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You searched for +publisher:"Georgia Tech" +contributor:("Sun, Wenting"). Showing records 1 – 28 of 28 total matches.

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Georgia Tech

1. Chan, Cheong Yu. Experimental investigation of fast plasma production for the VAIPER antenna.

Degree: MS, Aerospace Engineering, 2017, Georgia Tech

 For this Master’s thesis, I will conduct the preliminary experimental study of fast plasma ignition times under varying conditions. The timing of the plasma needs… (more)

Subjects/Keywords: Plasma; Antenna

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APA (6th Edition):

Chan, C. Y. (2017). Experimental investigation of fast plasma production for the VAIPER antenna. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59307

Chicago Manual of Style (16th Edition):

Chan, Cheong Yu. “Experimental investigation of fast plasma production for the VAIPER antenna.” 2017. Masters Thesis, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/59307.

MLA Handbook (7th Edition):

Chan, Cheong Yu. “Experimental investigation of fast plasma production for the VAIPER antenna.” 2017. Web. 30 Mar 2020.

Vancouver:

Chan CY. Experimental investigation of fast plasma production for the VAIPER antenna. [Internet] [Masters thesis]. Georgia Tech; 2017. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/59307.

Council of Science Editors:

Chan CY. Experimental investigation of fast plasma production for the VAIPER antenna. [Masters Thesis]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59307


Georgia Tech

2. Lim, Chang Hyeon. Visualization of nucleation of supercritical carbon dioxide flow through a nozzle.

Degree: MS, Mechanical Engineering, 2019, Georgia Tech

 Interest in fundamental properties of carbon dioxide near the critical point led to an investigation of supercritical CO2 flow through a converging-diverging nozzle. To study… (more)

Subjects/Keywords: Supercritical CO2; High speed optical diagnostics; Two-phase flow

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APA (6th Edition):

Lim, C. H. (2019). Visualization of nucleation of supercritical carbon dioxide flow through a nozzle. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61291

Chicago Manual of Style (16th Edition):

Lim, Chang Hyeon. “Visualization of nucleation of supercritical carbon dioxide flow through a nozzle.” 2019. Masters Thesis, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61291.

MLA Handbook (7th Edition):

Lim, Chang Hyeon. “Visualization of nucleation of supercritical carbon dioxide flow through a nozzle.” 2019. Web. 30 Mar 2020.

Vancouver:

Lim CH. Visualization of nucleation of supercritical carbon dioxide flow through a nozzle. [Internet] [Masters thesis]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61291.

Council of Science Editors:

Lim CH. Visualization of nucleation of supercritical carbon dioxide flow through a nozzle. [Masters Thesis]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61291


Georgia Tech

3. Nagaraja, Sharath. Multi-scale modeling of nanosecond plasma assisted combustion.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The effect of temperature on fuel-air ignition and combustion (thermal effects) have been widely studied and well understood. However, a comprehensive understanding of nonequilibrium plasma… (more)

Subjects/Keywords: Plasma assisted combustion; Computational fluid dynamics; Nanosecond plasma discharges; Plasma modeling

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APA (6th Edition):

Nagaraja, S. (2014). Multi-scale modeling of nanosecond plasma assisted combustion. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52228

Chicago Manual of Style (16th Edition):

Nagaraja, Sharath. “Multi-scale modeling of nanosecond plasma assisted combustion.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/52228.

MLA Handbook (7th Edition):

Nagaraja, Sharath. “Multi-scale modeling of nanosecond plasma assisted combustion.” 2014. Web. 30 Mar 2020.

Vancouver:

Nagaraja S. Multi-scale modeling of nanosecond plasma assisted combustion. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/52228.

