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You searched for +publisher:"University of Texas – Austin" +contributor:("Varghese, Philip L."). Showing records 1 – 30 of 34 total matches.

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University of Texas – Austin

1. Hegermiller, David Benjamin. A new method to incorporate internal energy into a discrete velocity Monte Carlo Boltzmann Equation solver.

Degree: MSin Engineering, Aerospace Engineering, 2011, University of Texas – Austin

 A new method has been developed to incorporate particles with internal structure into the framework of the Variance Reduction method [17] for solving the discrete… (more)

Subjects/Keywords: Boltzmann Equation; Internal energy; Discrete velocity

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APA (6th Edition):

Hegermiller, D. B. (2011). A new method to incorporate internal energy into a discrete velocity Monte Carlo Boltzmann Equation solver. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-08-4328

Chicago Manual of Style (16th Edition):

Hegermiller, David Benjamin. “A new method to incorporate internal energy into a discrete velocity Monte Carlo Boltzmann Equation solver.” 2011. Masters Thesis, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2011-08-4328.

MLA Handbook (7th Edition):

Hegermiller, David Benjamin. “A new method to incorporate internal energy into a discrete velocity Monte Carlo Boltzmann Equation solver.” 2011. Web. 03 Mar 2021.

Vancouver:

Hegermiller DB. A new method to incorporate internal energy into a discrete velocity Monte Carlo Boltzmann Equation solver. [Internet] [Masters thesis]. University of Texas – Austin; 2011. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-08-4328.

Council of Science Editors:

Hegermiller DB. A new method to incorporate internal energy into a discrete velocity Monte Carlo Boltzmann Equation solver. [Masters Thesis]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-08-4328


University of Texas – Austin

2. Tovar, Sergio Andre. Simulation of LCROSS hydroxyl band strength data.

Degree: MSin Engineering, Aerospace Engineering, 2019, University of Texas – Austin

 In 2009, NASA launched the Lunar CRater Observation and Sensing Satellite (LCROSS) mission to confirm and characterize the presence of water ice in the Moon.… (more)

Subjects/Keywords: LCROSS; Hydroxyl; Curve fit

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APA (6th Edition):

Tovar, S. A. (2019). Simulation of LCROSS hydroxyl band strength data. (Masters Thesis). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/2152

Chicago Manual of Style (16th Edition):

Tovar, Sergio Andre. “Simulation of LCROSS hydroxyl band strength data.” 2019. Masters Thesis, University of Texas – Austin. Accessed March 03, 2021. http://dx.doi.org/10.26153/tsw/2152.

MLA Handbook (7th Edition):

Tovar, Sergio Andre. “Simulation of LCROSS hydroxyl band strength data.” 2019. Web. 03 Mar 2021.

Vancouver:

Tovar SA. Simulation of LCROSS hydroxyl band strength data. [Internet] [Masters thesis]. University of Texas – Austin; 2019. [cited 2021 Mar 03]. Available from: http://dx.doi.org/10.26153/tsw/2152.

Council of Science Editors:

Tovar SA. Simulation of LCROSS hydroxyl band strength data. [Masters Thesis]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/2152

3. KC, Utsav. Development of a multiple-pass Raman spectrometer for flame diagnostics.

Degree: PhD, Aerospace Engineering, 2013, University of Texas – Austin

 A multiple-pass cell is developed and applied to enhance the Raman signal from methane-air flames for temperature measurements. Stable operation of the cell was demonstrated… (more)

Subjects/Keywords: Raman spectroscopy; Combustion; Instrument development; Temperature measurement

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APA (6th Edition):

KC, U. (2013). Development of a multiple-pass Raman spectrometer for flame diagnostics. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/21454

Chicago Manual of Style (16th Edition):

KC, Utsav. “Development of a multiple-pass Raman spectrometer for flame diagnostics.” 2013. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/21454.

MLA Handbook (7th Edition):

KC, Utsav. “Development of a multiple-pass Raman spectrometer for flame diagnostics.” 2013. Web. 03 Mar 2021.

Vancouver:

KC U. Development of a multiple-pass Raman spectrometer for flame diagnostics. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2013. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/21454.

