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

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Georgia Tech

1. 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 February 17, 2020. http://hdl.handle.net/1853/52247.

MLA Handbook (7th Edition):

Amato, Alberto. “Leading points concepts in turbulent premixed combustion modeling.” 2014. Web. 17 Feb 2020.

Vancouver:

Amato A. Leading points concepts in turbulent premixed combustion modeling. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Feb 17]. 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

2. Khare, Prashant. Breakup of liquid droplets.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Liquid droplet breakup and dynamics is a phenomena of immense practical importance in a wide variety of applications in science and engineering. Albeit, researchers have… (more)

Subjects/Keywords: Liquid droplets; VOF; Bag breakup; Multimode breakup; Oscillatory breakup; Shear breakup

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APA (6th Edition):

Khare, P. (2013). Breakup of liquid droplets. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53395

Chicago Manual of Style (16th Edition):

Khare, Prashant. “Breakup of liquid droplets.” 2013. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/53395.

MLA Handbook (7th Edition):

Khare, Prashant. “Breakup of liquid droplets.” 2013. Web. 17 Feb 2020.

Vancouver:

Khare P. Breakup of liquid droplets. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/53395.

Council of Science Editors:

Khare P. Breakup of liquid droplets. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/53395


Georgia Tech

3. 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 February 17, 2020. http://hdl.handle.net/1853/58565.

MLA Handbook (7th Edition):

Wang, Xingjian. “Swirling fluid mixing and combustion dynamics at supercritical conditions.” 2016. Web. 17 Feb 2020.

Vancouver:

Wang X. Swirling fluid mixing and combustion dynamics at supercritical conditions. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Feb 17]. 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

4. Jain, Nishant. COMBUSTION AND FLOW CHARACTERISTICS OF STAGED COMBUSTORS INVOLVING CONFINED JETS IN CROSSFLOW.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Staged combustion offers many advantages in high performance aero-propulsion and power generation applications of gas turbine engines. For example, staged combustors can operate at low… (more)

Subjects/Keywords: Combustion; flow; jet in crossflow; JICF; multiple confined jets in crossflow; CJICF; RQL; LQL; staged combustion; crossflow; jets; fluid mechanics; flame; characteristics; mixing; low emissions; velocity field; gas turbine; propulsion

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APA (6th Edition):

Jain, N. (2019). COMBUSTION AND FLOW CHARACTERISTICS OF STAGED COMBUSTORS INVOLVING CONFINED JETS IN CROSSFLOW. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61213

Chicago Manual of Style (16th Edition):

Jain, Nishant. “COMBUSTION AND FLOW CHARACTERISTICS OF STAGED COMBUSTORS INVOLVING CONFINED JETS IN CROSSFLOW.” 2019. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/61213.

MLA Handbook (7th Edition):

Jain, Nishant. “COMBUSTION AND FLOW CHARACTERISTICS OF STAGED COMBUSTORS INVOLVING CONFINED JETS IN CROSSFLOW.” 2019. Web. 17 Feb 2020.

Vancouver:

Jain N. COMBUSTION AND FLOW CHARACTERISTICS OF STAGED COMBUSTORS INVOLVING CONFINED JETS IN CROSSFLOW. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/61213.

Council of Science Editors:

Jain N. COMBUSTION AND FLOW CHARACTERISTICS OF STAGED COMBUSTORS INVOLVING CONFINED JETS IN CROSSFLOW. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61213


Georgia Tech

5. Li, Yixing. High-fidelity numerical simulation and emulation of bi-fluid swirl injector flow and combustion dynamics.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Injectors are critical components of combustion devices in liquid-fueled propulsion systems. By controlling the atomization and mixing of propellants, injectors can affect combustion efficiency, dynamic… (more)

Subjects/Keywords: Large Eddy simulation; Emulation

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APA (6th Edition):

Li, Y. (2019). High-fidelity numerical simulation and emulation of bi-fluid swirl injector flow and combustion dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61698

Chicago Manual of Style (16th Edition):

Li, Yixing. “High-fidelity numerical simulation and emulation of bi-fluid swirl injector flow and combustion dynamics.” 2019. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/61698.

MLA Handbook (7th Edition):

Li, Yixing. “High-fidelity numerical simulation and emulation of bi-fluid swirl injector flow and combustion dynamics.” 2019. Web. 17 Feb 2020.

Vancouver:

Li Y. High-fidelity numerical simulation and emulation of bi-fluid swirl injector flow and combustion dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/61698.