Council of Science Editors:

Nagaraja S. Multi-scale modeling of nanosecond plasma assisted combustion. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52228


Georgia Tech

4. Schulz, Joseph C. A study of magnetoplasmadynamic effects in turbulent supersonic flows with application to detonation and explosion.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Explosions are a common phenomena in the Universe. Beginning with the Big Bang, one could say the history of the Universe is narrated by a… (more)

Subjects/Keywords: Magnetohydrodynamics; Detonation; Fluid instability; Numerical methods

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APA (6th Edition):

Schulz, J. C. (2015). A study of magnetoplasmadynamic effects in turbulent supersonic flows with application to detonation and explosion. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53971

Chicago Manual of Style (16th Edition):

Schulz, Joseph C. “A study of magnetoplasmadynamic effects in turbulent supersonic flows with application to detonation and explosion.” 2015. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/53971.

MLA Handbook (7th Edition):

Schulz, Joseph C. “A study of magnetoplasmadynamic effects in turbulent supersonic flows with application to detonation and explosion.” 2015. Web. 30 Mar 2020.

Vancouver:

Schulz JC. A study of magnetoplasmadynamic effects in turbulent supersonic flows with application to detonation and explosion. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/53971.

Council of Science Editors:

Schulz JC. A study of magnetoplasmadynamic effects in turbulent supersonic flows with application to detonation and explosion. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53971


Georgia Tech

5. Caruso, Natalie R. S. Facility effects on Helicon ion thruster operation.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 In order to enable comparison of Helicon ion thruster performance across different vacuum test facilities, an understanding of the effect of operating pressure on plasma… (more)

Subjects/Keywords: Helicon ion thruster; MadHeX; Facility effects; Neutral ingestion; Magnetic nozzle; Plasma; Electric propulsion

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APA (6th Edition):

Caruso, N. R. S. (2016). Facility effects on Helicon ion thruster operation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55014

Chicago Manual of Style (16th Edition):

Caruso, Natalie R S. “Facility effects on Helicon ion thruster operation.” 2016. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/55014.

MLA Handbook (7th Edition):

Caruso, Natalie R S. “Facility effects on Helicon ion thruster operation.” 2016. Web. 30 Mar 2020.

Vancouver:

Caruso NRS. Facility effects on Helicon ion thruster operation. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/55014.

Council of Science Editors:

Caruso NRS. Facility effects on Helicon ion thruster operation. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55014


Georgia Tech

6. Wang, Xingjian. Swirling fluid mixing and combustion dynamics at supercritical conditions.

Degree: PhD, Mechanical Engineering, 2016, Georgia Tech

 A unified theoretical and numerical framework is established to study supercritical mixing and combustion over the entire range of fluid thermodynamic states of concern. Turbulence… (more)

Subjects/Keywords: Supercritical fluid; Swirl Injector; Large eddy simulation; Combustion dynamics; Flame stabilization; Liquid oxygen; Kerosene; Flamelet; Counterflow diffusion flame; S-curve

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APA (6th Edition):

Wang, X. (2016). Swirling fluid mixing and combustion dynamics at supercritical conditions. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58565

Chicago Manual of Style (16th Edition):

Wang, Xingjian. “Swirling fluid mixing and combustion dynamics at supercritical conditions.” 2016. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/58565.

MLA Handbook (7th Edition):

Wang, Xingjian. “Swirling fluid mixing and combustion dynamics at supercritical conditions.” 2016. Web. 30 Mar 2020.

Vancouver:

Wang X. Swirling fluid mixing and combustion dynamics at supercritical conditions. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/58565.

Council of Science Editors:

Wang X. Swirling fluid mixing and combustion dynamics at supercritical conditions. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/58565


Georgia Tech

7. Gao, Xiang. The effects of ozone addition on flame propagation and stabilization.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Combustion plays a vital role in transportation and power generation. However, concerns of efficiency, emission, and operations at extreme conditions highlight the needs to enhance… (more)

Subjects/Keywords: Ozone; Flame propagation; Flame stabilization; Ozonolysis

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APA (6th Edition):

Gao, X. (2017). The effects of ozone addition on flame propagation and stabilization. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59251

Chicago Manual of Style (16th Edition):

Gao, Xiang. “The effects of ozone addition on flame propagation and stabilization.” 2017. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/59251.

MLA Handbook (7th Edition):

Gao, Xiang. “The effects of ozone addition on flame propagation and stabilization.” 2017. Web. 30 Mar 2020.