Council of Science Editors:

KC U. Development of a multiple-pass Raman spectrometer for flame diagnostics. [Doctoral Dissertation]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/21454

4. Zhang, Ju. Simulation of gas dynamics, radiation and particulates in volcanic plumes on Io.

Degree: PhD, Aerospace Engineering, 2004, University of Texas – Austin

Subjects/Keywords: Volcanic plumes – Io (Satellite); Rarefied gas dynamics – Mathematical models

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APA (6th Edition):

Zhang, J. (2004). Simulation of gas dynamics, radiation and particulates in volcanic plumes on Io. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/2103

Chicago Manual of Style (16th Edition):

Zhang, Ju. “Simulation of gas dynamics, radiation and particulates in volcanic plumes on Io.” 2004. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/2103.

MLA Handbook (7th Edition):

Zhang, Ju. “Simulation of gas dynamics, radiation and particulates in volcanic plumes on Io.” 2004. Web. 03 Mar 2021.

Vancouver:

Zhang J. Simulation of gas dynamics, radiation and particulates in volcanic plumes on Io. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2004. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/2103.

Council of Science Editors:

Zhang J. Simulation of gas dynamics, radiation and particulates in volcanic plumes on Io. [Doctoral Dissertation]. University of Texas – Austin; 2004. Available from: http://hdl.handle.net/2152/2103

5. -9775-4068. Computational modeling of high pressure plasmas for plasma assisted combustion, liquid reforming and thermal breakdown applications.

Degree: PhD, Aerospace Engineering, 2019, University of Texas – Austin

 The goal of the present work is to study high pressure non-equilibrium plasma discharges in chemically reactive systems. In this work, we present coupled computational… (more)

Subjects/Keywords: Modeling; Plasma; Combustion; Streamers; Photoionization; Reforming; Fast gas heating; Multiphysics; Streamers in bubbles; Fluid model; Self-consistent

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APA (6th Edition):

-9775-4068. (2019). Computational modeling of high pressure plasmas for plasma assisted combustion, liquid reforming and thermal breakdown applications. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/1069

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-9775-4068. “Computational modeling of high pressure plasmas for plasma assisted combustion, liquid reforming and thermal breakdown applications.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://dx.doi.org/10.26153/tsw/1069.

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

MLA Handbook (7th Edition):

-9775-4068. “Computational modeling of high pressure plasmas for plasma assisted combustion, liquid reforming and thermal breakdown applications.” 2019. Web. 03 Mar 2021.

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

Vancouver:

-9775-4068. Computational modeling of high pressure plasmas for plasma assisted combustion, liquid reforming and thermal breakdown applications. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2021 Mar 03]. Available from: http://dx.doi.org/10.26153/tsw/1069.

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

Council of Science Editors:

-9775-4068. Computational modeling of high pressure plasmas for plasma assisted combustion, liquid reforming and thermal breakdown applications. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/1069

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Author name may be incomplete


University of Texas – Austin

6. Ebi, Dominik Fabian. Boundary layer flashback of swirl flames.

Degree: PhD, Aerospace Engineering, 2016, University of Texas – Austin

 Flame flashback in the boundary layer of swirling flows is investigated experimentally in a model swirl combustor. The model combustor features a mixing tube with… (more)

Subjects/Keywords: Turbulent flames; Flashback; High-speed PIV; Tomographic PIV

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APA (6th Edition):

Ebi, D. F. (2016). Boundary layer flashback of swirl flames. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/38721

Chicago Manual of Style (16th Edition):

Ebi, Dominik Fabian. “Boundary layer flashback of swirl flames.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/38721.

MLA Handbook (7th Edition):

Ebi, Dominik Fabian. “Boundary layer flashback of swirl flames.” 2016. Web. 03 Mar 2021.

Vancouver:

Ebi DF. Boundary layer flashback of swirl flames. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/38721.

Council of Science Editors:

Ebi DF. Boundary layer flashback of swirl flames. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/38721


University of Texas – Austin

7. -3357-9103. Multi-physics modeling of electromagnetically driven surface plasma discharges.

Degree: PhD, Aerospace Engineering, 2019, University of Texas – Austin

 This dissertation presents the computational modeling of non-equilibrium plasma discharges on an electromagnetically driven surface and its application to plasma assisted combustion. We address challenges… (more)

Subjects/Keywords: Computational modeling; Plasma discharges; Microwave plasmas; Surface plasmas; Metamaterials; Metasurfaces; Spoof surface plasmon polariton; Combustion ignition; Plasma assisted combustion

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APA (6th Edition):

-3357-9103. (2019). Multi-physics modeling of electromagnetically driven surface plasma discharges. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/9007

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-3357-9103. “Multi-physics modeling of electromagnetically driven surface plasma discharges.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://dx.doi.org/10.26153/tsw/9007.