Council of Science Editors:

Li Y. High-fidelity numerical simulation and emulation of bi-fluid swirl injector flow and combustion dynamics. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61698


Georgia Tech

6. Rock, Nicholas. Lean blowout sensitivities of complex liquid fuels.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Lean blowout is a process whereby a previously stable flame is either extinguished or convected out of its combustor. In aviation applications, blowout is a… (more)

Subjects/Keywords: Lean blowout; Alternative jet fuels; Extinction and re-ignition

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APA (6th Edition):

Rock, N. (2019). Lean blowout sensitivities of complex liquid fuels. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61726

Chicago Manual of Style (16th Edition):

Rock, Nicholas. “Lean blowout sensitivities of complex liquid fuels.” 2019. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/61726.

MLA Handbook (7th Edition):

Rock, Nicholas. “Lean blowout sensitivities of complex liquid fuels.” 2019. Web. 17 Feb 2020.

Vancouver:

Rock N. Lean blowout sensitivities of complex liquid fuels. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/61726.

Council of Science Editors:

Rock N. Lean blowout sensitivities of complex liquid fuels. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61726


Georgia Tech

7. Schrader, Andrew J. Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power.

Degree: PhD, Mechanical Engineering, 2019, Georgia Tech

 Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power Andrew J. Schrader 182 Pages Directed by Dr. Peter… (more)

Subjects/Keywords: Solar Thermochemistry; Granular Flow; Concentrated Solar Power; Reactor

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APA (6th Edition):

Schrader, A. J. (2019). Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62282

Chicago Manual of Style (16th Edition):

Schrader, Andrew J. “Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power.” 2019. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/62282.

MLA Handbook (7th Edition):

Schrader, Andrew J. “Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power.” 2019. Web. 17 Feb 2020.

Vancouver:

Schrader AJ. Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/62282.

Council of Science Editors:

Schrader AJ. Design, Modeling, and Testing of a Solar Thermochemical Inclined Granular Flow Reactor for Concentrated Solar Power. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62282


Georgia Tech

8. 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 February 17, 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. 17 Feb 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 Feb 17]. 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

9. 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 February 17, 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. 17 Feb 2020.

Vancouver:

Karimi M. INVESTIGATION OF HIGH-PRESSURE METHANE AND SYNGAS AUTOIGNITION DELAY TIMES. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2020 Feb 17]. 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

10. Axdahl, Erik Lee. A study of premixed, shock-induced combustion with application to hypervelocity flight.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 One of the current goals of research in hypersonic, airbreathing propulsion is access to higher Mach numbers. A strong driver of this goal is the… (more)

Subjects/Keywords: PMSIC; Combustion; Hypervelocity; Hypersonic; Injection; Hypersonic planes; Aerodynamics, Hypersonic; Combustion; Mach number; Aerodynamics; Aerodynamics, Supersonic; Airplanes Scramjet engines

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APA (6th Edition):

Axdahl, E. L. (2013). A study of premixed, shock-induced combustion with application to hypervelocity flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50290

Chicago Manual of Style (16th Edition):

Axdahl, Erik Lee. “A study of premixed, shock-induced combustion with application to hypervelocity flight.” 2013. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/50290.

MLA Handbook (7th Edition):

Axdahl, Erik Lee. “A study of premixed, shock-induced combustion with application to hypervelocity flight.” 2013. Web. 17 Feb 2020.

Vancouver:

Axdahl EL. A study of premixed, shock-induced combustion with application to hypervelocity flight. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/50290.

Council of Science Editors:

Axdahl EL. A study of premixed, shock-induced combustion with application to hypervelocity flight. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50290

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

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

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

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

…had over my time here at Georgia Tech. In no particular order, I would like to thank Manisha… 

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

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

MLA Handbook (7th Edition):

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

Vancouver:

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

Council of Science Editors:

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

12. 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 February 17, 2020. 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. 17 Feb 2020.

Vancouver:

Sundaram DS. Multi-scale modeling of thermochemical behavior of nano-energetic materials. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Feb 17]. 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

13. 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 February 17, 2020. 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. 17 Feb 2020.

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 2020 Feb 17]. 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

14. 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 February 17, 2020. http://hdl.handle.net/1853/49073.

MLA Handbook (7th Edition):

Emerson, Benjamin L. “Dynamical characteristics of reacting bluff body wakes.” 2013. Web. 17 Feb 2020.

