Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for +publisher:"Georgia Tech" +contributor:("Yang, Vigor"). Showing records 1 – 18 of 18 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


Georgia Tech

1. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 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. 22 Jan 2021.

Vancouver:

Muraleedharan MGg. Nanoscale heat transfer effects in the combustion of nanoenergetic materials. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Jan 22]. 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

2. Lioi, Christopher. Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 This thesis concerns the consistent linear acoustic stability analysis of an engine modeled on the RD-170, a prototypical example of an Oxidizer Rich Staged Combustion… (more)

Subjects/Keywords: Combustion instabilities; Acoustics; Liquid rocket engines; ORSC engines; Finite element analysis; LES; Flame transfer function

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lioi, C. (2019). Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/62579

Chicago Manual of Style (16th Edition):

Lioi, Christopher. “Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines.” 2019. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/62579.

MLA Handbook (7th Edition):

Lioi, Christopher. “Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines.” 2019. Web. 22 Jan 2021.

Vancouver:

Lioi C. Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/62579.

Council of Science Editors:

Lioi C. Linear combustion stabiliy analysis of oxidizer-rich staged combustion engines. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/62579


Georgia Tech

3. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 2021. http://hdl.handle.net/1853/53395.

MLA Handbook (7th Edition):

Khare, Prashant. “Breakup of liquid droplets.” 2013. Web. 22 Jan 2021.

Vancouver:

Khare P. Breakup of liquid droplets. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 22]. 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

4. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 2021. http://hdl.handle.net/1853/58565.

MLA Handbook (7th Edition):

Wang, Xingjian. “Swirling fluid mixing and combustion dynamics at supercritical conditions.” 2016. Web. 22 Jan 2021.

Vancouver:

Wang X. Swirling fluid mixing and combustion dynamics at supercritical conditions. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Jan 22]. 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

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

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Nagaraja, Sharath. “Multi-scale modeling of nanosecond plasma assisted combustion.” 2014. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/52228.

MLA Handbook (7th Edition):

Nagaraja, Sharath. “Multi-scale modeling of nanosecond plasma assisted combustion.” 2014. Web. 22 Jan 2021.

Vancouver:

Nagaraja S. Multi-scale modeling of nanosecond plasma assisted combustion. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/52228.

Council of Science Editors:

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


Georgia Tech

6. Lympany, Shane V. Acoustic damping mechanisms of half-wave resonators in a rocket engine environment.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Combustion instabilities in rocket engines are caused by coupling between the combustion processes and pressure oscillations in a combustor, and they are characterized by the… (more)

Subjects/Keywords: Acoustics; Acoustic damping; Acoustic resonators; Half-wave resonators; Acoustic impedance; Absorption coefficient; Scattering; Impedance tube; Nonlinear acoustics; Higher-order modes; Combustion instability; Propellant injectors

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lympany, S. V. (2018). Acoustic damping mechanisms of half-wave resonators in a rocket engine environment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60266

Chicago Manual of Style (16th Edition):

Lympany, Shane V. “Acoustic damping mechanisms of half-wave resonators in a rocket engine environment.” 2018. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/60266.

MLA Handbook (7th Edition):

Lympany, Shane V. “Acoustic damping mechanisms of half-wave resonators in a rocket engine environment.” 2018. Web. 22 Jan 2021.

Vancouver:

Lympany SV. Acoustic damping mechanisms of half-wave resonators in a rocket engine environment. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/60266.

Council of Science Editors:

Lympany SV. Acoustic damping mechanisms of half-wave resonators in a rocket engine environment. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60266


Georgia Tech

7. Chang, Yu-Hung. High-fidelity emulation of spatiotemporally evolving flow dynamics.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 This dissertation utilizes a comprehensive interdisciplinary approach to demonstrate a paradigm for a novel design strategy for new generation engineering. Computational fluid dynamics (CFD), reduced-basis… (more)

Subjects/Keywords: Design study; High-fidelity simulation; Kriging; Data reduction; Surrogate model; Swirl injector

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chang, Y. (2018). High-fidelity emulation of spatiotemporally evolving flow dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60842

Chicago Manual of Style (16th Edition):

Chang, Yu-Hung. “High-fidelity emulation of spatiotemporally evolving flow dynamics.” 2018. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/60842.

