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You searched for +publisher:"Georgia Tech" +contributor:("Seitzman, Jerry"). Showing records 1 – 30 of 69 total matches.

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Georgia Tech

1. Lambert, Alexander. LES of Turbulent Premixed Flame Kernel Formation and Development.

Degree: MS, Aerospace Engineering, 2020, Georgia Tech

 Spark ignition of flammable mixtures is highly sensitive to early and local conditions. Kernel formation and subsequent flame development are largely governed by turbulent conditions… (more)

Subjects/Keywords: Large Eddy Simulation; Spark Ignition; Turbulent Combustion; Computational Fluid Dynamics

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APA (6th Edition):

Lambert, A. (2020). LES of Turbulent Premixed Flame Kernel Formation and Development. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/64079

Chicago Manual of Style (16th Edition):

Lambert, Alexander. “LES of Turbulent Premixed Flame Kernel Formation and Development.” 2020. Masters Thesis, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/64079.

MLA Handbook (7th Edition):

Lambert, Alexander. “LES of Turbulent Premixed Flame Kernel Formation and Development.” 2020. Web. 11 Apr 2021.

Vancouver:

Lambert A. LES of Turbulent Premixed Flame Kernel Formation and Development. [Internet] [Masters thesis]. Georgia Tech; 2020. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/64079.

Council of Science Editors:

Lambert A. LES of Turbulent Premixed Flame Kernel Formation and Development. [Masters Thesis]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/64079


Georgia Tech

2. 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 April 11, 2021. 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. 11 Apr 2021.

Vancouver:

Sirignano MD. Experimental investigation of nitrogen oxide production in premixed reacting jets in a vitiated crossflow. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Apr 11]. 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

3. 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 April 11, 2021. 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. 11 Apr 2021.

Vancouver:

Wei S. Effect of jet fuel composition on forced ignition in gas turbine combustors. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Apr 11]. 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

4. Muraleedharan, Murali Gopal gopal. Nanoscale heat transfer effects in the combustion of nanoenergetic materials.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Metal-based composite energetic materials have substantially higher volumetric energy density when compared with monomolecular compounds such as trinitrotoluene (TNT). Micron-sized metal particles have been routinely… (more)

Subjects/Keywords: Nanoenergetic materials; Nanoscale heat transfer; Atomistic simulations; Molecular dynamics; Density functional theory

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APA (6th Edition):

Muraleedharan, M. G. g. (2018). Nanoscale heat transfer effects in the combustion of nanoenergetic materials. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62223

Chicago Manual of Style (16th Edition):

Muraleedharan, Murali Gopal gopal. “Nanoscale heat transfer effects in the combustion of nanoenergetic materials.” 2018. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/62223.

MLA Handbook (7th Edition):

Muraleedharan, Murali Gopal gopal. “Nanoscale heat transfer effects in the combustion of nanoenergetic materials.” 2018. Web. 11 Apr 2021.

Vancouver:

Muraleedharan MGg. Nanoscale heat transfer effects in the combustion of nanoenergetic materials. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/62223.

Council of Science Editors:

Muraleedharan MGg. Nanoscale heat transfer effects in the combustion of nanoenergetic materials. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/62223


Georgia Tech

5. Goh, Edwin. Reduced-order model for prediction of staged-combustor NOx emissions with detailed chemistry and finite-rate mixing.

Degree: PhD, Aerospace Engineering, 2020, Georgia Tech

 The ground power industry is targeting combined cycle plant efficiencies of 65% and above, which can be achieved primarily through higher combustor firing temperatures. Because… (more)

Subjects/Keywords: Power generation; Emissions; Chemical reactor network; Combustion; Staged combustion; Oxides of nitrogen

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APA (6th Edition):

Goh, E. (2020). Reduced-order model for prediction of staged-combustor NOx emissions with detailed chemistry and finite-rate mixing. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62848

Chicago Manual of Style (16th Edition):

Goh, Edwin. “Reduced-order model for prediction of staged-combustor NOx emissions with detailed chemistry and finite-rate mixing.” 2020. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/62848.

