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You searched for subject:(Combustion Instabilities). Showing records 1 – 30 of 54 total matches.

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University of Adelaide

1. Hardi, Justin S. Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.

Degree: 2012, University of Adelaide

 Self-sustaining pressure oscillations in the combustion chamber, or combustion instability, is a commonly encountered and potentially damaging phenomenon in liquid propellant rocket engines (LPREs). In… (more)

Subjects/Keywords: rocket engine; combustion; cryogenic; instabilities; combustion instabilities; liquid rocket

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APA (6th Edition):

Hardi, J. S. (2012). Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/82071

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):

Hardi, Justin S. “Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.” 2012. Thesis, University of Adelaide. Accessed October 22, 2019. http://hdl.handle.net/2440/82071.

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

MLA Handbook (7th Edition):

Hardi, Justin S. “Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines.” 2012. Web. 22 Oct 2019.

Vancouver:

Hardi JS. Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines. [Internet] [Thesis]. University of Adelaide; 2012. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/2440/82071.

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

Council of Science Editors:

Hardi JS. Experimental investigation of high frequency combustion instability in cryogenic oxygen-hydrogen rocket engines. [Thesis]. University of Adelaide; 2012. Available from: http://hdl.handle.net/2440/82071

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


University of Cincinnati

2. Knadler, Michael. Validation of a Physics-Based Low-Order Thermo-Acoustic Model of a Liquid-Fueled Gas Turbine Combustor and its Application for Predicting Combustion Driven Oscillations.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2017, University of Cincinnati

 This research validates a physics based model for the thermo-acoustic behavior of a liquid-fueled gas turbine combustor as a tool for diagnosing the cause of… (more)

Subjects/Keywords: Aerospace Materials; Combustion; Combustion Instabilities; Thermoacoustics; Gas Turbine Combustion

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APA (6th Edition):

Knadler, M. (2017). Validation of a Physics-Based Low-Order Thermo-Acoustic Model of a Liquid-Fueled Gas Turbine Combustor and its Application for Predicting Combustion Driven Oscillations. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1511861629413018

Chicago Manual of Style (16th Edition):

Knadler, Michael. “Validation of a Physics-Based Low-Order Thermo-Acoustic Model of a Liquid-Fueled Gas Turbine Combustor and its Application for Predicting Combustion Driven Oscillations.” 2017. Doctoral Dissertation, University of Cincinnati. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1511861629413018.

MLA Handbook (7th Edition):

Knadler, Michael. “Validation of a Physics-Based Low-Order Thermo-Acoustic Model of a Liquid-Fueled Gas Turbine Combustor and its Application for Predicting Combustion Driven Oscillations.” 2017. Web. 22 Oct 2019.

Vancouver:

Knadler M. Validation of a Physics-Based Low-Order Thermo-Acoustic Model of a Liquid-Fueled Gas Turbine Combustor and its Application for Predicting Combustion Driven Oscillations. [Internet] [Doctoral dissertation]. University of Cincinnati; 2017. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1511861629413018.

Council of Science Editors:

Knadler M. Validation of a Physics-Based Low-Order Thermo-Acoustic Model of a Liquid-Fueled Gas Turbine Combustor and its Application for Predicting Combustion Driven Oscillations. [Doctoral Dissertation]. University of Cincinnati; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1511861629413018


Miami University

3. Wisman, David L, II. ELECTRIC FIELD INDUCED STABILITY MODIFICATIONS IN PRE-MIXED HYDROCARBON FLAMES.

Degree: MS, Physics, 2006, Miami University

 This work focuses upon the effects of electric fields on the stability of pre-mixed hydrocarbon flames fueled by methane, propane and butane. For all fuels… (more)

Subjects/Keywords: Combustion; Flame Instabilities

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APA (6th Edition):

Wisman, David L, I. (2006). ELECTRIC FIELD INDUCED STABILITY MODIFICATIONS IN PRE-MIXED HYDROCARBON FLAMES. (Masters Thesis). Miami University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=miami1154727896

Chicago Manual of Style (16th Edition):

Wisman, David L, II. “ELECTRIC FIELD INDUCED STABILITY MODIFICATIONS IN PRE-MIXED HYDROCARBON FLAMES.” 2006. Masters Thesis, Miami University. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=miami1154727896.

MLA Handbook (7th Edition):

Wisman, David L, II. “ELECTRIC FIELD INDUCED STABILITY MODIFICATIONS IN PRE-MIXED HYDROCARBON FLAMES.” 2006. Web. 22 Oct 2019.

Vancouver:

Wisman, David L I. ELECTRIC FIELD INDUCED STABILITY MODIFICATIONS IN PRE-MIXED HYDROCARBON FLAMES. [Internet] [Masters thesis]. Miami University; 2006. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1154727896.

Council of Science Editors:

Wisman, David L I. ELECTRIC FIELD INDUCED STABILITY MODIFICATIONS IN PRE-MIXED HYDROCARBON FLAMES. [Masters Thesis]. Miami University; 2006. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1154727896


Georgia Tech

4. Smith, Travis Edward. Experimental investigation of transverse acoustic instabilities.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 This work presents 5 kHz stereo PIV and OH PLIF measurements as well as OH* and CH* chemiluminescence measurements of transversely forced swirl flames. The… (more)

Subjects/Keywords: Combustion instabilities; Swirl flame; Transverse acoustics

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APA (6th Edition):

Smith, T. E. (2017). Experimental investigation of transverse acoustic instabilities. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59252

Chicago Manual of Style (16th Edition):

Smith, Travis Edward. “Experimental investigation of transverse acoustic instabilities.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 22, 2019. http://hdl.handle.net/1853/59252.

MLA Handbook (7th Edition):

Smith, Travis Edward. “Experimental investigation of transverse acoustic instabilities.” 2017. Web. 22 Oct 2019.

Vancouver:

Smith TE. Experimental investigation of transverse acoustic instabilities. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/1853/59252.

Council of Science Editors:

Smith TE. Experimental investigation of transverse acoustic instabilities. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59252

5. Lamraoui, Ammar. Acoustique et dynamique de flamme dans un foyer turbulent prémélangé swirlé : application à l'étude du bruit de combustion dans les chambres de turbines à gaz. : Investigating combustion noise and instabilities in a gas turbine combustor : acoustic propagation and flame dynamics.