Vancouver:

Gao X. The effects of ozone addition on flame propagation and stabilization. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/59251.

Council of Science Editors:

Gao X. The effects of ozone addition on flame propagation and stabilization. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59251


Georgia Tech

8. Wei, Sheng. Effect of Jet Fuel Composition on Forced Ignition in Gas Turbine Combustors.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 The rapid growth in the aviation industry means increasing consumption of jet fuels, which is leading to greater interest in alternate and sustainable fuel sources.… (more)

Subjects/Keywords: Ignition; Combustion

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APA (6th Edition):

Wei, S. (2019). Effect of Jet Fuel Composition on Forced Ignition in Gas Turbine Combustors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61204

Chicago Manual of Style (16th Edition):

Wei, Sheng. “Effect of Jet Fuel Composition on Forced Ignition in Gas Turbine Combustors.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61204.

MLA Handbook (7th Edition):

Wei, Sheng. “Effect of Jet Fuel Composition on Forced Ignition in Gas Turbine Combustors.” 2019. Web. 30 Mar 2020.

Vancouver:

Wei S. Effect of Jet Fuel Composition on Forced Ignition in Gas Turbine Combustors. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61204.

Council of Science Editors:

Wei S. Effect of Jet Fuel Composition on Forced Ignition in Gas Turbine Combustors. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61204


Georgia Tech

9. Kim, Sayop. Advancing Turbulent Spray and Combustion Models for Compression Ignition Engine Simulations.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 This thesis seeks to investigate the turbulent mixing influence on spray atomization and combustion processes encountered in compression ignition diesel engines. Despite greater thermal efficiency… (more)

Subjects/Keywords: Diesel Engine; CFD; Spray Modeling; Turbulence-Chemistry Interaction; Combustion Modeling

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APA (6th Edition):

Kim, S. (2019). Advancing Turbulent Spray and Combustion Models for Compression Ignition Engine Simulations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61216

Chicago Manual of Style (16th Edition):

Kim, Sayop. “Advancing Turbulent Spray and Combustion Models for Compression Ignition Engine Simulations.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61216.

MLA Handbook (7th Edition):

Kim, Sayop. “Advancing Turbulent Spray and Combustion Models for Compression Ignition Engine Simulations.” 2019. Web. 30 Mar 2020.

Vancouver:

Kim S. Advancing Turbulent Spray and Combustion Models for Compression Ignition Engine Simulations. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61216.

Council of Science Editors:

Kim S. Advancing Turbulent Spray and Combustion Models for Compression Ignition Engine Simulations. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61216


Georgia Tech

10. Sirignano, Matthew Davis. Experimental Investigation of Nitrogen Oxide Production in Premixed Reacting Jets in a Vitiated Crossflow.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 The presented work describes the experimental investigation of nitrogen oxide (NOx) emissions from reacting jets in a vitiated crossflow (RJICF). It is motivated by interest… (more)

Subjects/Keywords: NOx Emissions; Gas Turbines; Axial Staging; Reacting Jet in Crossflow; Flame Lifting; Hydrodynamic Stability

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APA (6th Edition):

Sirignano, M. D. (2019). Experimental Investigation of Nitrogen Oxide Production in Premixed Reacting Jets in a Vitiated Crossflow. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62291

Chicago Manual of Style (16th Edition):

Sirignano, Matthew Davis. “Experimental Investigation of Nitrogen Oxide Production in Premixed Reacting Jets in a Vitiated Crossflow.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/62291.

MLA Handbook (7th Edition):

Sirignano, Matthew Davis. “Experimental Investigation of Nitrogen Oxide Production in Premixed Reacting Jets in a Vitiated Crossflow.” 2019. Web. 30 Mar 2020.

Vancouver:

Sirignano MD. Experimental Investigation of Nitrogen Oxide Production in Premixed Reacting Jets in a Vitiated Crossflow. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/62291.