MLA Handbook (7th Edition):

Goh, Edwin. “Reduced-order model for prediction of staged-combustor NOx emissions with detailed chemistry and finite-rate mixing.” 2020. Web. 11 Apr 2021.

Vancouver:

Goh E. Reduced-order model for prediction of staged-combustor NOx emissions with detailed chemistry and finite-rate mixing. [Internet] [Doctoral dissertation]. Georgia Tech; 2020. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/62848.

Council of Science Editors:

Goh E. Reduced-order model for prediction of staged-combustor NOx emissions with detailed chemistry and finite-rate mixing. [Doctoral Dissertation]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/62848


Georgia Tech

6. 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 April 11, 2021. 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. 11 Apr 2021.

Vancouver:

Ochs BA. Ignition, topology, and growth of turbulent premixed flames in supersonic flows. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Apr 11]. 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


Georgia Tech

7. Amato, Alberto. Leading points concepts in turbulent premixed combustion modeling.

Degree: PhD, Mechanical Engineering, 2014, Georgia Tech

 The propagation of premixed flames in turbulent flows is a problem of wide physical and technological interest, with a significant literature on their propagation speed… (more)

Subjects/Keywords: Premixed flames; Turbulent combustion; Leading points; Flame stretch; G-equation

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APA (6th Edition):

Amato, A. (2014). Leading points concepts in turbulent premixed combustion modeling. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52247

Chicago Manual of Style (16th Edition):

Amato, Alberto. “Leading points concepts in turbulent premixed combustion modeling.” 2014. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/52247.

MLA Handbook (7th Edition):

Amato, Alberto. “Leading points concepts in turbulent premixed combustion modeling.” 2014. Web. 11 Apr 2021.

Vancouver:

Amato A. Leading points concepts in turbulent premixed combustion modeling. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/52247.

Council of Science Editors:

Amato A. Leading points concepts in turbulent premixed combustion modeling. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52247


Georgia Tech

8. Coso, Alexandra Emelina. Preparing students to incorporate stakeholder requirements in aerospace vehicle design.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The design of an aerospace vehicle system is a complex integration process driven by technological developments, stakeholder and mission needs, cost, and schedule. The vehicle… (more)

Subjects/Keywords: Aerospace vehicle design; Engineering design education; Stakeholder considerations; Space vehicles; Design; Group decision making; Multiple criteria decision making

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APA (6th Edition):

Coso, A. E. (2014). Preparing students to incorporate stakeholder requirements in aerospace vehicle design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51885

Chicago Manual of Style (16th Edition):

Coso, Alexandra Emelina. “Preparing students to incorporate stakeholder requirements in aerospace vehicle design.” 2014. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/51885.

MLA Handbook (7th Edition):

Coso, Alexandra Emelina. “Preparing students to incorporate stakeholder requirements in aerospace vehicle design.” 2014. Web. 11 Apr 2021.

Vancouver:

Coso AE. Preparing students to incorporate stakeholder requirements in aerospace vehicle design. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/51885.

Council of Science Editors:

Coso AE. Preparing students to incorporate stakeholder requirements in aerospace vehicle design. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51885


Georgia Tech

9. 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 April 11, 2021. http://hdl.handle.net/1853/59251.

MLA Handbook (7th Edition):

Gao, Xiang. “The effects of ozone addition on flame propagation and stabilization.” 2017. Web. 11 Apr 2021.

Vancouver:

Gao X. The effects of ozone addition on flame propagation and stabilization. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2021 Apr 11]. 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

10. Marshall, Andrew. Turbulent flame propagation characteristics of high hydrogen content fuels.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 Increasingly stringent pollution and emission controls have caused a rise in the use of combustors operating under lean, premixed conditions. Operating lean (excess air) lowers… (more)

Subjects/Keywords: Turbulent flames; Premixed flames; Turbulent flame speed; High hydrogen; Stretch effects; Curvature; Tangential strain rate; Leading points; Fuel effects; Low swirl burner; Particle image velocimetry; Flame topology

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APA (6th Edition):

Marshall, A. (2015). Turbulent flame propagation characteristics of high hydrogen content fuels. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53859

Chicago Manual of Style (16th Edition):

Marshall, Andrew. “Turbulent flame propagation characteristics of high hydrogen content fuels.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/53859.