Degree: Docteur es, Energétique, 2011, Châtenay-Malabry, Ecole centrale de Paris

 La réduction des émissions de polluants et l’augmentation du rendement des moteurs ont conduit à une large utilisation de régimes de combustion pauvres en carburant… (more)

Subjects/Keywords: Bruit de combustion; Instabilités de combustion; Dynamique de flamme; Combustion noise; Combustion instabilities; Flame dynamics

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APA (6th Edition):

Lamraoui, A. (2011). Acoustique et dynamique de flamme dans un foyer turbulent prémélangé swirlé : application à l'étude du bruit de combustion dans les chambres de turbines à gaz. : Investigating combustion noise and instabilities in a gas turbine combustor : acoustic propagation and flame dynamics. (Doctoral Dissertation). Châtenay-Malabry, Ecole centrale de Paris. Retrieved from http://www.theses.fr/2011ECAP0028

Chicago Manual of Style (16th Edition):

Lamraoui, Ammar. “Acoustique et dynamique de flamme dans un foyer turbulent prémélangé swirlé : application à l'étude du bruit de combustion dans les chambres de turbines à gaz. : Investigating combustion noise and instabilities in a gas turbine combustor : acoustic propagation and flame dynamics.” 2011. Doctoral Dissertation, Châtenay-Malabry, Ecole centrale de Paris. Accessed October 22, 2019. http://www.theses.fr/2011ECAP0028.

MLA Handbook (7th Edition):

Lamraoui, Ammar. “Acoustique et dynamique de flamme dans un foyer turbulent prémélangé swirlé : application à l'étude du bruit de combustion dans les chambres de turbines à gaz. : Investigating combustion noise and instabilities in a gas turbine combustor : acoustic propagation and flame dynamics.” 2011. Web. 22 Oct 2019.

Vancouver:

Lamraoui A. Acoustique et dynamique de flamme dans un foyer turbulent prémélangé swirlé : application à l'étude du bruit de combustion dans les chambres de turbines à gaz. : Investigating combustion noise and instabilities in a gas turbine combustor : acoustic propagation and flame dynamics. [Internet] [Doctoral dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2011. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2011ECAP0028.

Council of Science Editors:

Lamraoui A. Acoustique et dynamique de flamme dans un foyer turbulent prémélangé swirlé : application à l'étude du bruit de combustion dans les chambres de turbines à gaz. : Investigating combustion noise and instabilities in a gas turbine combustor : acoustic propagation and flame dynamics. [Doctoral Dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2011. Available from: http://www.theses.fr/2011ECAP0028

6. Ndiaye, Aïssatou. Uncertainty Quantification of Thermo-acousticinstabilities in gas turbine combustors : Quantification des incertitudes pour la prédiction des instabilités thermo-acoustiques dans les chambres de combustion.

Degree: Docteur es, Mathématiques et modélisation, 2017, Montpellier

 Les instabilités thermo-acoustiques résultent de l'interaction entre les oscillations de pression acoustique et les fluctuations du taux de dégagement de chaleur de la flamme. Ces… (more)

Subjects/Keywords: Quantification d'incertitudes; Combustion; Instabilités Thermoacoustique; Combustion; Uncertainty quantification; Thermoacoustic Instabilities

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APA (6th Edition):

Ndiaye, A. (2017). Uncertainty Quantification of Thermo-acousticinstabilities in gas turbine combustors : Quantification des incertitudes pour la prédiction des instabilités thermo-acoustiques dans les chambres de combustion. (Doctoral Dissertation). Montpellier. Retrieved from http://www.theses.fr/2017MONTS062

Chicago Manual of Style (16th Edition):

Ndiaye, Aïssatou. “Uncertainty Quantification of Thermo-acousticinstabilities in gas turbine combustors : Quantification des incertitudes pour la prédiction des instabilités thermo-acoustiques dans les chambres de combustion.” 2017. Doctoral Dissertation, Montpellier. Accessed October 22, 2019. http://www.theses.fr/2017MONTS062.

MLA Handbook (7th Edition):

Ndiaye, Aïssatou. “Uncertainty Quantification of Thermo-acousticinstabilities in gas turbine combustors : Quantification des incertitudes pour la prédiction des instabilités thermo-acoustiques dans les chambres de combustion.” 2017. Web. 22 Oct 2019.

Vancouver:

Ndiaye A. Uncertainty Quantification of Thermo-acousticinstabilities in gas turbine combustors : Quantification des incertitudes pour la prédiction des instabilités thermo-acoustiques dans les chambres de combustion. [Internet] [Doctoral dissertation]. Montpellier; 2017. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2017MONTS062.

Council of Science Editors:

Ndiaye A. Uncertainty Quantification of Thermo-acousticinstabilities in gas turbine combustors : Quantification des incertitudes pour la prédiction des instabilités thermo-acoustiques dans les chambres de combustion. [Doctoral Dissertation]. Montpellier; 2017. Available from: http://www.theses.fr/2017MONTS062


INP Toulouse

7. Ghani, Abdulla. Simulation aux grandes échelles des instabilités de combustion transverses des flammes parfaitement prémélangées et swirlées diphasiques : LES of self-excited transverse combustion instabilities in perfectly-premixed and swirling spray flames.

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

Dans cette thèse, les instabilités de combustion sont étudiées sur deux types de configuration. Tout d’abord, un cas académique stabilisé par un dièdre (Volvo) est… (more)

Subjects/Keywords: Mode transverse; Instabilités de combustion; Transverse modes; Combustion instabilities

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APA (6th Edition):

Ghani, A. (2015). Simulation aux grandes échelles des instabilités de combustion transverses des flammes parfaitement prémélangées et swirlées diphasiques : LES of self-excited transverse combustion instabilities in perfectly-premixed and swirling spray flames. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2015INPT0068

Chicago Manual of Style (16th Edition):

Ghani, Abdulla. “Simulation aux grandes échelles des instabilités de combustion transverses des flammes parfaitement prémélangées et swirlées diphasiques : LES of self-excited transverse combustion instabilities in perfectly-premixed and swirling spray flames.” 2015. Doctoral Dissertation, INP Toulouse. Accessed October 22, 2019. http://www.theses.fr/2015INPT0068.

MLA Handbook (7th Edition):

Ghani, Abdulla. “Simulation aux grandes échelles des instabilités de combustion transverses des flammes parfaitement prémélangées et swirlées diphasiques : LES of self-excited transverse combustion instabilities in perfectly-premixed and swirling spray flames.” 2015. Web. 22 Oct 2019.

Vancouver:

Ghani A. Simulation aux grandes échelles des instabilités de combustion transverses des flammes parfaitement prémélangées et swirlées diphasiques : LES of self-excited transverse combustion instabilities in perfectly-premixed and swirling spray flames. [Internet] [Doctoral dissertation]. INP Toulouse; 2015. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2015INPT0068.