Council of Science Editors:

Sirignano MD. Experimental Investigation of Nitrogen Oxide Production in Premixed Reacting Jets in a Vitiated Crossflow. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62291


Georgia Tech

11. Karimi, Miad. INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 This thesis reports methane (CH4) and a syngas mixture (H2/CO=95:5) autoignition delay measurements relevant to operating conditions of supercritical carbon dioxide (sCO2) power cycle (100… (more)

Subjects/Keywords: High-Pressure Ignition Delay Times; Chemical Kinetics; Supercritical CO2

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APA (6th Edition):

Karimi, M. (2019). INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62295

Chicago Manual of Style (16th Edition):

Karimi, Miad. “INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/62295.

MLA Handbook (7th Edition):

Karimi, Miad. “INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES.” 2019. Web. 30 Mar 2020.

Vancouver:

Karimi M. INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/62295.

Council of Science Editors:

Karimi M. INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62295


Georgia Tech

12. Ochs, Bradley Alan. Ignition, Topology, and Growth of Turbulent Premixed Flames in Supersonic Flows.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Supersonic combustion ramjets (scramjets) are currently the most efficient combustor technology for air breathing hypersonic flight, however, lack of fundamental understanding and numerous engineering challenges… (more)

Subjects/Keywords: Hypersonics; supersonic flows; supersonic combustion; laser ignition; turbulent flames; premixed flames

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APA (6th Edition):

Ochs, B. A. (2019). Ignition, Topology, and Growth of Turbulent Premixed Flames in Supersonic Flows. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62313

Chicago Manual of Style (16th Edition):

Ochs, Bradley Alan. “Ignition, Topology, and Growth of Turbulent Premixed Flames in Supersonic Flows.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/62313.

MLA Handbook (7th Edition):

Ochs, Bradley Alan. “Ignition, Topology, and Growth of Turbulent Premixed Flames in Supersonic Flows.” 2019. Web. 30 Mar 2020.

Vancouver:

Ochs BA. Ignition, Topology, and Growth of Turbulent Premixed Flames in Supersonic Flows. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/62313.

Council of Science Editors:

Ochs BA. Ignition, Topology, and Growth of Turbulent Premixed Flames in Supersonic Flows. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62313

13. Gallagher, Timothy. Towards multi-scale reacting fluid-structure interaction: micro-scale structural modeling.

Degree: MS, Aerospace Engineering, 2015, Georgia Tech

 The fluid-structure interaction of reacting materials requires computational models capable of resolving the wide range of scales present in both the condensed phase energetic materials… (more)

Subjects/Keywords: Explosives simulation

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APA (6th Edition):

Gallagher, T. (2015). Towards multi-scale reacting fluid-structure interaction: micro-scale structural modeling. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53483

Chicago Manual of Style (16th Edition):

Gallagher, Timothy. “Towards multi-scale reacting fluid-structure interaction: micro-scale structural modeling.” 2015. Masters Thesis, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/53483.

MLA Handbook (7th Edition):

Gallagher, Timothy. “Towards multi-scale reacting fluid-structure interaction: micro-scale structural modeling.” 2015. Web. 30 Mar 2020.

Vancouver:

Gallagher T. Towards multi-scale reacting fluid-structure interaction: micro-scale structural modeling. [Internet] [Masters thesis]. Georgia Tech; 2015. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/53483.

Council of Science Editors:

Gallagher T. Towards multi-scale reacting fluid-structure interaction: micro-scale structural modeling. [Masters Thesis]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53483

14. Magina, Nicholas A. Dynamics of Harmonically Forced Nonpremixed Flames.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 This thesis describes the dynamics, both spatio-temporal and heat release, of harmonically excited non-premixed flames. Analytical, numerical, computational, and, experimental analyses were performed, along with… (more)

Subjects/Keywords: Non-premixed flame; Diffusion flame; Linear flame response dynamics; Velocity coupled response; Combustion instabilities; Flame transfer function

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APA (6th Edition):

Magina, N. A. (2016). Dynamics of Harmonically Forced Nonpremixed Flames. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55559

Chicago Manual of Style (16th Edition):

Magina, Nicholas A. “Dynamics of Harmonically Forced Nonpremixed Flames.” 2016. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/55559.