MLA Handbook (7th Edition):

Marshall, Andrew. “Turbulent flame propagation characteristics of high hydrogen content fuels.” 2015. Web. 11 Apr 2021.

Vancouver:

Marshall A. Turbulent flame propagation characteristics of high hydrogen content fuels. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/53859.

Council of Science Editors:

Marshall A. Turbulent flame propagation characteristics of high hydrogen content fuels. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53859


Georgia Tech

11. Quinlan, John Mathew. Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Combustion instability due to feedback coupling between unsteady heat release and natural acoustic modes can cause catastrophic failure in liquid rocket engines and to predict… (more)

Subjects/Keywords: CI; LRE; DMD; Floquet; Floquet decomposition; FD; EFD; POD; Combustion; Stability; Instability; Acoustic; Liquid rocket; Dynamic mode decomposition; Ensemble floquet decomposition; Periodic; Vibrations; Time-varying; Eigenvalues

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APA (6th Edition):

Quinlan, J. M. (2015). Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54343

Chicago Manual of Style (16th Edition):

Quinlan, John Mathew. “Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/54343.

MLA Handbook (7th Edition):

Quinlan, John Mathew. “Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition.” 2015. Web. 11 Apr 2021.

Vancouver:

Quinlan JM. Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/54343.

Council of Science Editors:

Quinlan JM. Investigation of driving mechanisms of combustion instabilities in liquid rocket engines via the dynamic mode decomposition. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54343


Georgia Tech

12. Kundu, Reema. Impact of engine icing on jet engine compressor flow dynamics.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This previously unrecognized form of icing occurs in flights… (more)

Subjects/Keywords: Engine icing; Compressor; Jet engine; Compressible flow; Compressor stall

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APA (6th Edition):

Kundu, R. (2015). Impact of engine icing on jet engine compressor flow dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54870

Chicago Manual of Style (16th Edition):

Kundu, Reema. “Impact of engine icing on jet engine compressor flow dynamics.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/54870.

MLA Handbook (7th Edition):

Kundu, Reema. “Impact of engine icing on jet engine compressor flow dynamics.” 2015. Web. 11 Apr 2021.

Vancouver:

Kundu R. Impact of engine icing on jet engine compressor flow dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/54870.

Council of Science Editors:

Kundu R. Impact of engine icing on jet engine compressor flow dynamics. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54870


Georgia Tech

13. 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 April 11, 2021. http://hdl.handle.net/1853/55014.

MLA Handbook (7th Edition):

Caruso, Natalie R S. “Facility effects on Helicon ion thruster operation.” 2016. Web. 11 Apr 2021.

Vancouver:

Caruso NRS. Facility effects on Helicon ion thruster operation. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Apr 11]. 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

14. Smith, Andrew Gerard. Simulations of vitiated bluff body stabilized flames.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Bluff bodies have a wide range of applications where low-cost, light weight methods are needed to stabilize flames in high-speed flow. The principles of bluff… (more)

Subjects/Keywords: LES; Bluff body; Combustion

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APA (6th Edition):

Smith, A. G. (2016). Simulations of vitiated bluff body stabilized flames. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55582

Chicago Manual of Style (16th Edition):

Smith, Andrew Gerard. “Simulations of vitiated bluff body stabilized flames.” 2016. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/55582.

MLA Handbook (7th Edition):

Smith, Andrew Gerard. “Simulations of vitiated bluff body stabilized flames.” 2016. Web. 11 Apr 2021.

Vancouver:

Smith AG. Simulations of vitiated bluff body stabilized flames. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/55582.