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Author name may be incomplete

MLA Handbook (7th Edition):

-3357-9103. “Multi-physics modeling of electromagnetically driven surface plasma discharges.” 2019. Web. 03 Mar 2021.

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

Vancouver:

-3357-9103. Multi-physics modeling of electromagnetically driven surface plasma discharges. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2021 Mar 03]. Available from: http://dx.doi.org/10.26153/tsw/9007.

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

Council of Science Editors:

-3357-9103. Multi-physics modeling of electromagnetically driven surface plasma discharges. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/9007

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Author name may be incomplete

8. -8933-0393. Study of non-equilibrium plasma streamer discharges in high pressure molecular gases.

Degree: PhD, Aerospace Engineering, 2017, University of Texas – Austin

 A study of streamer discharge properties in the context of their applications in: large-gap arc breakdown, and plasma reforming of carbon-dioxide is presented. The first… (more)

Subjects/Keywords: Carbon dioxide; Reforming; Plasma; Streamer; Non-equilibrium; Thermal plasma; Surface streamer

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APA (6th Edition):

-8933-0393. (2017). Study of non-equilibrium plasma streamer discharges in high pressure molecular gases. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/63282

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

Chicago Manual of Style (16th Edition):

-8933-0393. “Study of non-equilibrium plasma streamer discharges in high pressure molecular gases.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/63282.

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

MLA Handbook (7th Edition):

-8933-0393. “Study of non-equilibrium plasma streamer discharges in high pressure molecular gases.” 2017. Web. 03 Mar 2021.

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

Vancouver:

-8933-0393. Study of non-equilibrium plasma streamer discharges in high pressure molecular gases. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/63282.

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

Council of Science Editors:

-8933-0393. Study of non-equilibrium plasma streamer discharges in high pressure molecular gases. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/63282

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Author name may be incomplete


University of Texas – Austin

9. Koo, Heeseok. Large-eddy simulations of scramjet engines.

Degree: PhD, Aerospace Engineering, 2011, University of Texas – Austin

 The main objective of this dissertation is to develop large-eddy simulation (LES) based computational tools for supersonic inlet and combustor design. In the recent past,… (more)

Subjects/Keywords: Large-eddy simulations; Combustion model; DQMOM; Direct quadrature method of moments; Compressible flow; Shock capturing method; Hyperviscosity; Scramjet; Inlet-isolator; Unstart

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APA (6th Edition):

Koo, H. (2011). Large-eddy simulations of scramjet engines. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-05-3203

Chicago Manual of Style (16th Edition):

Koo, Heeseok. “Large-eddy simulations of scramjet engines.” 2011. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2011-05-3203.

MLA Handbook (7th Edition):

Koo, Heeseok. “Large-eddy simulations of scramjet engines.” 2011. Web. 03 Mar 2021.

Vancouver:

Koo H. Large-eddy simulations of scramjet engines. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2011. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3203.

Council of Science Editors:

Koo H. Large-eddy simulations of scramjet engines. [Doctoral Dissertation]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3203


University of Texas – Austin

10. Panneer Chelvam, Prem Kumar. Computational modeling of electromagnetic waves and their interactions with microplasmas.

Degree: PhD, Aerospace Engineering, 2017, University of Texas – Austin

 Development of a computational model to study the interaction of high frequency electromagnetic (EM) waves with plasmas is presented. The plasma is described using a… (more)

Subjects/Keywords: Electromagnetic waves; Plasmas; Computational modeling; Nédélec elements of first type; Nodal auxiliary space preconditioning; Preconditioning Helmholtz equation; Microdischarges; Dielectric resonators; Microplasmas

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APA (6th Edition):

Panneer Chelvam, P. K. (2017). Computational modeling of electromagnetic waves and their interactions with microplasmas. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/63458

Chicago Manual of Style (16th Edition):

Panneer Chelvam, Prem Kumar. “Computational modeling of electromagnetic waves and their interactions with microplasmas.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/63458.

MLA Handbook (7th Edition):

Panneer Chelvam, Prem Kumar. “Computational modeling of electromagnetic waves and their interactions with microplasmas.” 2017. Web. 03 Mar 2021.

Vancouver:

Panneer Chelvam PK. Computational modeling of electromagnetic waves and their interactions with microplasmas. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/63458.