Vancouver:

Emerson BL. Dynamical characteristics of reacting bluff body wakes. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Feb 17]. 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

15. Scarborough, David E. An experimental and theoretical investigation of a fuel system tuner for the suppression of combustion driven oscillations.

Degree: PhD, Mechanical Engineering, 2010, Georgia Tech

 Manufacturers of commercial, power-generating, gas turbine engines continue to develop combustors that produce lower emissions of nitrogen oxides (NOx) in order to meet the environmental… (more)

Subjects/Keywords: Power generation; Gas turbine; Tuner; Fuel system; Acoustic impedance; Combustion instabilities; Oscillations; Damping (Mechanics); Gas-turbines Fuel systems; Combustion

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APA (6th Edition):

Scarborough, D. E. (2010). An experimental and theoretical investigation of a fuel system tuner for the suppression of combustion driven oscillations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/33838

Chicago Manual of Style (16th Edition):

Scarborough, David E. “An experimental and theoretical investigation of a fuel system tuner for the suppression of combustion driven oscillations.” 2010. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/33838.

MLA Handbook (7th Edition):

Scarborough, David E. “An experimental and theoretical investigation of a fuel system tuner for the suppression of combustion driven oscillations.” 2010. Web. 17 Feb 2020.

Vancouver:

Scarborough DE. An experimental and theoretical investigation of a fuel system tuner for the suppression of combustion driven oscillations. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/33838.

Council of Science Editors:

Scarborough DE. An experimental and theoretical investigation of a fuel system tuner for the suppression of combustion driven oscillations. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/33838

16. Shreekrishna. Response mechanisms of attached premixed flames to harmonic forcing.

Degree: PhD, Aerospace Engineering, 2011, Georgia Tech

 The persistent thrust for a cleaner, greener environment has prompted air pollution regulations to be enforced with increased stringency by environmental protection bodies all over… (more)

Subjects/Keywords: Reduced order modeling; Flame transfer function; G-equation; Flame response; Combustion dynamics; Gas turbines; Thermoacoustic instabilities; Combustion instabilities; Gas-turbines; Aircraft gas-turbines; Combustion engineering

…all the great times that we have spent together. My last year at Georgia Tech was absolutely… …providing me with the culture of my country and hometown very close to Georgia Tech, that I would… 

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APA (6th Edition):

Shreekrishna. (2011). Response mechanisms of attached premixed flames to harmonic forcing. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/42759

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16th Edition):

Shreekrishna. “Response mechanisms of attached premixed flames to harmonic forcing.” 2011. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/42759.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7th Edition):

Shreekrishna. “Response mechanisms of attached premixed flames to harmonic forcing.” 2011. Web. 17 Feb 2020.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

Shreekrishna. Response mechanisms of attached premixed flames to harmonic forcing. [Internet] [Doctoral dissertation]. Georgia Tech; 2011. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/42759.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

Shreekrishna. Response mechanisms of attached premixed flames to harmonic forcing. [Doctoral Dissertation]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/42759

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

17. Cross, Caleb Nathaniel. Combustion heat release effects on asymmetric vortex shedding from bluff bodies.

Degree: PhD, Mechanical Engineering, 2011, Georgia Tech

 Combustion systems utilizing bluff bodies to stabilize the combustion processes can experience oscillatory heat release due to the alternate shedding of coherent, von Kármán vortices… (more)

Subjects/Keywords: Flame stability; Stability analysis; Bluff body; Combustion dynamics; Vortex shedding; Von Karman; Chemiluminescence; Combustion; Heat Transmission; Thermodynamics

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APA (6th Edition):

Cross, C. N. (2011). Combustion heat release effects on asymmetric vortex shedding from bluff bodies. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/42772

Chicago Manual of Style (16th Edition):

Cross, Caleb Nathaniel. “Combustion heat release effects on asymmetric vortex shedding from bluff bodies.” 2011. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/42772.

MLA Handbook (7th Edition):

Cross, Caleb Nathaniel. “Combustion heat release effects on asymmetric vortex shedding from bluff bodies.” 2011. Web. 17 Feb 2020.

Vancouver:

Cross CN. Combustion heat release effects on asymmetric vortex shedding from bluff bodies. [Internet] [Doctoral dissertation]. Georgia Tech; 2011. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/42772.