Council of Science Editors:

Ghani A. Simulation aux grandes échelles des instabilités de combustion transverses des flammes parfaitement prémélangées et swirlées diphasiques : LES of self-excited transverse combustion instabilities in perfectly-premixed and swirling spray flames. [Doctoral Dissertation]. INP Toulouse; 2015. Available from: http://www.theses.fr/2015INPT0068


Purdue University

8. Tamanampudi, Gowtham Manikanta Reddy. Reduced Order Modeling and Analysis of Combustion Instabilities.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2015, Purdue University

 The coupling between unsteady heat release and pressure fluctuations in a combustor leads to the complex phenomenon of combustion instability. Combustion instability can lead to… (more)

Subjects/Keywords: Combustion instabilities; Combustion response function; COMSOL; Linearized Euler equation; Transverse Instability

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APA (6th Edition):

Tamanampudi, G. M. R. (2015). Reduced Order Modeling and Analysis of Combustion Instabilities. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/1080

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):

Tamanampudi, Gowtham Manikanta Reddy. “Reduced Order Modeling and Analysis of Combustion Instabilities.” 2015. Thesis, Purdue University. Accessed October 22, 2019. https://docs.lib.purdue.edu/open_access_theses/1080.

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

MLA Handbook (7th Edition):

Tamanampudi, Gowtham Manikanta Reddy. “Reduced Order Modeling and Analysis of Combustion Instabilities.” 2015. Web. 22 Oct 2019.

Vancouver:

Tamanampudi GMR. Reduced Order Modeling and Analysis of Combustion Instabilities. [Internet] [Thesis]. Purdue University; 2015. [cited 2019 Oct 22]. Available from: https://docs.lib.purdue.edu/open_access_theses/1080.

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

Council of Science Editors:

Tamanampudi GMR. Reduced Order Modeling and Analysis of Combustion Instabilities. [Thesis]. Purdue University; 2015. Available from: https://docs.lib.purdue.edu/open_access_theses/1080

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

9. Prieur, Kevin. Dynamique de la combustion dans un foyer annulaire multi-injecteurs diphasique : Combustion dynamics of an annular combustor with multiple spray injectors.

Degree: Docteur es, Combustion, 2017, Paris Saclay

Ces dernières décennies ont vu apparaître de nombreuses innovations dans le domaine de la combustion afin de réduire la consommation et les émissions polluantes. De… (more)

Subjects/Keywords: Dynamique de la combustion; Instabilités de combustion; Chambre annulaire; Allumage; Combustion dynamics; Combustion instabilities; Annular chamber; Light-round

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APA (6th Edition):

Prieur, K. (2017). Dynamique de la combustion dans un foyer annulaire multi-injecteurs diphasique : Combustion dynamics of an annular combustor with multiple spray injectors. (Doctoral Dissertation). Paris Saclay. Retrieved from http://www.theses.fr/2017SACLC070

Chicago Manual of Style (16th Edition):

Prieur, Kevin. “Dynamique de la combustion dans un foyer annulaire multi-injecteurs diphasique : Combustion dynamics of an annular combustor with multiple spray injectors.” 2017. Doctoral Dissertation, Paris Saclay. Accessed October 22, 2019. http://www.theses.fr/2017SACLC070.

MLA Handbook (7th Edition):

Prieur, Kevin. “Dynamique de la combustion dans un foyer annulaire multi-injecteurs diphasique : Combustion dynamics of an annular combustor with multiple spray injectors.” 2017. Web. 22 Oct 2019.

Vancouver:

Prieur K. Dynamique de la combustion dans un foyer annulaire multi-injecteurs diphasique : Combustion dynamics of an annular combustor with multiple spray injectors. [Internet] [Doctoral dissertation]. Paris Saclay; 2017. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2017SACLC070.

Council of Science Editors:

Prieur K. Dynamique de la combustion dans un foyer annulaire multi-injecteurs diphasique : Combustion dynamics of an annular combustor with multiple spray injectors. [Doctoral Dissertation]. Paris Saclay; 2017. Available from: http://www.theses.fr/2017SACLC070

10. Boudy, Frédéric. Analyse de la dynamique non-linéaire et du contrôle des instabilités de combustion fondée sur la "Flame Describing Function" (FDF) : Nonlinear dynamics and control analysis of combustion instabilities based on the “Flame Describing Function” (FDF).

Degree: Docteur es, Energétique, 2012, Châtenay-Malabry, Ecole centrale de Paris

 Cette thèse se concentre sur l’étude des instabilités de combustion dans un brûleur prémélangé. Les instabilités sont généralement issues d’un couplage entre la combustion et… (more)

Subjects/Keywords: Instabilités de combustion; Couplage thermoacoustique; Cycle limite stable; Combustion instabilities; Thermoacoustic coupling; Flame Describing Function

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APA (6th Edition):

Boudy, F. (2012). Analyse de la dynamique non-linéaire et du contrôle des instabilités de combustion fondée sur la "Flame Describing Function" (FDF) : Nonlinear dynamics and control analysis of combustion instabilities based on the “Flame Describing Function” (FDF). (Doctoral Dissertation). Châtenay-Malabry, Ecole centrale de Paris. Retrieved from http://www.theses.fr/2012ECAP0056

Chicago Manual of Style (16th Edition):

Boudy, Frédéric. “Analyse de la dynamique non-linéaire et du contrôle des instabilités de combustion fondée sur la "Flame Describing Function" (FDF) : Nonlinear dynamics and control analysis of combustion instabilities based on the “Flame Describing Function” (FDF).” 2012. Doctoral Dissertation, Châtenay-Malabry, Ecole centrale de Paris. Accessed October 22, 2019. http://www.theses.fr/2012ECAP0056.

MLA Handbook (7th Edition):

Boudy, Frédéric. “Analyse de la dynamique non-linéaire et du contrôle des instabilités de combustion fondée sur la "Flame Describing Function" (FDF) : Nonlinear dynamics and control analysis of combustion instabilities based on the “Flame Describing Function” (FDF).” 2012. Web. 22 Oct 2019.

Vancouver:

Boudy F. Analyse de la dynamique non-linéaire et du contrôle des instabilités de combustion fondée sur la "Flame Describing Function" (FDF) : Nonlinear dynamics and control analysis of combustion instabilities based on the “Flame Describing Function” (FDF). [Internet] [Doctoral dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2012. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2012ECAP0056.

Council of Science Editors:

Boudy F. Analyse de la dynamique non-linéaire et du contrôle des instabilités de combustion fondée sur la "Flame Describing Function" (FDF) : Nonlinear dynamics and control analysis of combustion instabilities based on the “Flame Describing Function” (FDF). [Doctoral Dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2012. Available from: http://www.theses.fr/2012ECAP0056

11. Tran, Nicolas. Influence de la condition limite acoustique amont sur les instabilités de combustion de grande amplitude : conception d’un système robuste de contrôle d’impédance : Influence of inlet acoustic boundary condition on large amplitude combustion instabilities : design of a robust impedance control system.