MLA Handbook (7th Edition):

Magina, Nicholas A. “Dynamics of Harmonically Forced Nonpremixed Flames.” 2016. Web. 30 Mar 2020.

Vancouver:

Magina NA. Dynamics of Harmonically Forced Nonpremixed Flames. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/55559.

Council of Science Editors:

Magina NA. Dynamics of Harmonically Forced Nonpremixed Flames. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55559

15. Dasgupta, Debolina. Turbulence-chemistry interactions for lean premixed flames.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Turbulent combustion, particularly premixed combustion has great practical importance due to their extensive industrial usage in gas turbines, internal combustion engines etc. However, the physics… (more)

Subjects/Keywords: Premixed flames; Turbulent combustion; Turbulence-chemistry interactions; Combustion modeling; Numerical combustion

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APA (6th Edition):

Dasgupta, D. (2018). Turbulence-chemistry interactions for lean premixed flames. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60746

Chicago Manual of Style (16th Edition):

Dasgupta, Debolina. “Turbulence-chemistry interactions for lean premixed flames.” 2018. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/60746.

MLA Handbook (7th Edition):

Dasgupta, Debolina. “Turbulence-chemistry interactions for lean premixed flames.” 2018. Web. 30 Mar 2020.

Vancouver:

Dasgupta D. Turbulence-chemistry interactions for lean premixed flames. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/60746.

Council of Science Editors:

Dasgupta D. Turbulence-chemistry interactions for lean premixed flames. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60746

16. Humphrey, Luke. Ensemble-averaged dynamics of premixed, turbulent, harmonically excited flames.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Increasing awareness of the negative impacts of pollutant emissions associated with combustion is driving increasingly stringent regulatory limits. In particular, oxides of nitrogen, generally referred… (more)

Subjects/Keywords: Turbulent flame speed; Ensemble-averaged; Premixed flames

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APA (6th Edition):

Humphrey, L. (2017). Ensemble-averaged dynamics of premixed, turbulent, harmonically excited flames. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59784

Chicago Manual of Style (16th Edition):

Humphrey, Luke. “Ensemble-averaged dynamics of premixed, turbulent, harmonically excited flames.” 2017. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/59784.

MLA Handbook (7th Edition):

Humphrey, Luke. “Ensemble-averaged dynamics of premixed, turbulent, harmonically excited flames.” 2017. Web. 30 Mar 2020.

Vancouver:

Humphrey L. Ensemble-averaged dynamics of premixed, turbulent, harmonically excited flames. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/59784.

Council of Science Editors:

Humphrey L. Ensemble-averaged dynamics of premixed, turbulent, harmonically excited flames. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59784

17. Liu, Connie Y. Investigating physics of nanosecond-pulsed argon plasma discharges for a VLF plasma antenna.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Very low frequency (VLF) waves (3-30 kHz) are useful in communication and navigation, can deeply penetrate the ground and ocean surface, and help with satellite… (more)

Subjects/Keywords: Plasma; Antenna; Nanosecond ionization; OES; VLF

…the first people I met at Georgia Tech, and I am so appreciative of the adventures we have… 

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APA (6th Edition):

Liu, C. Y. (2019). Investigating physics of nanosecond-pulsed argon plasma discharges for a VLF plasma antenna. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61753

Chicago Manual of Style (16th Edition):

Liu, Connie Y. “Investigating physics of nanosecond-pulsed argon plasma discharges for a VLF plasma antenna.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61753.

MLA Handbook (7th Edition):

Liu, Connie Y. “Investigating physics of nanosecond-pulsed argon plasma discharges for a VLF plasma antenna.” 2019. Web. 30 Mar 2020.

Vancouver:

Liu CY. Investigating physics of nanosecond-pulsed argon plasma discharges for a VLF plasma antenna. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61753.