Council of Science Editors:

Cross CN. Combustion heat release effects on asymmetric vortex shedding from bluff bodies. [Doctoral Dissertation]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/42772

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

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

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

MLA Handbook (7th Edition):

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

Vancouver:

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

Council of Science Editors:

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

19. 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 February 17, 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. 17 Feb 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 Feb 17]. 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

20. 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 February 17, 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. 17 Feb 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 Feb 17]. 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

21. Wilde, Benjamin R. Dynamics of variable density ratio reacting jets in unsteady, vitiated crossflow.

Degree: PhD, Mechanical Engineering, 2014, Georgia Tech

 Jet in crossflow (JICF) configurations are often used for secondary fuel injection in staged-fuel combustion systems. The high temperature, vitiated crossflow in these systems is… (more)

Subjects/Keywords: Jet in crossflow; Acoustic forcing; Reacting jet; Shear layer dynamics

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APA (6th Edition):

Wilde, B. R. (2014). Dynamics of variable density ratio reacting jets in unsteady, vitiated crossflow. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53040

Chicago Manual of Style (16th Edition):

Wilde, Benjamin R. “Dynamics of variable density ratio reacting jets in unsteady, vitiated crossflow.” 2014. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/53040.

MLA Handbook (7th Edition):

Wilde, Benjamin R. “Dynamics of variable density ratio reacting jets in unsteady, vitiated crossflow.” 2014. Web. 17 Feb 2020.

Vancouver:

Wilde BR. Dynamics of variable density ratio reacting jets in unsteady, vitiated crossflow. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/53040.

Council of Science Editors:

Wilde BR. Dynamics of variable density ratio reacting jets in unsteady, vitiated crossflow. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53040

22. Yun, Thomas. Fuel reformation and hydrogen generation in variable volume membrane batch reactors with dynamic liquid fuel introduction.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 In recent years, the need for high performance power sources has increased dramatically with the proliferation of ultra-compact electronic systems for mobile communication, man-portable and… (more)

Subjects/Keywords: Hydrogen; Reformation; Reactor; Droplet evaporation; Catalytic reaction; Membrane

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APA (6th Edition):

Yun, T. (2015). Fuel reformation and hydrogen generation in variable volume membrane batch reactors with dynamic liquid fuel introduction. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53550

Chicago Manual of Style (16th Edition):

Yun, Thomas. “Fuel reformation and hydrogen generation in variable volume membrane batch reactors with dynamic liquid fuel introduction.” 2015. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/53550.

MLA Handbook (7th Edition):

Yun, Thomas. “Fuel reformation and hydrogen generation in variable volume membrane batch reactors with dynamic liquid fuel introduction.” 2015. Web. 17 Feb 2020.

Vancouver:

Yun T. Fuel reformation and hydrogen generation in variable volume membrane batch reactors with dynamic liquid fuel introduction. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/53550.

Council of Science Editors:

Yun T. Fuel reformation and hydrogen generation in variable volume membrane batch reactors with dynamic liquid fuel introduction. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53550


Georgia Tech

23. Parisi, Valerio. Large Eddy Simulation of a Stagnation Point Reverse Flow Combustor.

Degree: MS, Aerospace Engineering, 2006, Georgia Tech

 In this study, numerical simulations of a low emission lab-scale non-premixed combustor are conducted and analyzed. The objectives are to provide new insight into the… (more)

Subjects/Keywords: Entrainment; Reverse flow; Diffusion; Recirculation; Steady flamelet; EBU; LEM; LES; Combustion models; Non-premixed combustion; Combustion; Eddies Computer simulation; Unsteady flow (Fluid dynamics) Mathematical models; Turbulence Computer simulation

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APA (6th Edition):

Parisi, V. (2006). Large Eddy Simulation of a Stagnation Point Reverse Flow Combustor. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13995

Chicago Manual of Style (16th Edition):

Parisi, Valerio. “Large Eddy Simulation of a Stagnation Point Reverse Flow Combustor.” 2006. Masters Thesis, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/13995.

MLA Handbook (7th Edition):

Parisi, Valerio. “Large Eddy Simulation of a Stagnation Point Reverse Flow Combustor.” 2006. Web. 17 Feb 2020.

Vancouver:

Parisi V. Large Eddy Simulation of a Stagnation Point Reverse Flow Combustor. [Internet] [Masters thesis]. Georgia Tech; 2006. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/13995.

