. 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

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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 19, 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. 19 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 19]. 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

19. 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

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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 19, 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. 19 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 19]. 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

20. 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

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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 19, 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. 19 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 19]. 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


INP Toulouse

21. 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

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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 19, 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. 19 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 19]. 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


University of New South Wales

22. 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

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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 19, 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. 19 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 19]. 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


University of Florida

23. 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

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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 19, 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. 19 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 19]. 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


ETH Zürich

24. Vacchieri, Erica. Creep-Fatigue and Small Punch Creep in Gas Turbine Hot Gas Path Materials.

Degree: 2016, ETH Zürich

Subjects/Keywords: GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); ERMÜDUNG, WECHSELFESTIGKEIT (ELASTOMECHANIK); KRIECHEN, KRIECHVERHALTEN (ELASTOMECHANIK); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); FATIGUE RESISTANCE, LOAD-CYCLE STRENGTH (ELASTOMECHANICS); CREEP (ELASTOMECHANICS); info:eu-repo/classification/ddc/620; Engineering & allied operations

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APA (6th Edition):

Vacchieri, E. (2016). Creep-Fatigue and Small Punch Creep in Gas Turbine Hot Gas Path Materials. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/156213

Chicago Manual of Style (16th Edition):

Vacchieri, Erica. “Creep-Fatigue and Small Punch Creep in Gas Turbine Hot Gas Path Materials.” 2016. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/156213.

MLA Handbook (7th Edition):

Vacchieri, Erica. “Creep-Fatigue and Small Punch Creep in Gas Turbine Hot Gas Path Materials.” 2016. Web. 19 Jan 2020.

Vancouver:

Vacchieri E. Creep-Fatigue and Small Punch Creep in Gas Turbine Hot Gas Path Materials. [Internet] [Doctoral dissertation]. ETH Zürich; 2016. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/156213.

Council of Science Editors:

Vacchieri E. Creep-Fatigue and Small Punch Creep in Gas Turbine Hot Gas Path Materials. [Doctoral Dissertation]. ETH Zürich; 2016. Available from: http://hdl.handle.net/20.500.11850/156213


ETH Zürich

25. Basol, Altug M. Turbine Design Optimizations using High Fidelity CFD.

Degree: 2014, ETH Zürich

Subjects/Keywords: COMPUTATIONAL FLUID DYNAMICS (FLUIDMECHANIK); STRUKTUROPTIMIERUNG (INGENIEURWESEN); STRUCTURAL OPTIMIZATION (ENGINEERING); COMPUTATIONAL FLUID DYNAMICS (FLUID MECHANICS); GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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APA (6th Edition):

Basol, A. M. (2014). Turbine Design Optimizations using High Fidelity CFD. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/97455

Chicago Manual of Style (16th Edition):

Basol, Altug M. “Turbine Design Optimizations using High Fidelity CFD.” 2014. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/97455.

MLA Handbook (7th Edition):

Basol, Altug M. “Turbine Design Optimizations using High Fidelity CFD.” 2014. Web. 19 Jan 2020.

Vancouver:

Basol AM. Turbine Design Optimizations using High Fidelity CFD. [Internet] [Doctoral dissertation]. ETH Zürich; 2014. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/97455.

Council of Science Editors:

Basol AM. Turbine Design Optimizations using High Fidelity CFD. [Doctoral Dissertation]. ETH Zürich; 2014. Available from: http://hdl.handle.net/20.500.11850/97455


ETH Zürich

26. McMullen, John Joseph. Wahl und Entwurf einer Gasturbine und Untersuchung ihrer Eignung zum Antrieb eines Frachtschiffes.

Degree: 1950, ETH Zürich

Subjects/Keywords: WASSERFAHRZEUGE UND SCHIFFBAU; GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); WATERCRAFT ENGINEERING AND SHIPBUILDING; GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/620; Engineering & allied operations; Engineering & allied operations

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APA (6th Edition):

McMullen, J. J. (1950). Wahl und Entwurf einer Gasturbine und Untersuchung ihrer Eignung zum Antrieb eines Frachtschiffes. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/137464

Chicago Manual of Style (16th Edition):

McMullen, John Joseph. “Wahl und Entwurf einer Gasturbine und Untersuchung ihrer Eignung zum Antrieb eines Frachtschiffes.” 1950. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/137464.

MLA Handbook (7th Edition):

McMullen, John Joseph. “Wahl und Entwurf einer Gasturbine und Untersuchung ihrer Eignung zum Antrieb eines Frachtschiffes.” 1950. Web. 19 Jan 2020.

Vancouver:

McMullen JJ. Wahl und Entwurf einer Gasturbine und Untersuchung ihrer Eignung zum Antrieb eines Frachtschiffes. [Internet] [Doctoral dissertation]. ETH Zürich; 1950. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/137464.