Degree: Docteur es, Energétique, 2009, Châtenay-Malabry, Ecole centrale de Paris

 Les contraintes économiques, environnementales et sociétales de ces vingt dernières années notamment dans les domaines de l’énergie et des transports ont débouché sur le développement… (more)

Subjects/Keywords: Combustion; Acoustique; Instabilités thermoacoustiques; Contrôle Passif; Plaques Perforées; Combustion; Thermo-acoustic instabilities; Passive Control

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APA (6th Edition):

Tran, N. (2009). Influence de la condition limite acoustique amont sur les instabilités de combustion de grande amplitude : conception d’un système robuste de contrôle d’impédance : Influence of inlet acoustic boundary condition on large amplitude combustion instabilities : design of a robust impedance control system. (Doctoral Dissertation). Châtenay-Malabry, Ecole centrale de Paris. Retrieved from http://www.theses.fr/2009ECAP0013

Chicago Manual of Style (16th Edition):

Tran, Nicolas. “Influence de la condition limite acoustique amont sur les instabilités de combustion de grande amplitude : conception d’un système robuste de contrôle d’impédance : Influence of inlet acoustic boundary condition on large amplitude combustion instabilities : design of a robust impedance control system.” 2009. Doctoral Dissertation, Châtenay-Malabry, Ecole centrale de Paris. Accessed October 22, 2019. http://www.theses.fr/2009ECAP0013.

MLA Handbook (7th Edition):

Tran, Nicolas. “Influence de la condition limite acoustique amont sur les instabilités de combustion de grande amplitude : conception d’un système robuste de contrôle d’impédance : Influence of inlet acoustic boundary condition on large amplitude combustion instabilities : design of a robust impedance control system.” 2009. Web. 22 Oct 2019.

Vancouver:

Tran N. Influence de la condition limite acoustique amont sur les instabilités de combustion de grande amplitude : conception d’un système robuste de contrôle d’impédance : Influence of inlet acoustic boundary condition on large amplitude combustion instabilities : design of a robust impedance control system. [Internet] [Doctoral dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2009. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2009ECAP0013.

Council of Science Editors:

Tran N. Influence de la condition limite acoustique amont sur les instabilités de combustion de grande amplitude : conception d’un système robuste de contrôle d’impédance : Influence of inlet acoustic boundary condition on large amplitude combustion instabilities : design of a robust impedance control system. [Doctoral Dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2009. Available from: http://www.theses.fr/2009ECAP0013


University of Cincinnati

12. Estefanos, Wessam. Effects of the Fuel-Air Mixing on Combustion Instabilities and NOx Emissions in Lean Premixed Combustion.

Degree: PhD, Engineering and Applied Science: Aerospace Engineering, 2016, University of Cincinnati

 An experimental study was conducted to investigate the effects of the fuel-air mixing on combustion instabilities and NO<i>x</i> emissions in lean premixed combustion. High speed… (more)

Subjects/Keywords: Engineering; Lean premixed combustion; Fuel-air mixing; NOx emissions; Combustion instabilities; Unsteady flow behavior

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APA (6th Edition):

Estefanos, W. (2016). Effects of the Fuel-Air Mixing on Combustion Instabilities and NOx Emissions in Lean Premixed Combustion. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1460731723

Chicago Manual of Style (16th Edition):

Estefanos, Wessam. “Effects of the Fuel-Air Mixing on Combustion Instabilities and NOx Emissions in Lean Premixed Combustion.” 2016. Doctoral Dissertation, University of Cincinnati. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1460731723.

MLA Handbook (7th Edition):

Estefanos, Wessam. “Effects of the Fuel-Air Mixing on Combustion Instabilities and NOx Emissions in Lean Premixed Combustion.” 2016. Web. 22 Oct 2019.

Vancouver:

Estefanos W. Effects of the Fuel-Air Mixing on Combustion Instabilities and NOx Emissions in Lean Premixed Combustion. [Internet] [Doctoral dissertation]. University of Cincinnati; 2016. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1460731723.

Council of Science Editors:

Estefanos W. Effects of the Fuel-Air Mixing on Combustion Instabilities and NOx Emissions in Lean Premixed Combustion. [Doctoral Dissertation]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1460731723


Penn State University

13. Orawannukul, Poravee. An experimental study of forced flame response in technically premixed flame in a lean premixed gas turbine combustor.

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

 Flame response in a technically premixed, swirl-stabilized, turbulent, lean-premixed natural gas-air flame is investigated in a single research gas turbine injector. The main purpose of… (more)

Subjects/Keywords: Forced flame response; technically premixed flames; combustion instabilities; flame transfer function

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APA (6th Edition):

Orawannukul, P. (2014). An experimental study of forced flame response in technically premixed flame in a lean premixed gas turbine combustor. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/20795

Chicago Manual of Style (16th Edition):

Orawannukul, Poravee. “An experimental study of forced flame response in technically premixed flame in a lean premixed gas turbine combustor.” 2014. Doctoral Dissertation, Penn State University. Accessed October 22, 2019. https://etda.libraries.psu.edu/catalog/20795.

MLA Handbook (7th Edition):

Orawannukul, Poravee. “An experimental study of forced flame response in technically premixed flame in a lean premixed gas turbine combustor.” 2014. Web. 22 Oct 2019.

Vancouver:

Orawannukul P. An experimental study of forced flame response in technically premixed flame in a lean premixed gas turbine combustor. [Internet] [Doctoral dissertation]. Penn State University; 2014. [cited 2019 Oct 22]. Available from: https://etda.libraries.psu.edu/catalog/20795.

Council of Science Editors:

Orawannukul P. An experimental study of forced flame response in technically premixed flame in a lean premixed gas turbine combustor. [Doctoral Dissertation]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/20795


Virginia Tech

14. Nord, Lars. A Thermoacoustic Characterization of a Rijke-type Tube Combustor.

Degree: MS, Mechanical Engineering, 2001, Virginia Tech

 Pressure pulsations, or thermoacoustic instabilities, as they are called in the research community, can cause extensive damage in gas turbine combustion chambers. To understand the… (more)

Subjects/Keywords: flame instabilities; combustion; chemiluminescence; acoustics

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APA (6th Edition):

Nord, L. (2001). A Thermoacoustic Characterization of a Rijke-type Tube Combustor. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31437

Chicago Manual of Style (16th Edition):

Nord, Lars. “A Thermoacoustic Characterization of a Rijke-type Tube Combustor.” 2001. Masters Thesis, Virginia Tech. Accessed October 22, 2019. http://hdl.handle.net/10919/31437.