Council of Science Editors:

Liu CY. Investigating physics of nanosecond-pulsed argon plasma discharges for a VLF plasma antenna. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61753

18. Sforzo, Brandon Anthony. High energy spark ignition in non-premixed flowing combustors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 In many practical combustion devices, including those used in gas turbine engines for aircraft and power generation, a high energy spark kernel is necessary to… (more)

Subjects/Keywords: Ignition; Combustion; Experimental; Numerical; Gas turbines

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APA (6th Edition):

Sforzo, B. A. (2014). High energy spark ignition in non-premixed flowing combustors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53014

Chicago Manual of Style (16th Edition):

Sforzo, Brandon Anthony. “High energy spark ignition in non-premixed flowing combustors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/53014.

MLA Handbook (7th Edition):

Sforzo, Brandon Anthony. “High energy spark ignition in non-premixed flowing combustors.” 2014. Web. 30 Mar 2020.

Vancouver:

Sforzo BA. High energy spark ignition in non-premixed flowing combustors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/53014.

Council of Science Editors:

Sforzo BA. High energy spark ignition in non-premixed flowing combustors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53014

19. Knox, Benjamin W. End-of-injection effects on diesel spray combustion.

Degree: PhD, Mechanical Engineering, 2016, Georgia Tech

 Increasingly stringent emissions regulations have created a demand for cleaner burning engines. Low-temperature combustion (LTC) strategies have been proposed to meet low soot and nitrogen… (more)

Subjects/Keywords: Diesel; Combustion; Spray; Kinetics; Ignition; Fuel; Engine; Flame; Fluids; Injection

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APA (6th Edition):

Knox, B. W. (2016). End-of-injection effects on diesel spray combustion. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56274

Chicago Manual of Style (16th Edition):

Knox, Benjamin W. “End-of-injection effects on diesel spray combustion.” 2016. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/56274.

MLA Handbook (7th Edition):

Knox, Benjamin W. “End-of-injection effects on diesel spray combustion.” 2016. Web. 30 Mar 2020.

Vancouver:

Knox BW. End-of-injection effects on diesel spray combustion. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/56274.

Council of Science Editors:

Knox BW. End-of-injection effects on diesel spray combustion. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56274

20. Frieman, Jason David. Characterization of background neutral flows in vacuum test facilities and impacts on hall effect thruster operation.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Hall effect thrusters (HETs) are a type of electrostatic electric propulsion device characterized by high specific impulses, thrust efficiencies, and thrust densities. These performance attributes… (more)

Subjects/Keywords: Hall effect thrusters; Electric propulsion; Facility effects; Vacuum test facilities

…you enough for all the adventures and laughs we have shared throughout my time at Georgia… …Tech. To my parents Jan and Ron Frieman, you always encouraged me to get an education and… 

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APA (6th Edition):

Frieman, J. D. (2017). Characterization of background neutral flows in vacuum test facilities and impacts on hall effect thruster operation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58650

Chicago Manual of Style (16th Edition):

Frieman, Jason David. “Characterization of background neutral flows in vacuum test facilities and impacts on hall effect thruster operation.” 2017. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/58650.

MLA Handbook (7th Edition):

Frieman, Jason David. “Characterization of background neutral flows in vacuum test facilities and impacts on hall effect thruster operation.” 2017. Web. 30 Mar 2020.

Vancouver:

Frieman JD. Characterization of background neutral flows in vacuum test facilities and impacts on hall effect thruster operation. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/58650.

Council of Science Editors:

Frieman JD. Characterization of background neutral flows in vacuum test facilities and impacts on hall effect thruster operation. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58650

21. Yang, Suo. Effects of detailed finite rate chemistry in turbulent combustion.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The development of advanced combustion energy-conversion systems requires accurate simulation tools, such as Direct Numerical Simulation (DNS) and Large Eddy Simulation (LES), for capturing and… (more)

Subjects/Keywords: Turbulent combustion; Chemical kinetics; Modeling and simulation; Finite-rate effects; Extinction and ignition

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APA (6th Edition):

Yang, S. (2017). Effects of detailed finite rate chemistry in turbulent combustion. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58672

Chicago Manual of Style (16th Edition):

Yang, Suo. “Effects of detailed finite rate chemistry in turbulent combustion.” 2017. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/58672.

MLA Handbook (7th Edition):

Yang, Suo. “Effects of detailed finite rate chemistry in turbulent combustion.” 2017. Web. 30 Mar 2020.