Council of Science Editors:

Panneer Chelvam PK. Computational modeling of electromagnetic waves and their interactions with microplasmas. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/63458


University of Texas – Austin

11. Marr, Kevin Chek-Shing. Investigation of acoustically forced non-premixed jet flames in crossflow.

Degree: PhD, Aerospace Engineering, 2011, University of Texas – Austin

 The work presented here discusses the effects of strong acoustic forcing on jet flames in crossflow (JFICF) and the physical mechanisms behind theses effects. For… (more)

Subjects/Keywords: Pulsed combustion; Acoustics; Jet flames; Emissions; Flame stability

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APA (6th Edition):

Marr, K. C. (2011). Investigation of acoustically forced non-premixed jet flames in crossflow. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-05-3133

Chicago Manual of Style (16th Edition):

Marr, Kevin Chek-Shing. “Investigation of acoustically forced non-premixed jet flames in crossflow.” 2011. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2011-05-3133.

MLA Handbook (7th Edition):

Marr, Kevin Chek-Shing. “Investigation of acoustically forced non-premixed jet flames in crossflow.” 2011. Web. 03 Mar 2021.

Vancouver:

Marr KC. Investigation of acoustically forced non-premixed jet flames in crossflow. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2011. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3133.

Council of Science Editors:

Marr KC. Investigation of acoustically forced non-premixed jet flames in crossflow. [Doctoral Dissertation]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-05-3133


University of Texas – Austin

12. Lietz, Christopher Fernandez. Large-Eddy simulation of gas turbine combustors using Flamelet Manifold methods.

Degree: PhD, Aerospace engineering, 2015, University of Texas – Austin

 The main objective of this work was to develop a large-eddy simulation (LES) based computational tool for application to both premixed and non- premixed combustion… (more)

Subjects/Keywords: Computational fluid dynamics (CFD); Large-Eddy simulation (LES); Combustion; Flamelet progress variable approach (FPVA)

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APA (6th Edition):

Lietz, C. F. (2015). Large-Eddy simulation of gas turbine combustors using Flamelet Manifold methods. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/32911

Chicago Manual of Style (16th Edition):

Lietz, Christopher Fernandez. “Large-Eddy simulation of gas turbine combustors using Flamelet Manifold methods.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/32911.

MLA Handbook (7th Edition):

Lietz, Christopher Fernandez. “Large-Eddy simulation of gas turbine combustors using Flamelet Manifold methods.” 2015. Web. 03 Mar 2021.

Vancouver:

Lietz CF. Large-Eddy simulation of gas turbine combustors using Flamelet Manifold methods. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/32911.

Council of Science Editors:

Lietz CF. Large-Eddy simulation of gas turbine combustors using Flamelet Manifold methods. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/32911


University of Texas – Austin

13. -3704-0597. Quantitative measurements of ablation-products transport in supersonic turbulent flows using planar laser-induced fluorescence.

Degree: PhD, Aerospace engineering, 2015, University of Texas – Austin

 A recently-developed experimental technique based on the sublimation of naphthalene, which enables imaging of the dispersion of a passive scalar using planar laser-induced fluorescence (PLIF),… (more)

Subjects/Keywords: PLIF; PIV; Scalar transport; Supersonic flows; Ablation; Reentry; Orion capsule; Turbulence; Naphthalene; Fluorescence; Laser diagnostics

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APA (6th Edition):

-3704-0597. (2015). Quantitative measurements of ablation-products transport in supersonic turbulent flows using planar laser-induced fluorescence. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31340

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-3704-0597. “Quantitative measurements of ablation-products transport in supersonic turbulent flows using planar laser-induced fluorescence.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/31340.

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

MLA Handbook (7th Edition):

-3704-0597. “Quantitative measurements of ablation-products transport in supersonic turbulent flows using planar laser-induced fluorescence.” 2015. Web. 03 Mar 2021.

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

Vancouver:

-3704-0597. Quantitative measurements of ablation-products transport in supersonic turbulent flows using planar laser-induced fluorescence. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/31340.

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

Council of Science Editors:

-3704-0597. Quantitative measurements of ablation-products transport in supersonic turbulent flows using planar laser-induced fluorescence. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31340

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


University of Texas – Austin

14. Clarke, Peter Barry. A discrete velocity method for the Boltzmann equation with internal energy and stochastic variance reduction.