MLA Handbook (7th Edition):

Nord, Lars. “A Thermoacoustic Characterization of a Rijke-type Tube Combustor.” 2001. Web. 22 Oct 2019.

Vancouver:

Nord L. A Thermoacoustic Characterization of a Rijke-type Tube Combustor. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/10919/31437.

Council of Science Editors:

Nord L. A Thermoacoustic Characterization of a Rijke-type Tube Combustor. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/31437


Virginia Tech

15. 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 October 22, 2019. 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. 22 Oct 2019.

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 2019 Oct 22]. 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

16. Mirat, Clément. Analyse des instabilités de combustion dans des foyers de centrale thermique fonctionnant au fioul lourd : Analysis of combustion instabilities in thermal power plants operating with heavy fuel oil.

Degree: Docteur es, Energétique, 2015, Châtenay-Malabry, Ecole centrale de Paris

 Des crises vibratoires ont été constatées dans plusieurs centrales thermiques d’EDF opérant avec du fioul lourd, certaines ayant entraîné l’arrêt du foyer. Ce travail traite… (more)

Subjects/Keywords: Ecoulement swirlé; Spray; Dynamique de la combustion; Instabilités de combustion; Swirl flame; Spray; Combustion dynamics; Thermo-acoustics instabilities

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APA (6th Edition):

Mirat, C. (2015). Analyse des instabilités de combustion dans des foyers de centrale thermique fonctionnant au fioul lourd : Analysis of combustion instabilities in thermal power plants operating with heavy fuel oil. (Doctoral Dissertation). Châtenay-Malabry, Ecole centrale de Paris. Retrieved from http://www.theses.fr/2015ECAP0037

Chicago Manual of Style (16th Edition):

Mirat, Clément. “Analyse des instabilités de combustion dans des foyers de centrale thermique fonctionnant au fioul lourd : Analysis of combustion instabilities in thermal power plants operating with heavy fuel oil.” 2015. Doctoral Dissertation, Châtenay-Malabry, Ecole centrale de Paris. Accessed October 22, 2019. http://www.theses.fr/2015ECAP0037.

MLA Handbook (7th Edition):

Mirat, Clément. “Analyse des instabilités de combustion dans des foyers de centrale thermique fonctionnant au fioul lourd : Analysis of combustion instabilities in thermal power plants operating with heavy fuel oil.” 2015. Web. 22 Oct 2019.

Vancouver:

Mirat C. Analyse des instabilités de combustion dans des foyers de centrale thermique fonctionnant au fioul lourd : Analysis of combustion instabilities in thermal power plants operating with heavy fuel oil. [Internet] [Doctoral dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2015. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2015ECAP0037.

Council of Science Editors:

Mirat C. Analyse des instabilités de combustion dans des foyers de centrale thermique fonctionnant au fioul lourd : Analysis of combustion instabilities in thermal power plants operating with heavy fuel oil. [Doctoral Dissertation]. Châtenay-Malabry, Ecole centrale de Paris; 2015. Available from: http://www.theses.fr/2015ECAP0037


Georgia Tech

17. Bellows, Benjamin Davis. Characterization of nonlinear heat release-acoustic interactions in gas turbine combustors.

Degree: PhD, Aerospace Engineering, 2006, Georgia Tech

 This thesis describes an experimental investigation of the flame transfer function between flow disturbances and heat release oscillations in lean, premixed combustors. This research effort… (more)

Subjects/Keywords: Nonlinear flame transfer function; Combustion instabilities

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APA (6th Edition):

Bellows, B. D. (2006). Characterization of nonlinear heat release-acoustic interactions in gas turbine combustors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/10474

Chicago Manual of Style (16th Edition):

Bellows, Benjamin Davis. “Characterization of nonlinear heat release-acoustic interactions in gas turbine combustors.” 2006. Doctoral Dissertation, Georgia Tech. Accessed October 22, 2019. http://hdl.handle.net/1853/10474.

MLA Handbook (7th Edition):

Bellows, Benjamin Davis. “Characterization of nonlinear heat release-acoustic interactions in gas turbine combustors.” 2006. Web. 22 Oct 2019.

Vancouver:

Bellows BD. Characterization of nonlinear heat release-acoustic interactions in gas turbine combustors. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/1853/10474.

Council of Science Editors:

Bellows BD. Characterization of nonlinear heat release-acoustic interactions in gas turbine combustors. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/10474


University of Alabama

18. Sequera, Daniel E. Reduction of combustion noise and instabilities using porous inert material with a swirl-stabilized burner.

Degree: 2011, University of Alabama

Combustion instabilities represent a major problem during operation of power generation systems that can lead to costly shutdown. Combustion instabilities are self excited large amplitude… (more)

Subjects/Keywords: Electronic Thesis or Dissertation;  – thesis; Mechanical Engineering; Acoustics; Combustion; Instabilities; Noise; PIM; Porous; Swirl

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APA (6th Edition):

Sequera, D. E. (2011). Reduction of combustion noise and instabilities using porous inert material with a swirl-stabilized burner. (Thesis). University of Alabama. Retrieved from http://purl.lib.ua.edu/34954

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):

Sequera, Daniel E. “Reduction of combustion noise and instabilities using porous inert material with a swirl-stabilized burner.” 2011. Thesis, University of Alabama. Accessed October 22, 2019. http://purl.lib.ua.edu/34954.

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

MLA Handbook (7th Edition):

Sequera, Daniel E. “Reduction of combustion noise and instabilities using porous inert material with a swirl-stabilized burner.” 2011. Web. 22 Oct 2019.

Vancouver:

Sequera DE. Reduction of combustion noise and instabilities using porous inert material with a swirl-stabilized burner. [Internet] [Thesis]. University of Alabama; 2011. [cited 2019 Oct 22]. Available from: http://purl.lib.ua.edu/34954.

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

Council of Science Editors:

Sequera DE. Reduction of combustion noise and instabilities using porous inert material with a swirl-stabilized burner. [Thesis]. University of Alabama; 2011. Available from: http://purl.lib.ua.edu/34954

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


INP Toulouse

19. Roux, Anthony. Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets.

Degree: Docteur es, Dynamique des fluides, 2009, INP Toulouse

La conception d'un statoréacteur bénificie aujourd'hui des progrès divers des outils numériques permettant par la même occasion d'alléger les différentes étapes préliminaires de tests en… (more)

Subjects/Keywords: Simulations aux Grandes Echelles; Statoréacteur; Turbulence; Instabilitiés de combustion; Ecoulement Diphasique; Large-Eddy Simulation; Ramjet; Turbulence; Combustion instabilities; Two-Phase Flows

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APA (6th Edition):

Roux, A. (2009). Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2009INPT025H

Chicago Manual of Style (16th Edition):

Roux, Anthony. “Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets.” 2009. Doctoral Dissertation, INP Toulouse. Accessed October 22, 2019. http://www.theses.fr/2009INPT025H.