Vancouver:

Yang S. Effects of detailed finite rate chemistry in turbulent combustion. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/58672.

Council of Science Editors:

Yang S. Effects of detailed finite rate chemistry in turbulent combustion. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58672

22. Raghunandan, Pratibha. A numerical study on non-equilibrium multi-temperature thermo-chemistry.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 The accurate computation of hypersonic flowfields is an ongoing endeavor and is important for the accurate prediction of heat transfer and space vehicle design. The… (more)

Subjects/Keywords: Non-equilibrium; Multi-temperature modeling

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APA (6th Edition):

Raghunandan, P. (2019). A numerical study on non-equilibrium multi-temperature thermo-chemistry. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61243

Chicago Manual of Style (16th Edition):

Raghunandan, Pratibha. “A numerical study on non-equilibrium multi-temperature thermo-chemistry.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61243.

MLA Handbook (7th Edition):

Raghunandan, Pratibha. “A numerical study on non-equilibrium multi-temperature thermo-chemistry.” 2019. Web. 30 Mar 2020.

Vancouver:

Raghunandan P. A numerical study on non-equilibrium multi-temperature thermo-chemistry. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61243.

Council of Science Editors:

Raghunandan P. A numerical study on non-equilibrium multi-temperature thermo-chemistry. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61243

23. Adusumilli, Sampath. Effects of preheat temperature and vitiation on reaction kinetics of higher hydrocarbon fuels.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Conducting full-scale experiments as part of the design process of jet engine combustors is a costly and time-consuming process. Therefore engine developers have been increasingly… (more)

Subjects/Keywords: Laminar flow; Flame speed; Jet fuels; Reaction kinetics; Alkenes; Stretch sensitivity; Rate coefficients; Reaction rates; Vitiation; Preheat temperature; Hydrocarbon fuels

…The badminton club at Georgia Tech served as an essential distraction and kept me… 

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APA (6th Edition):

Adusumilli, S. (2019). Effects of preheat temperature and vitiation on reaction kinetics of higher hydrocarbon fuels. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61803

Chicago Manual of Style (16th Edition):

Adusumilli, Sampath. “Effects of preheat temperature and vitiation on reaction kinetics of higher hydrocarbon fuels.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61803.

MLA Handbook (7th Edition):

Adusumilli, Sampath. “Effects of preheat temperature and vitiation on reaction kinetics of higher hydrocarbon fuels.” 2019. Web. 30 Mar 2020.

Vancouver:

Adusumilli S. Effects of preheat temperature and vitiation on reaction kinetics of higher hydrocarbon fuels. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61803.

Council of Science Editors:

Adusumilli S. Effects of preheat temperature and vitiation on reaction kinetics of higher hydrocarbon fuels. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61803

24. Pidaparti, Sandeep R. Heat transfer and fluid flow characteristics of supercritical carbon dioxide flow.

Degree: PhD, Mechanical Engineering, 2019, Georgia Tech

 The goal of this dissertation is to enhance the fundamental understanding of heat transfer phenomenon of sCO2 especially near the critical point and to investigate… (more)

Subjects/Keywords: Heat transfer; Supercritical carbon dioxide; Printed circuit heat exchangers

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APA (6th Edition):

Pidaparti, S. R. (2019). Heat transfer and fluid flow characteristics of supercritical carbon dioxide flow. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61805

Chicago Manual of Style (16th Edition):

Pidaparti, Sandeep R. “Heat transfer and fluid flow characteristics of supercritical carbon dioxide flow.” 2019. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/61805.

MLA Handbook (7th Edition):

Pidaparti, Sandeep R. “Heat transfer and fluid flow characteristics of supercritical carbon dioxide flow.” 2019. Web. 30 Mar 2020.

Vancouver:

Pidaparti SR. Heat transfer and fluid flow characteristics of supercritical carbon dioxide flow. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/61805.