Degree: PhD, Aerospace engineering, 2015, University of Texas – Austin

 The goal of this work is to develop an accurate and efficient flow solver based upon a discrete velocity description of the Boltzmann equation. Standard… (more)

Subjects/Keywords: Rarefied gas dynamics; Boltzmann equation; Discrete velocity method; Monte Carlo method; Variance reduction; Collision integral; Internal energy

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APA (6th Edition):

Clarke, P. B. (2015). A discrete velocity method for the Boltzmann equation with internal energy and stochastic variance reduction. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/32934

Chicago Manual of Style (16th Edition):

Clarke, Peter Barry. “A discrete velocity method for the Boltzmann equation with internal energy and stochastic variance reduction.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/32934.

MLA Handbook (7th Edition):

Clarke, Peter Barry. “A discrete velocity method for the Boltzmann equation with internal energy and stochastic variance reduction.” 2015. Web. 03 Mar 2021.

Vancouver:

Clarke PB. A discrete velocity method for the Boltzmann equation with internal energy and stochastic variance reduction. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/32934.

Council of Science Editors:

Clarke PB. A discrete velocity method for the Boltzmann equation with internal energy and stochastic variance reduction. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/32934


University of Texas – Austin

15. -0021-1302. Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 This work focuses on the development and sensitivity analyses of a direct simulation Monte Carlo (DSMC) code to understand the complex physical processes that occur… (more)

Subjects/Keywords: DSMC; Hypersonic; Radiation; Simulation; Sensitivity analysis; Monte Carlo; Reentry; Shock tube; CHIPS; EAST; NEQAIR; Backward reaction; Higdon; Ionizing

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APA (6th Edition):

-0021-1302. (2018). Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/69005

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-0021-1302. “Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/69005.

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

MLA Handbook (7th Edition):

-0021-1302. “Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows.” 2018. Web. 03 Mar 2021.

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

Vancouver:

-0021-1302. Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/69005.

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Council of Science Editors:

-0021-1302. Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/69005

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16. Voelkel, Stephen Joseph. Thermal nonequilibrium models for high-temperature reactive processes.

Degree: PhD, Computational Science, Engineering, and Mathematics, 2016, University of Texas – Austin

 This dissertation examines how thermal nonequilibrium affects mixing and combustion in high-enthalpy, high-speed systems such as reentry vehicles, scramjets, and detonation-driven engines. Specifically, the focus… (more)

Subjects/Keywords: Thermal nonequilibrium; Scramjet; Reentry vehicle; Quasi-classical trajectory; QCT; Hydrogen combustion; Nitrogen dissociation; Nitrogen-oxygen scattering

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APA (6th Edition):

Voelkel, S. J. (2016). Thermal nonequilibrium models for high-temperature reactive processes. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/47234

Chicago Manual of Style (16th Edition):

Voelkel, Stephen Joseph. “Thermal nonequilibrium models for high-temperature reactive processes.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/47234.

MLA Handbook (7th Edition):

Voelkel, Stephen Joseph. “Thermal nonequilibrium models for high-temperature reactive processes.” 2016. Web. 03 Mar 2021.

Vancouver:

Voelkel SJ. Thermal nonequilibrium models for high-temperature reactive processes. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/47234.

Council of Science Editors:

Voelkel SJ. Thermal nonequilibrium models for high-temperature reactive processes. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/47234


University of Texas – Austin

17. -5890-8543. Realistic simulation of Io's Pele plume and its effects on Io's atmosphere.

Degree: PhD, Aerospace Engineering, 2015, University of Texas – Austin

 The direct simulation Monte Carlo (DSMC) method is used to investigate gas and dust in Io's giant Pele plume as well as the interaction of… (more)

Subjects/Keywords: Direct simulation Monte Carlo; DSMC; Io; Plumes; Pele

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APA (6th Edition):

-5890-8543. (2015). Realistic simulation of Io's Pele plume and its effects on Io's atmosphere. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/32821

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Chicago Manual of Style (16th Edition):

-5890-8543. “Realistic simulation of Io's Pele plume and its effects on Io's atmosphere.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/32821.

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MLA Handbook (7th Edition):

-5890-8543. “Realistic simulation of Io's Pele plume and its effects on Io's atmosphere.” 2015. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-5890-8543. Realistic simulation of Io's Pele plume and its effects on Io's atmosphere. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/32821.