Council of Science Editors:

Parisi V. Large Eddy Simulation of a Stagnation Point Reverse Flow Combustor. [Masters Thesis]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/13995


Georgia Tech

24. Schild, Ilissa Brooke. Influence of Spark Energy, Spark Number, and Flow Velocity on Detonation Initiation in a Hydrocarbon-fueled PDE.

Degree: MS, Mechanical Engineering, 2005, Georgia Tech

 Pulsed Detonation Engines (PDEs) have the potential to revolutionize fight by better utilizing the chemical energy content of reactive fuel/air mixtures over conventional combustion processes.… (more)

Subjects/Keywords: Number; Energy; Velocity; Transition; Deflagration; DDT; PDE; Detonation; Kernel; Spark; Ignition; Initiation; Pulsed; Pulsed power systems; Combustion Computer simulation; Propulsion systems

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APA (6th Edition):

Schild, I. B. (2005). Influence of Spark Energy, Spark Number, and Flow Velocity on Detonation Initiation in a Hydrocarbon-fueled PDE. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/7527

Chicago Manual of Style (16th Edition):

Schild, Ilissa Brooke. “Influence of Spark Energy, Spark Number, and Flow Velocity on Detonation Initiation in a Hydrocarbon-fueled PDE.” 2005. Masters Thesis, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/7527.

MLA Handbook (7th Edition):

Schild, Ilissa Brooke. “Influence of Spark Energy, Spark Number, and Flow Velocity on Detonation Initiation in a Hydrocarbon-fueled PDE.” 2005. Web. 17 Feb 2020.

Vancouver:

Schild IB. Influence of Spark Energy, Spark Number, and Flow Velocity on Detonation Initiation in a Hydrocarbon-fueled PDE. [Internet] [Masters thesis]. Georgia Tech; 2005. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/7527.

Council of Science Editors:

Schild IB. Influence of Spark Energy, Spark Number, and Flow Velocity on Detonation Initiation in a Hydrocarbon-fueled PDE. [Masters Thesis]. Georgia Tech; 2005. Available from: http://hdl.handle.net/1853/7527


Georgia Tech

25. Kirtaş, Mehmet. Large Eddy Simulation of a High Aspect Ratio Combustor.

Degree: PhD, Aerospace Engineering, 2006, Georgia Tech

 The present research investigates the details of mixture preparation and combustion in a two-stroke, small-scale research engine with a numerical methodology based on large eddy… (more)

Subjects/Keywords: Flame; LES; Turbulence; Engine; Combustion

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APA (6th Edition):

Kirtaş, M. (2006). Large Eddy Simulation of a High Aspect Ratio Combustor. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/14134

Chicago Manual of Style (16th Edition):

Kirtaş, Mehmet. “Large Eddy Simulation of a High Aspect Ratio Combustor.” 2006. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/14134.

MLA Handbook (7th Edition):

Kirtaş, Mehmet. “Large Eddy Simulation of a High Aspect Ratio Combustor.” 2006. Web. 17 Feb 2020.

Vancouver:

Kirtaş M. Large Eddy Simulation of a High Aspect Ratio Combustor. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/14134.

Council of Science Editors:

Kirtaş M. Large Eddy Simulation of a High Aspect Ratio Combustor. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/14134


Georgia Tech

26. Sen, Baris Ali. Artificial neural networks based subgrid chemistry model for turbulent reactive flow simulations.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 Two new models to calculate the species instantaneous and filtered reaction rates for multi-step, multi-species chemical kinetics mechanisms are developed based on the artificial neural… (more)

Subjects/Keywords: Artificial neural networks; Tabulation; Linear eddy mixing; Turbulent combustion modeling; Chemical kinetics; Large eddy simulation; Turbulence; Eddies; Combustion

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APA (6th Edition):

Sen, B. A. (2009). Artificial neural networks based subgrid chemistry model for turbulent reactive flow simulations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/31757

Chicago Manual of Style (16th Edition):

Sen, Baris Ali. “Artificial neural networks based subgrid chemistry model for turbulent reactive flow simulations.” 2009. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/31757.

MLA Handbook (7th Edition):

Sen, Baris Ali. “Artificial neural networks based subgrid chemistry model for turbulent reactive flow simulations.” 2009. Web. 17 Feb 2020.

Vancouver:

Sen BA. Artificial neural networks based subgrid chemistry model for turbulent reactive flow simulations. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/31757.