MLA Handbook (7th Edition):

Chang, Yu-Hung. “High-fidelity emulation of spatiotemporally evolving flow dynamics.” 2018. Web. 22 Jan 2021.

Vancouver:

Chang Y. High-fidelity emulation of spatiotemporally evolving flow dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/60842.

Council of Science Editors:

Chang Y. High-fidelity emulation of spatiotemporally evolving flow dynamics. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60842


Georgia Tech

8. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 2021. 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. 22 Jan 2021.

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 2021 Jan 22]. 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

9. Shin, Dong-hyuk. Premixed flame kinematics in a harmonically oscillating velocity field.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Air pollution regulations have driven modern power generation systems to move from diffusion to premixed combustion. However, these premixed combustion systems are prone to combustion… (more)

Subjects/Keywords: Combustion instability; Combustion dynamics; Flame stability; Combustion; Combustion engineering; Combustion Research

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Shin, D. (2012). Premixed flame kinematics in a harmonically oscillating velocity field. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/45950

Chicago Manual of Style (16th Edition):

Shin, Dong-hyuk. “Premixed flame kinematics in a harmonically oscillating velocity field.” 2012. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/45950.

MLA Handbook (7th Edition):

Shin, Dong-hyuk. “Premixed flame kinematics in a harmonically oscillating velocity field.” 2012. Web. 22 Jan 2021.

Vancouver:

Shin D. Premixed flame kinematics in a harmonically oscillating velocity field. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/45950.

Council of Science Editors:

Shin D. Premixed flame kinematics in a harmonically oscillating velocity field. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/45950

10. 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… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 2021. http://hdl.handle.net/1853/50213.

MLA Handbook (7th Edition):

Acharya, Vishal Srinivas. “Dynamics of premixed flames in non-axisymmetric disturbance fields.” 2013. Web. 22 Jan 2021.

Vancouver:

Acharya VS. Dynamics of premixed flames in non-axisymmetric disturbance fields. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 22]. 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

11. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 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. 22 Jan 2021.

Vancouver:

Sundaram DS. Multi-scale modeling of thermochemical behavior of nano-energetic materials. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 22]. 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

12. Masquelet, Matthieu Marc. Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 The understanding and prediction of transient phenomena inside Liquid Rocket Engines (LREs) have been very difficult because of the many challenges posed by the conditions… (more)

Subjects/Keywords: Combustion; Supercritical; Scaling; LES; LRE; CFD; Computational fluid dynamics; Propulsion systems; Rocket engines; Rocket engines Combustion; Liquid propellant rocket engines

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Masquelet, M. M. (2013). Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/47522

Chicago Manual of Style (16th Edition):

Masquelet, Matthieu Marc. “Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines.” 2013. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/47522.

MLA Handbook (7th Edition):

Masquelet, Matthieu Marc. “Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines.” 2013. Web. 22 Jan 2021.

Vancouver:

Masquelet MM. Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/47522.

Council of Science Editors:

Masquelet MM. Large-eddy simulations of high-pressure shear coaxial flows relevant for H2/O2 rocket engines. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/47522

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

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Yang, Suo. “Effects of detailed finite rate chemistry in turbulent combustion.” 2017. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/58672.

MLA Handbook (7th Edition):

Yang, Suo. “Effects of detailed finite rate chemistry in turbulent combustion.” 2017. Web. 22 Jan 2021.

Vancouver:

Yang S. Effects of detailed finite rate chemistry in turbulent combustion. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/58672.

Council of Science Editors:

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

14. Yeh, Shiang-Ting. Common proper orthogonal decomposition-based emulation and system identification for model-based analysis of combustion dynamics.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 For high-performance power generation and propulsion systems, such as those of airbreathing and rocket engines, physical experiments are expensive due to the harsh requirements of… (more)

Subjects/Keywords: Emulation; Combustion response

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Yeh, S. (2018). Common proper orthogonal decomposition-based emulation and system identification for model-based analysis of combustion dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59965

Chicago Manual of Style (16th Edition):

Yeh, Shiang-Ting. “Common proper orthogonal decomposition-based emulation and system identification for model-based analysis of combustion dynamics.” 2018. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/59965.