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Author name may be incomplete

Council of Science Editors:

-5890-8543. Realistic simulation of Io's Pele plume and its effects on Io's atmosphere. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/32821

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Author name may be incomplete


University of Texas – Austin

18. -8909-3631. Multi-physics computational modeling of electromagnetic acceleration devices.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 A multi-physics computational framework is developed to simulate dense, high-ionization fraction plasmas in electromagnetic acceleration devices. The primary motivation for this research is the simulation… (more)

Subjects/Keywords: Multiphysics; Computational modeling

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APA (6th Edition):

-8909-3631. (2018). Multi-physics computational modeling of electromagnetic acceleration devices. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/71466

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Chicago Manual of Style (16th Edition):

-8909-3631. “Multi-physics computational modeling of electromagnetic acceleration devices.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/71466.

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MLA Handbook (7th Edition):

-8909-3631. “Multi-physics computational modeling of electromagnetic acceleration devices.” 2018. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-8909-3631. Multi-physics computational modeling of electromagnetic acceleration devices. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/71466.

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Author name may be incomplete

Council of Science Editors:

-8909-3631. Multi-physics computational modeling of electromagnetic acceleration devices. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/71466

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University of Texas – Austin

19. -3650-2649. Rarefied gas dynamic simulations of planetary atmospheric systems.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 My doctoral research involves the advanced numerical simulation of rarefied (low-pressure) planetary atmospheres and volcanism with advanced physical modeling, in application of the Direct Simulation… (more)

Subjects/Keywords: DSMC; Rarefied gas dynamics; Planetary science; Atmospheric science; Planetary volcanism; Plumes; Io; Tvashtar; Pluto; Charon; Earth's atmosphere

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APA (6th Edition):

-3650-2649. (2018). Rarefied gas dynamic simulations of planetary atmospheric systems. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/63474

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Chicago Manual of Style (16th Edition):

-3650-2649. “Rarefied gas dynamic simulations of planetary atmospheric systems.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/63474.

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MLA Handbook (7th Edition):

-3650-2649. “Rarefied gas dynamic simulations of planetary atmospheric systems.” 2018. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-3650-2649. Rarefied gas dynamic simulations of planetary atmospheric systems. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/63474.

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

Council of Science Editors:

-3650-2649. Rarefied gas dynamic simulations of planetary atmospheric systems. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/63474

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Author name may be incomplete

20. Wang, Guanghua. Two-point high repetition rate measurement of temperature and thermal dissipation in a turbulent non-premixed jet flame.

Degree: PhD, Aerospace Engineering, 2004, University of Texas – Austin

 A high-repetition rate (10 kHz) laser Rayleigh scattering facility was developed and used to study the temperature fluctuations, power spectra, gradients and thermal dissipation rate… (more)

Subjects/Keywords: Jets – Fluid dynamics; Flame; Turbulence

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APA (6th Edition):

Wang, G. (2004). Two-point high repetition rate measurement of temperature and thermal dissipation in a turbulent non-premixed jet flame. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/1431

Chicago Manual of Style (16th Edition):

Wang, Guanghua. “Two-point high repetition rate measurement of temperature and thermal dissipation in a turbulent non-premixed jet flame.” 2004. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/1431.

MLA Handbook (7th Edition):

Wang, Guanghua. “Two-point high repetition rate measurement of temperature and thermal dissipation in a turbulent non-premixed jet flame.” 2004. Web. 03 Mar 2021.

Vancouver:

Wang G. Two-point high repetition rate measurement of temperature and thermal dissipation in a turbulent non-premixed jet flame. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2004. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/1431.

Council of Science Editors:

Wang G. Two-point high repetition rate measurement of temperature and thermal dissipation in a turbulent non-premixed jet flame. [Doctoral Dissertation]. University of Texas – Austin; 2004. Available from: http://hdl.handle.net/2152/1431

21. -6956-0215. On understanding the physics and source conditions of the Enceladus South Polar Plume via numerical simulation.

Degree: PhD, Aerospace Engineering, 2015, University of Texas – Austin

 Enceladus, a tiny moon of Saturn, is found to be geologically active. In 2005, Cassini detected an anomalously warm region and a plume, consisting of… (more)

Subjects/Keywords: Enceladus; Numerical simulation; Astronomy; Atmospheric science

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APA (6th Edition):

-6956-0215. (2015). On understanding the physics and source conditions of the Enceladus South Polar Plume via numerical simulation. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/30320

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Chicago Manual of Style (16th Edition):

-6956-0215. “On understanding the physics and source conditions of the Enceladus South Polar Plume via numerical simulation.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/30320.