Council of Science Editors:

McMullen JJ. Wahl und Entwurf einer Gasturbine und Untersuchung ihrer Eignung zum Antrieb eines Frachtschiffes. [Doctoral Dissertation]. ETH Zürich; 1950. Available from: http://hdl.handle.net/20.500.11850/137464


ETH Zürich

27. Lin, Yu-chun. Characteristics of turbulent lean-premixed combustion for hydrogen-rich fuel gases.

Degree: 2014, ETH Zürich

Subjects/Keywords: WASSERSTOFF (BRENNSTOFFTECHNOLOGIE); GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); HYDROGEN (FUEL TECHNOLOGY); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/333.7; Engineering & allied operations; Natural resources, energy and environment

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APA (6th Edition):

Lin, Y. (2014). Characteristics of turbulent lean-premixed combustion for hydrogen-rich fuel gases. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/154708

Chicago Manual of Style (16th Edition):

Lin, Yu-chun. “Characteristics of turbulent lean-premixed combustion for hydrogen-rich fuel gases.” 2014. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/154708.

MLA Handbook (7th Edition):

Lin, Yu-chun. “Characteristics of turbulent lean-premixed combustion for hydrogen-rich fuel gases.” 2014. Web. 19 Jan 2020.

Vancouver:

Lin Y. Characteristics of turbulent lean-premixed combustion for hydrogen-rich fuel gases. [Internet] [Doctoral dissertation]. ETH Zürich; 2014. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/154708.

Council of Science Editors:

Lin Y. Characteristics of turbulent lean-premixed combustion for hydrogen-rich fuel gases. [Doctoral Dissertation]. ETH Zürich; 2014. Available from: http://hdl.handle.net/20.500.11850/154708


ETH Zürich

28. Fritsche, Daniel. Origin and control of thermoacoustic instabilities in lean premixed gas turbine combustion.

Degree: 2005, ETH Zürich

 Modern gas turbines use lean premixedcombustion to achieve the best compromise between pollutant emissions and efficiency. This type of combustion increases the flame receptivityto external… (more)

Subjects/Keywords: VERBRENNUNGSDYNAMIK (BRENNSTOFFTECHNOLOGIE); VERBRENNUNGSDRUCK + FLAMMENGESCHWINDIGKEIT + FLAMMENAUSBREITUNG (WÄRMELEHRE); GAS COMBUSTION (FUEL TECHNOLOGY); FUEL SUPPLY + CARBURETION (INTERNAL COMBUSTION ENGINES); BRENNKAMMERN (GASTURBINEN); THERMAL EXCITATION OF VIBRATIONS (ACOUSTICS); COMBUSTION CHAMBERS (GAS TURBINES); THERMISCHE SCHWINGUNGSERREGUNG (AKUSTIK); BRENNSTOFFZUFUHR + GEMISCHBILDUNG (VERBRENNUNGSMOTOREN); GASVERBRENNUNG (BRENNSTOFFTECHNOLOGIE); GASTURBINEN (VERBRENNUNGSKRAFTMASCHINEN); COMBUSTION DYNAMICS (FUEL TECHNOLOGY); COMBUSTION PRESSURE + FLAME SPEED + FLAME PROPAGATION (THERMOPHYSICS); GAS TURBINES, COMBUSTION TURBINES (INTERNAL COMBUSTION ENGINES); info:eu-repo/classification/ddc/620; info:eu-repo/classification/ddc/530; Engineering & allied operations; Physics

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

APA (6th Edition):

Fritsche, D. (2005). Origin and control of thermoacoustic instabilities in lean premixed gas turbine combustion. (Doctoral Dissertation). ETH Zürich. Retrieved from http://hdl.handle.net/20.500.11850/47744

Chicago Manual of Style (16th Edition):

Fritsche, Daniel. “Origin and control of thermoacoustic instabilities in lean premixed gas turbine combustion.” 2005. Doctoral Dissertation, ETH Zürich. Accessed January 19, 2020. http://hdl.handle.net/20.500.11850/47744.

MLA Handbook (7th Edition):

Fritsche, Daniel. “Origin and control of thermoacoustic instabilities in lean premixed gas turbine combustion.” 2005. Web. 19 Jan 2020.

Vancouver:

Fritsche D. Origin and control of thermoacoustic instabilities in lean premixed gas turbine combustion. [Internet] [Doctoral dissertation]. ETH Zürich; 2005. [cited 2020 Jan 19]. Available from: http://hdl.handle.net/20.500.11850/47744.

Council of Science Editors:

Fritsche D. Origin and control of thermoacoustic instabilities in lean premixed gas turbine combustion. [Doctoral Dissertation]. ETH Zürich; 2005. Available from: http://hdl.handle.net/20.500.11850/47744


ETH Zürich

29. 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

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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 19, 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. 19 Jan 2020.

Vancouver:

Büche D. Multi-objective evolutionary optimization of gas turbine components. [Internet] [Doctoral dissertation]. ETH Zürich; 2003. [cited 2020 Jan 19]. 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

30. 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

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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 19, 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. 19 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 19]. 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

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