MLA Handbook (7th Edition):

Roux, Anthony. “Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets.” 2009. Web. 22 Oct 2019.

Vancouver:

Roux A. Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets. [Internet] [Doctoral dissertation]. INP Toulouse; 2009. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2009INPT025H.

Council of Science Editors:

Roux A. Simulation aux Grandes Echelles d'un statoréacteur : Large-Eddy Simulation of Ramjets. [Doctoral Dissertation]. INP Toulouse; 2009. Available from: http://www.theses.fr/2009INPT025H


INP Toulouse

20. Kaiser, Thomas. Impact of flow rotation on flame dynamics and hydrodynamic stability : Influence de la rotation de l'écoulement sur la dynamique des flammes et la stabilité hydrodynamique.

Degree: Docteur es, Dynamique des fluides, 2019, INP Toulouse

Cette thèse a pour but l’étude de la rotation de l’écoulement des grandes échelles dans deux configurations. La première configuration se concentre sur l’effet de… (more)

Subjects/Keywords: Instabilités de combustion; Analyses de stabilité; Acoustique; Dynamique des flammes; Combustion instabilities; Stability analysis; Acoustics; Flame dynamics; 530

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APA (6th Edition):

Kaiser, T. (2019). Impact of flow rotation on flame dynamics and hydrodynamic stability : Influence de la rotation de l'écoulement sur la dynamique des flammes et la stabilité hydrodynamique. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2019INPT0011

Chicago Manual of Style (16th Edition):

Kaiser, Thomas. “Impact of flow rotation on flame dynamics and hydrodynamic stability : Influence de la rotation de l'écoulement sur la dynamique des flammes et la stabilité hydrodynamique.” 2019. Doctoral Dissertation, INP Toulouse. Accessed October 22, 2019. http://www.theses.fr/2019INPT0011.

MLA Handbook (7th Edition):

Kaiser, Thomas. “Impact of flow rotation on flame dynamics and hydrodynamic stability : Influence de la rotation de l'écoulement sur la dynamique des flammes et la stabilité hydrodynamique.” 2019. Web. 22 Oct 2019.

Vancouver:

Kaiser T. Impact of flow rotation on flame dynamics and hydrodynamic stability : Influence de la rotation de l'écoulement sur la dynamique des flammes et la stabilité hydrodynamique. [Internet] [Doctoral dissertation]. INP Toulouse; 2019. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2019INPT0011.

Council of Science Editors:

Kaiser T. Impact of flow rotation on flame dynamics and hydrodynamic stability : Influence de la rotation de l'écoulement sur la dynamique des flammes et la stabilité hydrodynamique. [Doctoral Dissertation]. INP Toulouse; 2019. Available from: http://www.theses.fr/2019INPT0011


Delft University of Technology

21. Sliphorst, M. High Frequency Combustion Instabilities of LOx/CH4 Spray Flames in Rocket Engine Combustion Chambers.

Degree: 2011, Delft University of Technology

 Ever since the early stages of space transportation in the 1940’s, and the related liquid propellant rocket engine development, combustion instability has been a major… (more)

Subjects/Keywords: combustion; combustion instabilities; HF-instabilities; acoustics; eigenmodes; spray combustion; resonant combustion; resonance; Rayleigh criterion; response factor

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APA (6th Edition):

Sliphorst, M. (2011). High Frequency Combustion Instabilities of LOx/CH4 Spray Flames in Rocket Engine Combustion Chambers. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283

Chicago Manual of Style (16th Edition):

Sliphorst, M. “High Frequency Combustion Instabilities of LOx/CH4 Spray Flames in Rocket Engine Combustion Chambers.” 2011. Doctoral Dissertation, Delft University of Technology. Accessed October 22, 2019. http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283.

MLA Handbook (7th Edition):

Sliphorst, M. “High Frequency Combustion Instabilities of LOx/CH4 Spray Flames in Rocket Engine Combustion Chambers.” 2011. Web. 22 Oct 2019.

Vancouver:

Sliphorst M. High Frequency Combustion Instabilities of LOx/CH4 Spray Flames in Rocket Engine Combustion Chambers. [Internet] [Doctoral dissertation]. Delft University of Technology; 2011. [cited 2019 Oct 22]. Available from: http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283.

Council of Science Editors:

Sliphorst M. High Frequency Combustion Instabilities of LOx/CH4 Spray Flames in Rocket Engine Combustion Chambers. [Doctoral Dissertation]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; urn:NBN:nl:ui:24-uuid:403ca079-82db-4d09-9676-c3b38c007283 ; http://resolver.tudelft.nl/uuid:403ca079-82db-4d09-9676-c3b38c007283

22. Perovšek, Jaka. Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers.

Degree: Electrical and Space Engineering, 2018, Luleå University of Technology

  A visualisation procedure was developed which predicts excited hydroxyl (OH*) radiation from the Computational Fluid Dynamics (CFD) solutions of cryogenic hydrogen-oxygen rocket flames. The… (more)

Subjects/Keywords: spectral modelling; excited hydroxyl radiation; OH* radiation; ray tracing; spectroscopy; rocket combustion chambers; rocket engines; hydrogen-oxygen combustion; combustion instabilities; Aerospace Engineering; Rymd- och flygteknik

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APA (6th Edition):

Perovšek, J. (2018). Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277

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):

Perovšek, Jaka. “Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers.” 2018. Thesis, Luleå University of Technology. Accessed October 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277.

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

MLA Handbook (7th Edition):

Perovšek, Jaka. “Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers.” 2018. Web. 22 Oct 2019.

Vancouver:

Perovšek J. Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers. [Internet] [Thesis]. Luleå University of Technology; 2018. [cited 2019 Oct 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277.