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Author name may be incomplete

MLA Handbook (7th Edition):

-6956-0215. “On understanding the physics and source conditions of the Enceladus South Polar Plume via numerical simulation.” 2015. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-6956-0215. On understanding the physics and source conditions of the Enceladus South Polar Plume via numerical simulation. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/30320.

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Author name may be incomplete

Council of Science Editors:

-6956-0215. On understanding the physics and source conditions of the Enceladus South Polar Plume via numerical simulation. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/30320

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University of Texas – Austin

22. Jagodzinski, Jeremy James, 1973-. A diode laser-based velocimeter providing point measurements in unseeded flows using modulated filtered Rayleigh scattering (MFRS).

Degree: PhD, Aerospace Engineering, 2007, University of Texas – Austin

 The development to date of a diode-laser based velocimeter providing point-velocitymeasurements in unseeded flows using molecular Rayleigh scattering is discussed. The velocimeter is based on… (more)

Subjects/Keywords: Rayleigh scattering; Laser Doppler velocimeter

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APA (6th Edition):

Jagodzinski, Jeremy James, 1. (2007). A diode laser-based velocimeter providing point measurements in unseeded flows using modulated filtered Rayleigh scattering (MFRS). (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/3782

Chicago Manual of Style (16th Edition):

Jagodzinski, Jeremy James, 1973-. “A diode laser-based velocimeter providing point measurements in unseeded flows using modulated filtered Rayleigh scattering (MFRS).” 2007. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/3782.

MLA Handbook (7th Edition):

Jagodzinski, Jeremy James, 1973-. “A diode laser-based velocimeter providing point measurements in unseeded flows using modulated filtered Rayleigh scattering (MFRS).” 2007. Web. 03 Mar 2021.

Vancouver:

Jagodzinski, Jeremy James 1. A diode laser-based velocimeter providing point measurements in unseeded flows using modulated filtered Rayleigh scattering (MFRS). [Internet] [Doctoral dissertation]. University of Texas – Austin; 2007. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/3782.

Council of Science Editors:

Jagodzinski, Jeremy James 1. A diode laser-based velocimeter providing point measurements in unseeded flows using modulated filtered Rayleigh scattering (MFRS). [Doctoral Dissertation]. University of Texas – Austin; 2007. Available from: http://hdl.handle.net/2152/3782

23. -6542-7353. Application of spontaneous Raman scattering for measurements of thermal non-equilibrium in high-speed mixing and combustion.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 Mixing-induced vibrational non-equilibrium is studied in the turbulent shear layer between a high-speed jet and a surrounding hot-air coflow. The vibrational and rotational temperatures of… (more)

Subjects/Keywords: Raman scattering; Non-equilibrium; Nonequilibrium; Vibrational non-equilibrium; Spontaneous

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APA (6th Edition):

-6542-7353. (2018). Application of spontaneous Raman scattering for measurements of thermal non-equilibrium in high-speed mixing and combustion. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/63684

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Chicago Manual of Style (16th Edition):

-6542-7353. “Application of spontaneous Raman scattering for measurements of thermal non-equilibrium in high-speed mixing and combustion.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/63684.

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MLA Handbook (7th Edition):

-6542-7353. “Application of spontaneous Raman scattering for measurements of thermal non-equilibrium in high-speed mixing and combustion.” 2018. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-6542-7353. Application of spontaneous Raman scattering for measurements of thermal non-equilibrium in high-speed mixing and combustion. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/63684.

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Author name may be incomplete

Council of Science Editors:

-6542-7353. Application of spontaneous Raman scattering for measurements of thermal non-equilibrium in high-speed mixing and combustion. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/63684

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24. -9034-9438. Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample.

Degree: PhD, Aerospace Engineering, 2018, University of Texas – Austin

 When a spacecraft traveling at orbital speeds enters a planetary atmosphere, shock waves and friction heat the surrounding air to temperatures in excess of 6,000… (more)

Subjects/Keywords: Raman scattering; Plasma; ICP; Pyrolysis; Inductively coupled plasma; Ablation; Thermal protection system; Thermal protection; Charring ablator

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APA (6th Edition):

-9034-9438. (2018). Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/72664

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Chicago Manual of Style (16th Edition):

-9034-9438. “Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/72664.