Council of Science Editors:

Smith AG. Simulations of vitiated bluff body stabilized flames. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55582


Georgia Tech

15. Fries, Dan. Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow.

Degree: PhD, Aerospace Engineering, 2020, Georgia Tech

 Jets in crossflow are a canonical example for three-dimensional turbulent mixing. Here, non-reacting and reacting sonic jets in a supersonic crossflow are studied. The influence… (more)

Subjects/Keywords: Jet in Crossflow; Supersonic Flow; Turbulent mixing; Laser ignition; Staged jets

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APA (6th Edition):

Fries, D. (2020). Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/64095

Chicago Manual of Style (16th Edition):

Fries, Dan. “Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow.” 2020. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/64095.

MLA Handbook (7th Edition):

Fries, Dan. “Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow.” 2020. Web. 11 Apr 2021.

Vancouver:

Fries D. Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow. [Internet] [Doctoral dissertation]. Georgia Tech; 2020. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/64095.

Council of Science Editors:

Fries D. Entrainment, Mixing, and Ignition in Single and Multiple Jets in a Supersonic Crossflow. [Doctoral Dissertation]. Georgia Tech; 2020. Available from: http://hdl.handle.net/1853/64095

16. 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 April 11, 2021. http://hdl.handle.net/1853/55559.

MLA Handbook (7th Edition):

Magina, Nicholas A. “Dynamics of Harmonically Forced Nonpremixed Flames.” 2016. Web. 11 Apr 2021.

Vancouver:

Magina NA. Dynamics of Harmonically Forced Nonpremixed Flames. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Apr 11]. 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

17. Pasumarti, Venkata-Ramya. Large eddy simulation of heated pulsed jets in high speed turbulent crossflow.

Degree: MS, Aerospace Engineering, 2010, Georgia Tech

 The jet-in-crossflow problem has been extensively studied, mainly because of its applications in film cooling and injector designs. It has been established that in low-speed… (more)

Subjects/Keywords: LES; Jet in crossflow; Jet scaling; Compressible flow; Turbulent flow; Fluid dynamics; Eddies

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APA (6th Edition):

Pasumarti, V. (2010). Large eddy simulation of heated pulsed jets in high speed turbulent crossflow. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/37291

Chicago Manual of Style (16th Edition):

Pasumarti, Venkata-Ramya. “Large eddy simulation of heated pulsed jets in high speed turbulent crossflow.” 2010. Masters Thesis, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/37291.

MLA Handbook (7th Edition):

Pasumarti, Venkata-Ramya. “Large eddy simulation of heated pulsed jets in high speed turbulent crossflow.” 2010. Web. 11 Apr 2021.

Vancouver:

Pasumarti V. Large eddy simulation of heated pulsed jets in high speed turbulent crossflow. [Internet] [Masters thesis]. Georgia Tech; 2010. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/37291.

Council of Science Editors:

Pasumarti V. Large eddy simulation of heated pulsed jets in high speed turbulent crossflow. [Masters Thesis]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/37291


Georgia Tech

18. Syed, Mohmed Akil. High temperature pyrolysis and gasification of biomass and blends.

Degree: PhD, Chemical and Biomolecular Engineering, 2016, Georgia Tech

 Biomass is expected to play an important role in the future because biomass can be gasified to produce syngas for the sustainable production of electricity,… (more)

Subjects/Keywords: Biomass; Pyrolysis; Char gasification; High pressure pyrolysis; Pressurized entrained flow reactor; Sugarcane bagasse; Cane tops and leaves; CO2 gasification; Steam gasification; CO2 chemisorption; Co-gasification

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APA (6th Edition):

Syed, M. A. (2016). High temperature pyrolysis and gasification of biomass and blends. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59740

Chicago Manual of Style (16th Edition):

Syed, Mohmed Akil. “High temperature pyrolysis and gasification of biomass and blends.” 2016. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/59740.

MLA Handbook (7th Edition):

Syed, Mohmed Akil. “High temperature pyrolysis and gasification of biomass and blends.” 2016. Web. 11 Apr 2021.

Vancouver:

Syed MA. High temperature pyrolysis and gasification of biomass and blends. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/59740.