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

Council of Science Editors:

Perovšek J. Ray Tracing and Spectral Modelling of Excited Hydroxyl Radiation from Cryogenic Flames in Rocket Combustion Chambers. [Thesis]. Luleå University of Technology; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-71277

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

23. O'Connor, Jacqueline. Response of a swirl-stabilized flame to transverse acoustic excitation.

Degree: PhD, Aerospace Engineering, 2011, Georgia Tech

 This work addresses the issue of transverse combustion instabilities in annular gas turbine combustor geometries. While modern low-emissions combustion strategies have made great strides in… (more)

Subjects/Keywords: Swirl-stabilized flame; Combustion instabilities; Transverse instabilities; Vortex breakdown; Acoustic excitation; Combustion; Flame; Gas-turbines Combustion

…issue of transverse combustion instabilities in annular gas turbine combustor geometries… …instabilities have long plagued the development and operation of high performance combustion… …instabilities have been studied in a variety of combustion technologies, but in gas turbine engines in… …practical interest. The first occurs in annular combustion systems, such as the instabilities in… …encountered in can combustion systems. These instabilities occur at relatively high frequencies… 

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APA (6th Edition):

O'Connor, J. (2011). Response of a swirl-stabilized flame to transverse acoustic excitation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43756

Chicago Manual of Style (16th Edition):

O'Connor, Jacqueline. “Response of a swirl-stabilized flame to transverse acoustic excitation.” 2011. Doctoral Dissertation, Georgia Tech. Accessed October 22, 2019. http://hdl.handle.net/1853/43756.

MLA Handbook (7th Edition):

O'Connor, Jacqueline. “Response of a swirl-stabilized flame to transverse acoustic excitation.” 2011. Web. 22 Oct 2019.

Vancouver:

O'Connor J. Response of a swirl-stabilized flame to transverse acoustic excitation. [Internet] [Doctoral dissertation]. Georgia Tech; 2011. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/1853/43756.

Council of Science Editors:

O'Connor J. Response of a swirl-stabilized flame to transverse acoustic excitation. [Doctoral Dissertation]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/43756

24. Shyani, Rajeshkumar Ghanshyambhai. Utilizing a cycle simulation to examine the use of exhaust gas recirculation (EGR) for a spark-ignition engine: including the second law of thermodynamics.

Degree: 2008, Texas A&M University

 The exhaust gas recirculation (EGR) system has been widely used to reduce nitrogen oxide (NOx) emission, improve fuel economy and suppress knock by using the… (more)

Subjects/Keywords: Exhaust Gas Recirculation; Availability; Combustion Instabilities

combustion and combustion instabilities. g) Water Induction Water is introduced into the… …have the ability to incorporate the effects of such combustion instabilities. The fraction of… …all kinds of combustion instabilities like slow burn, misfire and incomplete combustion. 2… …fluctuation. Using COVimep as the parameter for indication of combustion instabilities, Cha et al… …chamber designs. This implies that as EGR level increases it causes combustion instabilities due… 

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Shyani, R. G. (2008). Utilizing a cycle simulation to examine the use of exhaust gas recirculation (EGR) for a spark-ignition engine: including the second law of thermodynamics. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/86044

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):

Shyani, Rajeshkumar Ghanshyambhai. “Utilizing a cycle simulation to examine the use of exhaust gas recirculation (EGR) for a spark-ignition engine: including the second law of thermodynamics.” 2008. Thesis, Texas A&M University. Accessed October 22, 2019. http://hdl.handle.net/1969.1/86044.

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

MLA Handbook (7th Edition):

Shyani, Rajeshkumar Ghanshyambhai. “Utilizing a cycle simulation to examine the use of exhaust gas recirculation (EGR) for a spark-ignition engine: including the second law of thermodynamics.” 2008. Web. 22 Oct 2019.

Vancouver:

Shyani RG. Utilizing a cycle simulation to examine the use of exhaust gas recirculation (EGR) for a spark-ignition engine: including the second law of thermodynamics. [Internet] [Thesis]. Texas A&M University; 2008. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/1969.1/86044.

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

Council of Science Editors:

Shyani RG. Utilizing a cycle simulation to examine the use of exhaust gas recirculation (EGR) for a spark-ignition engine: including the second law of thermodynamics. [Thesis]. Texas A&M University; 2008. Available from: http://hdl.handle.net/1969.1/86044

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

25. Jones, Brian Keith. Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor.

Degree: MS, Mechanical Engineering, 2011, Penn State University

 To satisfy increasingly stringent environmental regulations, gas turbine engines are run in a lean premixed mode. Unfortunately, operating in this mode greatly increases the flame’s… (more)

Subjects/Keywords: premixed; flame; instabilities; lean; combustion; gas turbine

…sustained combustion instabilities. 2 1.1.1 Combustion InstabilitiesCombustion instability… …Rayleigh [3], combustion instabilities have been encountered in numerous practical… …combustion instabilities for operating conditions specified by design requirements. Otherwise, a… …combustor needs to be modified post-design stage to eliminate combustion instabilities. To obtain… …capture the complex interactions inherent in combustion instabilities and are often used to… 

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APA (6th Edition):

Jones, B. K. (2011). Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10638

Chicago Manual of Style (16th Edition):

Jones, Brian Keith. “Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor.” 2011. Masters Thesis, Penn State University. Accessed October 22, 2019. https://etda.libraries.psu.edu/catalog/10638.

MLA Handbook (7th Edition):

Jones, Brian Keith. “Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor.” 2011. Web. 22 Oct 2019.

Vancouver:

Jones BK. Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor. [Internet] [Masters thesis]. Penn State University; 2011. [cited 2019 Oct 22]. Available from: https://etda.libraries.psu.edu/catalog/10638.

Council of Science Editors:

Jones BK. Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor. [Masters Thesis]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/10638


Virginia Tech

26. Liljenberg, Scott Alan. Modeling and Stability Analysis of Thermoacoustic Instabilities in Gas Turbine Combustor Sections.

Degree: MS, Mechanical Engineering, 2000, Virginia Tech

 In order to predict the linear stability of combustion systems in industrial-scale gas turbines, a stability analysis was completed using models generated for each of… (more)

Subjects/Keywords: Combustion; Stability; Linear Systems; Acoustics; Thermoacoustic Instabilities; Time Delay

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APA (6th Edition):

Liljenberg, S. A. (2000). Modeling and Stability Analysis of Thermoacoustic Instabilities in Gas Turbine Combustor Sections. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35469

Chicago Manual of Style (16th Edition):

Liljenberg, Scott Alan. “Modeling and Stability Analysis of Thermoacoustic Instabilities in Gas Turbine Combustor Sections.” 2000. Masters Thesis, Virginia Tech. Accessed October 22, 2019. http://hdl.handle.net/10919/35469.

MLA Handbook (7th Edition):

Liljenberg, Scott Alan. “Modeling and Stability Analysis of Thermoacoustic Instabilities in Gas Turbine Combustor Sections.” 2000. Web. 22 Oct 2019.