Council of Science Editors:

Pidaparti SR. Heat transfer and fluid flow characteristics of supercritical carbon dioxide flow. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61805

25. Langendorf, Samuel J. Effects of electron emission on plasma sheaths.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Current state-of-the-art plasma thrusters are limited in power density and thrust density by power losses to plasma-facing walls and electrodes. In the case of Hall… (more)

Subjects/Keywords: Hall effect thruster; Plasma; Plasma-wall interactions; Plasma sheath; Electric propulsion

…GEO Geosynchronous Earth Orbit GT Georgia Institute of Technology GTRI Georgia Tech… 

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APA (6th Edition):

Langendorf, S. J. (2015). Effects of electron emission on plasma sheaths. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54383

Chicago Manual of Style (16th Edition):

Langendorf, Samuel J. “Effects of electron emission on plasma sheaths.” 2015. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/54383.

MLA Handbook (7th Edition):

Langendorf, Samuel J. “Effects of electron emission on plasma sheaths.” 2015. Web. 30 Mar 2020.

Vancouver:

Langendorf SJ. Effects of electron emission on plasma sheaths. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/54383.

Council of Science Editors:

Langendorf SJ. Effects of electron emission on plasma sheaths. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54383

26. Kochar, Yash N. Laminar flame speed and stretch sensitivity of hydrocarbon fuels at high preheat, pressure and vitiation.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 This thesis investigates the laminar flame speed of C₁-C₃ alkanes and their binary mixtures at conditions of interest in natural gas based gas turbines viz.… (more)

Subjects/Keywords: Gas turbines; Laminar flame speed; High temperature; High pressure; Nitrogen dilution; Carbon dioxide dilution; Steam dilution; Helium dilution; Natural gas; Methane; Ethane; Propane; Chemical kinetics; Scaling rules

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APA (6th Edition):

Kochar, Y. N. (2014). Laminar flame speed and stretch sensitivity of hydrocarbon fuels at high preheat, pressure and vitiation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52216

Chicago Manual of Style (16th Edition):

Kochar, Yash N. “Laminar flame speed and stretch sensitivity of hydrocarbon fuels at high preheat, pressure and vitiation.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/52216.

MLA Handbook (7th Edition):

Kochar, Yash N. “Laminar flame speed and stretch sensitivity of hydrocarbon fuels at high preheat, pressure and vitiation.” 2014. Web. 30 Mar 2020.

Vancouver:

Kochar YN. Laminar flame speed and stretch sensitivity of hydrocarbon fuels at high preheat, pressure and vitiation. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/52216.

Council of Science Editors:

Kochar YN. Laminar flame speed and stretch sensitivity of hydrocarbon fuels at high preheat, pressure and vitiation. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52216

27. Walker, Jonathan A. Electrical facility effects on Hall effect thrusters.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The Hall effect thruster (HET) is a type of spacecraft propulsion that is used for satellite orbit raising and station keeping. HET development and lifetime… (more)

Subjects/Keywords: Facility effects; Hall effect thruster; Hall effect thrusters; Electric propulsion; Spacecraft propulsion

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APA (6th Edition):

Walker, J. A. (2016). Electrical facility effects on Hall effect thrusters. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56347

Chicago Manual of Style (16th Edition):

Walker, Jonathan A. “Electrical facility effects on Hall effect thrusters.” 2016. Doctoral Dissertation, Georgia Tech. Accessed March 30, 2020. http://hdl.handle.net/1853/56347.

MLA Handbook (7th Edition):

Walker, Jonathan A. “Electrical facility effects on Hall effect thrusters.” 2016. Web. 30 Mar 2020.

Vancouver:

Walker JA. Electrical facility effects on Hall effect thrusters. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Mar 30]. Available from: http://hdl.handle.net/1853/56347.

Council of Science Editors:

Walker JA. Electrical facility effects on Hall effect thrusters. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56347

28. 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 March 30, 2020. http://hdl.handle.net/1853/59252.

MLA Handbook (7th Edition):

Smith, Travis Edward. “Experimental investigation of transverse acoustic instabilities.” 2017. Web. 30 Mar 2020.

Vancouver:

Smith TE. Experimental investigation of transverse acoustic instabilities. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2020 Mar 30]. 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

.