Council of Science Editors:

Syed MA. High temperature pyrolysis and gasification of biomass and blends. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/59740


Georgia Tech

19. Newalkar, Gautami. High-pressure pyrolysis and gasification of biomass.

Degree: PhD, Chemical and Biomolecular Engineering, 2015, Georgia Tech

 With the limited reserves of fossil fuels and the environmental problems associated with their use, the world is moving towards cleaner, renewable, and sustainable sources… (more)

Subjects/Keywords: Biomass; Pyrolysis; Gasification; Co-gasification; Coal; Renewable energy

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APA (6th Edition):

Newalkar, G. (2015). High-pressure pyrolysis and gasification of biomass. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53917

Chicago Manual of Style (16th Edition):

Newalkar, Gautami. “High-pressure pyrolysis and gasification of biomass.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/53917.

MLA Handbook (7th Edition):

Newalkar, Gautami. “High-pressure pyrolysis and gasification of biomass.” 2015. Web. 11 Apr 2021.

Vancouver:

Newalkar G. High-pressure pyrolysis and gasification of biomass. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/53917.

Council of Science Editors:

Newalkar G. High-pressure pyrolysis and gasification of biomass. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53917

20. Periagaram, Karthik Balasubramanian. Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 This thesis explores the effects of operating parameters on the location and shape of lifted flames in a Low Swirl Burner (LSB). In addition, it… (more)

Subjects/Keywords: Chemkin; LIF modeling; LSB; CH PLIF; Swirl combustor; Combustion engineering; Combustion; Flame stability; Gas-turbines

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APA (6th Edition):

Periagaram, K. B. (2012). Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/45828

Chicago Manual of Style (16th Edition):

Periagaram, Karthik Balasubramanian. “Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging.” 2012. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/45828.

MLA Handbook (7th Edition):

Periagaram, Karthik Balasubramanian. “Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging.” 2012. Web. 11 Apr 2021.

Vancouver:

Periagaram KB. Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/45828.

Council of Science Editors:

Periagaram KB. Determination of flame characteristics in a low swirl burner at gas turbine conditions through reaction zone imaging. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/45828

21. Williams, Logan Todd. Ion acceleration mechanisms of helicon thrusters.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 A helicon plasma source is a device that can efficiently ionize a gas to create high density, low temperature plasma. There is growing interest in… (more)

Subjects/Keywords: Ion acceleration; Ion engine; Helicon; Ion accelerators; Particle accelerators; Propulsion systems; Helicons (Electromagnetism)

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APA (6th Edition):

Williams, L. T. (2013). Ion acceleration mechanisms of helicon thrusters. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/47691

Chicago Manual of Style (16th Edition):

Williams, Logan Todd. “Ion acceleration mechanisms of helicon thrusters.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/47691.

MLA Handbook (7th Edition):

Williams, Logan Todd. “Ion acceleration mechanisms of helicon thrusters.” 2013. Web. 11 Apr 2021.

Vancouver:

Williams LT. Ion acceleration mechanisms of helicon thrusters. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/47691.

Council of Science Editors:

Williams LT. Ion acceleration mechanisms of helicon thrusters. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/47691

22. Singh, Lake Austin. Very low earth orbit propellant collection feasibility assessment.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 This work focuses on the concept of sustainable propellant collection. The concept consists of gathering ambient gas while on-orbit and using it as propellant. Propellant… (more)

Subjects/Keywords: Propellant collection; Electric propulsion; Air-breathing propulsion

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APA (6th Edition):

Singh, L. A. (2014). Very low earth orbit propellant collection feasibility assessment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53039

Chicago Manual of Style (16th Edition):

Singh, Lake Austin. “Very low earth orbit propellant collection feasibility assessment.” 2014. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/53039.

MLA Handbook (7th Edition):

Singh, Lake Austin. “Very low earth orbit propellant collection feasibility assessment.” 2014. Web. 11 Apr 2021.

Vancouver:

Singh LA. Very low earth orbit propellant collection feasibility assessment. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/53039.