Council of Science Editors:

Sen BA. Artificial neural networks based subgrid chemistry model for turbulent reactive flow simulations. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/31757


Georgia Tech

27. Narisetti, Raj K. Wave propagation in nonlinear periodic structures.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 A periodic structure consists of spatially repeating unit cells. From man-made multi-span bridges to naturally occurring atomic lattices, periodic structures are ubiquitous. The periodicity can… (more)

Subjects/Keywords: Nonlinear wave propagation; Amplitude dependent dispersion; Nonlinear finite element dispersion; Nonlinear periodic structures; Strongly nonlinear chains; Granular media; Wave directionality; Amplitude dependent wave beaming; Nonlinear wave equations; Wave motion, Theory of; Nonlinear theories

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APA (6th Edition):

Narisetti, R. K. (2010). Wave propagation in nonlinear periodic structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/39643

Chicago Manual of Style (16th Edition):

Narisetti, Raj K. “Wave propagation in nonlinear periodic structures.” 2010. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/39643.

MLA Handbook (7th Edition):

Narisetti, Raj K. “Wave propagation in nonlinear periodic structures.” 2010. Web. 17 Feb 2020.

Vancouver:

Narisetti RK. Wave propagation in nonlinear periodic structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/39643.

Council of Science Editors:

Narisetti RK. Wave propagation in nonlinear periodic structures. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/39643


Georgia Tech

28. Sankaran, Vaidyanathan. Sub-grid Combustion Modeling for Compressible Two-Phase Flows.

Degree: PhD, Aerospace Engineering, 2003, Georgia Tech

 A generic formulation for modeling the sub-grid combustion in compressible, high Reynolds number, two-phase, reacting flows has been developed and validated. A sub-grid mixing/combustion model… (more)

Subjects/Keywords: Sub-grid model; Combustion; LES; Linear eddy model; Two-phase flow; Combustion; Two-phase flow

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APA (6th Edition):

Sankaran, V. (2003). Sub-grid Combustion Modeling for Compressible Two-Phase Flows. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/5274

Chicago Manual of Style (16th Edition):

Sankaran, Vaidyanathan. “Sub-grid Combustion Modeling for Compressible Two-Phase Flows.” 2003. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/5274.

MLA Handbook (7th Edition):

Sankaran, Vaidyanathan. “Sub-grid Combustion Modeling for Compressible Two-Phase Flows.” 2003. Web. 17 Feb 2020.

Vancouver:

Sankaran V. Sub-grid Combustion Modeling for Compressible Two-Phase Flows. [Internet] [Doctoral dissertation]. Georgia Tech; 2003. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/5274.

Council of Science Editors:

Sankaran V. Sub-grid Combustion Modeling for Compressible Two-Phase Flows. [Doctoral Dissertation]. Georgia Tech; 2003. Available from: http://hdl.handle.net/1853/5274


Georgia Tech

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

Degree: PhD, Aerospace Engineering, 2007, Georgia Tech

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

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

MLA Handbook (7th Edition):

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

Vancouver:

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

Council of Science Editors:

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


Georgia Tech

30. Cordeiro, Helio de Miranda. Stochastic dynamical system identification applied to combustor stability margin assessment.

Degree: PhD, Aerospace Engineering, 2008, Georgia Tech

 A new approach was developed to determine the operational stability margin of a laboratory scale combustor. Applying modern and robust techniques and tools from Dynamical… (more)

Subjects/Keywords: System identification; Stability margin; Combustion instability; Combustion engineering; Acoustical engineering; Thermodynamics; Combustion chambers

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APA (6th Edition):

Cordeiro, H. d. M. (2008). Stochastic dynamical system identification applied to combustor stability margin assessment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28167

Chicago Manual of Style (16th Edition):

Cordeiro, Helio de Miranda. “Stochastic dynamical system identification applied to combustor stability margin assessment.” 2008. Doctoral Dissertation, Georgia Tech. Accessed February 17, 2020. http://hdl.handle.net/1853/28167.

MLA Handbook (7th Edition):

Cordeiro, Helio de Miranda. “Stochastic dynamical system identification applied to combustor stability margin assessment.” 2008. Web. 17 Feb 2020.

Vancouver:

Cordeiro HdM. Stochastic dynamical system identification applied to combustor stability margin assessment. [Internet] [Doctoral dissertation]. Georgia Tech; 2008. [cited 2020 Feb 17]. Available from: http://hdl.handle.net/1853/28167.

Council of Science Editors:

Cordeiro HdM. Stochastic dynamical system identification applied to combustor stability margin assessment. [Doctoral Dissertation]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/28167

.