MLA Handbook (7th Edition):

Yeh, Shiang-Ting. “Common proper orthogonal decomposition-based emulation and system identification for model-based analysis of combustion dynamics.” 2018. Web. 22 Jan 2021.

Vancouver:

Yeh S. Common proper orthogonal decomposition-based emulation and system identification for model-based analysis of combustion dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/59965.

Council of Science Editors:

Yeh S. Common proper orthogonal decomposition-based emulation and system identification for model-based analysis of combustion dynamics. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59965

15. 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… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 January 22, 2021. 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. 22 Jan 2021.

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 2021 Jan 22]. 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

16. Pakmehr, Mehrdad. Towards verifiable adaptive control of gas turbine engines.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 This dissertation investigates the problem of developing verifiable stable control architectures for gas turbine engines. First, a nonlinear physics-based dynamic model of a twin spool… (more)

Subjects/Keywords: Adaptive control; Gain scheduled control; Gas turbine engines; Aerospace software verification; Gas-turbines; Jet engines; Adaptive control systems

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pakmehr, M. (2013). Towards verifiable adaptive control of gas turbine engines. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/49025

Chicago Manual of Style (16th Edition):

Pakmehr, Mehrdad. “Towards verifiable adaptive control of gas turbine engines.” 2013. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/49025.

MLA Handbook (7th Edition):

Pakmehr, Mehrdad. “Towards verifiable adaptive control of gas turbine engines.” 2013. Web. 22 Jan 2021.

Vancouver:

Pakmehr M. Towards verifiable adaptive control of gas turbine engines. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/49025.

Council of Science Editors:

Pakmehr M. Towards verifiable adaptive control of gas turbine engines. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/49025


Georgia Tech

17. Ukai, Satoshi. Richtmyer-Meshkov instability with reshock and particle interactions.

Degree: MS, Aerospace Engineering, 2010, Georgia Tech

 Richtmyer-Meshkov instability (RMI) occurs when an interface of two fluids with different densities is impulsively accelerated. The main interest in RMI is to understand the… (more)

Subjects/Keywords: Multiphase flow; Shock; Instability; Richtmyer-Meshkov instability; Navier-Stokes equations; Fluid dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ukai, S. (2010). Richtmyer-Meshkov instability with reshock and particle interactions. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/34724

Chicago Manual of Style (16th Edition):

Ukai, Satoshi. “Richtmyer-Meshkov instability with reshock and particle interactions.” 2010. Masters Thesis, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/34724.

MLA Handbook (7th Edition):

Ukai, Satoshi. “Richtmyer-Meshkov instability with reshock and particle interactions.” 2010. Web. 22 Jan 2021.

Vancouver:

Ukai S. Richtmyer-Meshkov instability with reshock and particle interactions. [Internet] [Masters thesis]. Georgia Tech; 2010. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/34724.

Council of Science Editors:

Ukai S. Richtmyer-Meshkov instability with reshock and particle interactions. [Masters Thesis]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/34724


Georgia Tech

18. Hemchandra, Santosh. Dynamics of turbulent premixed flames in acoustic fields.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 This thesis describes computational and theoretical studies of fundamental physical processes that influence the heat-release response of turbulent premixed flames to acoustic forcing. Attached turbulent… (more)

Subjects/Keywords: Heat release response; Turbulent flames; Level-set; Non-locality; Turbulent flame speed; Transfer function; Consumption speed; Turbulence; Combustion; Kinematics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hemchandra, S. (2009). Dynamics of turbulent premixed flames in acoustic fields. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/29615

Chicago Manual of Style (16th Edition):

Hemchandra, Santosh. “Dynamics of turbulent premixed flames in acoustic fields.” 2009. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/29615.

MLA Handbook (7th Edition):

Hemchandra, Santosh. “Dynamics of turbulent premixed flames in acoustic fields.” 2009. Web. 22 Jan 2021.

Vancouver:

Hemchandra S. Dynamics of turbulent premixed flames in acoustic fields. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/29615.

Council of Science Editors:

Hemchandra S. Dynamics of turbulent premixed flames in acoustic fields. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/29615

.