Vancouver:

Liljenberg SA. Modeling and Stability Analysis of Thermoacoustic Instabilities in Gas Turbine Combustor Sections. [Internet] [Masters thesis]. Virginia Tech; 2000. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/10919/35469.

Council of Science Editors:

Liljenberg SA. Modeling and Stability Analysis of Thermoacoustic Instabilities in Gas Turbine Combustor Sections. [Masters Thesis]. Virginia Tech; 2000. Available from: http://hdl.handle.net/10919/35469


University of Iowa

27. Karkow, Douglas W. Combustion instabilities: an experimental investigation on the effects of hydrogen in a lean premixed combustor.

Degree: MS, Mechanical Engineering, 2012, University of Iowa

Subjects/Keywords: Combustion; Hydrogen; Instabilities; Thermo-acoustic; Mechanical Engineering

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APA (6th Edition):

Karkow, D. W. (2012). Combustion instabilities: an experimental investigation on the effects of hydrogen in a lean premixed combustor. (Masters Thesis). University of Iowa. Retrieved from https://ir.uiowa.edu/etd/2911

Chicago Manual of Style (16th Edition):

Karkow, Douglas W. “Combustion instabilities: an experimental investigation on the effects of hydrogen in a lean premixed combustor.” 2012. Masters Thesis, University of Iowa. Accessed October 22, 2019. https://ir.uiowa.edu/etd/2911.

MLA Handbook (7th Edition):

Karkow, Douglas W. “Combustion instabilities: an experimental investigation on the effects of hydrogen in a lean premixed combustor.” 2012. Web. 22 Oct 2019.

Vancouver:

Karkow DW. Combustion instabilities: an experimental investigation on the effects of hydrogen in a lean premixed combustor. [Internet] [Masters thesis]. University of Iowa; 2012. [cited 2019 Oct 22]. Available from: https://ir.uiowa.edu/etd/2911.

Council of Science Editors:

Karkow DW. Combustion instabilities: an experimental investigation on the effects of hydrogen in a lean premixed combustor. [Masters Thesis]. University of Iowa; 2012. Available from: https://ir.uiowa.edu/etd/2911


University of Central Florida

28. Pent, Jared. Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions.

Degree: 2014, University of Central Florida

 Modern gas turbine designs often include lean premixed combustion for its emissions benefits; however, this type of combustion process is susceptible to self-excited combustion instabilities(more)

Subjects/Keywords: Combustion instabilities; reacting jet in cross flow; large eddy simulations; thermoacoustics; mechanism of instability; Engineering; Mechanical Engineering

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APA (6th Edition):

Pent, J. (2014). Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions. (Doctoral Dissertation). University of Central Florida. Retrieved from https://stars.library.ucf.edu/etd/1294

Chicago Manual of Style (16th Edition):

Pent, Jared. “Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions.” 2014. Doctoral Dissertation, University of Central Florida. Accessed October 22, 2019. https://stars.library.ucf.edu/etd/1294.

MLA Handbook (7th Edition):

Pent, Jared. “Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions.” 2014. Web. 22 Oct 2019.

Vancouver:

Pent J. Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions. [Internet] [Doctoral dissertation]. University of Central Florida; 2014. [cited 2019 Oct 22]. Available from: https://stars.library.ucf.edu/etd/1294.

Council of Science Editors:

Pent J. Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions. [Doctoral Dissertation]. University of Central Florida; 2014. Available from: https://stars.library.ucf.edu/etd/1294

29. Allison, Patton Manuel. Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Partially-premixed, swirl combustion is applied in gas turbine combustors to achieve flame stabilization and reduced emission production. However, this method is also inherently sensitive to… (more)

Subjects/Keywords: Combustion Instabilities; Laser Diagnostics; Aerospace Engineering; Engineering

…leading to combustion instabilities. . . . . . . . . . . . . . . . . . Schematic showing the… …However, operation in this regime is highly susceptible to combustion instabilities. Despite the… …lining due to large pressure fluctuations. 1 Combustion instabilities present complex cases… …pressure and velocity fields, combustion instabilities can occur which result in large scale heat… …combustion instabilities. The helical motion of the 6 Figure 1.3: Isosurface of low pressure to… 

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APA (6th Edition):

Allison, P. M. (2013). Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/102385

Chicago Manual of Style (16th Edition):

Allison, Patton Manuel. “Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor.” 2013. Doctoral Dissertation, University of Michigan. Accessed October 22, 2019. http://hdl.handle.net/2027.42/102385.

MLA Handbook (7th Edition):

Allison, Patton Manuel. “Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor.” 2013. Web. 22 Oct 2019.

Vancouver:

Allison PM. Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/2027.42/102385.

Council of Science Editors:

Allison PM. Experimental Characterization of Combustion Instabilities and Flow-Flame Dynamics in a Partially-Premixed Gas Turbine Model Combustor. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/102385


Loughborough University

30. Treleaven, Nick. The numerical prediction of the acoustic response of liquid-fuelled, swirl-stabilised flames.

Degree: PhD, 2019, Loughborough University

 This thesis sets out and tests several different approaches to predicting and understanding the acoustic response of an industrially representative liquid fuelled, swirl-stabilised, lean-burn fuel… (more)

Subjects/Keywords: Engineering not elsewhere classified; combustion behavior; instabilities; RANS; URANS; Large Eddy Simulation; proper orthogonal decomposition; multi-phase flow

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APA (6th Edition):

Treleaven, N. (2019). The numerical prediction of the acoustic response of liquid-fuelled, swirl-stabilised flames. (Doctoral Dissertation). Loughborough University. Retrieved from https://doi.org/10.26174/thesis.lboro.8165990.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.785307

Chicago Manual of Style (16th Edition):

Treleaven, Nick. “The numerical prediction of the acoustic response of liquid-fuelled, swirl-stabilised flames.” 2019. Doctoral Dissertation, Loughborough University. Accessed October 22, 2019. https://doi.org/10.26174/thesis.lboro.8165990.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.785307.

MLA Handbook (7th Edition):

Treleaven, Nick. “The numerical prediction of the acoustic response of liquid-fuelled, swirl-stabilised flames.” 2019. Web. 22 Oct 2019.

Vancouver:

Treleaven N. The numerical prediction of the acoustic response of liquid-fuelled, swirl-stabilised flames. [Internet] [Doctoral dissertation]. Loughborough University; 2019. [cited 2019 Oct 22]. Available from: https://doi.org/10.26174/thesis.lboro.8165990.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.785307.

Council of Science Editors:

Treleaven N. The numerical prediction of the acoustic response of liquid-fuelled, swirl-stabilised flames. [Doctoral Dissertation]. Loughborough University; 2019. Available from: https://doi.org/10.26174/thesis.lboro.8165990.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.785307

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