Council of Science Editors:

Singh LA. Very low earth orbit propellant collection feasibility assessment. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53039

23. Kim, Jaecheol. The role of radicals supplied directly and indirectly on ignition.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The ignition process is a critical consideration for combustion devices. External energy transfer to the combustor is required for ignition in common combustion systems. There… (more)

Subjects/Keywords: High energy; OH chemiluminescence;

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APA (6th Edition):

Kim, J. (2014). The role of radicals supplied directly and indirectly on ignition. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53001

Chicago Manual of Style (16th Edition):

Kim, Jaecheol. “The role of radicals supplied directly and indirectly on ignition.” 2014. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/53001.

MLA Handbook (7th Edition):

Kim, Jaecheol. “The role of radicals supplied directly and indirectly on ignition.” 2014. Web. 11 Apr 2021.

Vancouver:

Kim J. The role of radicals supplied directly and indirectly on ignition. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/53001.

Council of Science Editors:

Kim J. The role of radicals supplied directly and indirectly on ignition. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53001

24. 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 April 11, 2021. http://hdl.handle.net/1853/53014.

MLA Handbook (7th Edition):

Sforzo, Brandon Anthony. “High energy spark ignition in non-premixed flowing combustors.” 2014. Web. 11 Apr 2021.

Vancouver:

Sforzo BA. High energy spark ignition in non-premixed flowing combustors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Apr 11]. 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

25. Gopala, Yogish. Breakup characteristics of a liquid jet in subsonic crossflow.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 This thesis describes an experimental investigation of the breakup processes involved in the formation of a spray created by a liquid jet injected into a… (more)

Subjects/Keywords: Sharp edged orifice; Primary breakup; Column breakup point; Jet in crossflow; Round edged orifice; Airplanes Motors; Reynolds number; Fluid mechanics

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APA (6th Edition):

Gopala, Y. (2012). Breakup characteristics of a liquid jet in subsonic crossflow. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44741

Chicago Manual of Style (16th Edition):

Gopala, Yogish. “Breakup characteristics of a liquid jet in subsonic crossflow.” 2012. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/44741.

MLA Handbook (7th Edition):

Gopala, Yogish. “Breakup characteristics of a liquid jet in subsonic crossflow.” 2012. Web. 11 Apr 2021.

Vancouver:

Gopala Y. Breakup characteristics of a liquid jet in subsonic crossflow. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/44741.

Council of Science Editors:

Gopala Y. Breakup characteristics of a liquid jet in subsonic crossflow. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44741

26. Korzun, Ashley Marie. Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Supersonic deceleration has been identified as a critical deficiency in extending heritage technologies to the high-mass systems required to achieve long-term exploration goals at Mars.… (more)

Subjects/Keywords: EDL; Planetary entry; Mars exploration; Retropropulsion; Opposing jets; Aerodynamics; Space vehicles Atmospheric entry; Space vehicles Atmospheric entry Mars (Planet); Aeronautics; Mars (Planet) Aeronautics

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APA (6th Edition):

Korzun, A. M. (2012). Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43667

Chicago Manual of Style (16th Edition):

Korzun, Ashley Marie. “Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent.” 2012. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/43667.

MLA Handbook (7th Edition):

Korzun, Ashley Marie. “Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent.” 2012. Web. 11 Apr 2021.

Vancouver:

Korzun AM. Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/43667.

Council of Science Editors:

Korzun AM. Aerodynamic and performance characterization of supersonic retropropulsion for application to planetary entry and descent. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/43667

27. Genin, Franklin Marie. Study of compressible turbulent flows in supersonic environment by large-eddy simulation.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 A Large-Eddy Simulation (LES) methodology adapted to the resolution of high Reynolds number turbulent flows in supersonic conditions was proposed and developed. A novel numerical… (more)

Subjects/Keywords: Hybrid numerical scheme; Compressible turbulence; LDKM closure; Eddies; Computer simulation; Combustion; Turbulence

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APA (6th Edition):

Genin, F. M. (2009). Study of compressible turbulent flows in supersonic environment by large-eddy simulation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28085

Chicago Manual of Style (16th Edition):

Genin, Franklin Marie. “Study of compressible turbulent flows in supersonic environment by large-eddy simulation.” 2009. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/28085.

MLA Handbook (7th Edition):

Genin, Franklin Marie. “Study of compressible turbulent flows in supersonic environment by large-eddy simulation.” 2009. Web. 11 Apr 2021.

Vancouver:

Genin FM. Study of compressible turbulent flows in supersonic environment by large-eddy simulation. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/28085.

Council of Science Editors:

Genin FM. Study of compressible turbulent flows in supersonic environment by large-eddy simulation. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28085

28. Sundaram, Dilip Srinivas. Multi-scale modeling of thermochemical behavior of nano-energetic materials.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Conventional energetic materials which are based on monomolecular compounds such as trinitrotoluene (TNT) have relatively low volumetric energy density. The energy density can be significantly… (more)

Subjects/Keywords: Aluminum; Nano-particle; Molecular dynamics; Energetic materials; Nanostructured materials; Nanocomposites (Materials); Thermodynamics; Propellants; Combustion

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APA (6th Edition):

Sundaram, D. S. (2013). Multi-scale modeling of thermochemical behavior of nano-energetic materials. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50225

Chicago Manual of Style (16th Edition):

Sundaram, Dilip Srinivas. “Multi-scale modeling of thermochemical behavior of nano-energetic materials.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/50225.

MLA Handbook (7th Edition):

Sundaram, Dilip Srinivas. “Multi-scale modeling of thermochemical behavior of nano-energetic materials.” 2013. Web. 11 Apr 2021.

Vancouver:

Sundaram DS. Multi-scale modeling of thermochemical behavior of nano-energetic materials. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/50225.

Council of Science Editors:

Sundaram DS. Multi-scale modeling of thermochemical behavior of nano-energetic materials. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50225

29. Emerson, Benjamin L. Dynamical characteristics of reacting bluff body wakes.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Combustion instability plagues the combustion community in a wide range of applications. This un-solved problem is especially prevalent and expensive in aerospace propulsion and ground… (more)

Subjects/Keywords: Combustion; Bluff body; Hydrodynamics; Combustion instability; Thermoacoustics; Wakes (Fluid dynamics); Aerodynamics; Combustion Stability; Flame; Hydrodyamics

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APA (6th Edition):

Emerson, B. L. (2013). Dynamical characteristics of reacting bluff body wakes. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/49073

Chicago Manual of Style (16th Edition):

Emerson, Benjamin L. “Dynamical characteristics of reacting bluff body wakes.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/49073.

MLA Handbook (7th Edition):

Emerson, Benjamin L. “Dynamical characteristics of reacting bluff body wakes.” 2013. Web. 11 Apr 2021.

Vancouver:

Emerson BL. Dynamical characteristics of reacting bluff body wakes. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/49073.

Council of Science Editors:

Emerson BL. Dynamical characteristics of reacting bluff body wakes. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/49073

30. Radhakrishnan, Arun. Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 This thesis investigates the use of the Stagnation-Point Reverse-Flow (SPRF) combustor geometry for burning low-grade solid fuels that are attractive for specific industrial applications because… (more)

Subjects/Keywords: Petroleum-coke; Solid fuels; Combustion; Combustor; SPRF; Low-grade fuel; Combustion Research; Fuel Combustion; Combustion chambers

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APA (6th Edition):

Radhakrishnan, A. (2013). Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50275

Chicago Manual of Style (16th Edition):

Radhakrishnan, Arun. “Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 11, 2021. http://hdl.handle.net/1853/50275.

MLA Handbook (7th Edition):

Radhakrishnan, Arun. “Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor.” 2013. Web. 11 Apr 2021.

Vancouver:

Radhakrishnan A. Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 11]. Available from: http://hdl.handle.net/1853/50275.

Council of Science Editors:

Radhakrishnan A. Self-sustained combustion of low grade solid fuels in a stagnation-point reverse-flow combustor. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50275

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