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Author name may be incomplete

MLA Handbook (7th Edition):

-9034-9438. “Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample.” 2018. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-9034-9438. Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/72664.

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Author name may be incomplete

Council of Science Editors:

-9034-9438. Simulation of pyrolysis gas in a charring ablative thermal protection material using gas injection through a porous graphite sample. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/72664

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25. Borysow, Michael. A high-intensity cold atom source.

Degree: PhD, Physics, 2012, University of Texas – Austin

 Presented in this thesis is the design and characterization of a new, high-flux source of cold atoms based on continuous, post-nozzle injection of lithium atoms… (more)

Subjects/Keywords: Physics; Cold atoms; Atomic beam; Supersonic jet; Post-nozzle; Seeded jet; Atom laser; Helium jet; Lithium source; Atomic oven; Cryopump; Cryosorption pump

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APA (6th Edition):

Borysow, M. (2012). A high-intensity cold atom source. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-08-6249

Chicago Manual of Style (16th Edition):

Borysow, Michael. “A high-intensity cold atom source.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2012-08-6249.

MLA Handbook (7th Edition):

Borysow, Michael. “A high-intensity cold atom source.” 2012. Web. 03 Mar 2021.

Vancouver:

Borysow M. A high-intensity cold atom source. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-08-6249.

Council of Science Editors:

Borysow M. A high-intensity cold atom source. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-08-6249

26. Stephani, Kelly Ann. Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness.

Degree: PhD, Aerospace Engineering, 2012, University of Texas – Austin

 This work is focused on the development of a hybrid DSMC/CFD solver to examine hypersonic boundary layer flow over discrete surface roughness. The purpose of… (more)

Subjects/Keywords: DSMC; CFD; Hybrid methods; Chapman-Enskog Theory; Surface roughness

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APA (6th Edition):

Stephani, K. A. (2012). Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-05-5155

Chicago Manual of Style (16th Edition):

Stephani, Kelly Ann. “Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2012-05-5155.

MLA Handbook (7th Edition):

Stephani, Kelly Ann. “Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness.” 2012. Web. 03 Mar 2021.

Vancouver:

Stephani KA. Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5155.

Council of Science Editors:

Stephani KA. Development of a hybrid DSMC/CFD method for hypersonic boundary layer flow over discrete surface roughness. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5155

27. Moore, Christopher Hudson. Monte Carlo simulation of the Jovian plasma torus interaction with Io’s atmosphere and the resultant aurora during eclipse.

Degree: PhD, Aerospace Engineering, 2011, University of Texas – Austin

 Io, the innermost Galilean satellite of Jupiter, exhibits a wide variety of complex phenomena such as interaction with Jupiter’s magnetosphere, volcanic activity, and a rarefied… (more)

Subjects/Keywords: Io; Jovian plasma torus; Aurora; Monte Carlo simulation; DSMC simulation; Atmospheric dynamics; Io's volcanic activity

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APA (6th Edition):

Moore, C. H. (2011). Monte Carlo simulation of the Jovian plasma torus interaction with Io’s atmosphere and the resultant aurora during eclipse. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-08-4245

Chicago Manual of Style (16th Edition):

Moore, Christopher Hudson. “Monte Carlo simulation of the Jovian plasma torus interaction with Io’s atmosphere and the resultant aurora during eclipse.” 2011. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2011-08-4245.

MLA Handbook (7th Edition):

Moore, Christopher Hudson. “Monte Carlo simulation of the Jovian plasma torus interaction with Io’s atmosphere and the resultant aurora during eclipse.” 2011. Web. 03 Mar 2021.

Vancouver:

Moore CH. Monte Carlo simulation of the Jovian plasma torus interaction with Io’s atmosphere and the resultant aurora during eclipse. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2011. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-08-4245.

Council of Science Editors:

Moore CH. Monte Carlo simulation of the Jovian plasma torus interaction with Io’s atmosphere and the resultant aurora during eclipse. [Doctoral Dissertation]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-08-4245

28. Walker, Andrew Charles. A comprehensive numerical model of Io's chemically-reacting sublimation-driven atmosphere and its interaction with the Jovian plasma torus.

Degree: PhD, Aerospace Engineering, 2012, University of Texas – Austin

 Io has one of the most dynamic atmospheres in the solar system due in part to an orbital resonance with Europa and Ganymede that causes… (more)

Subjects/Keywords: Io; Atmospheres; Dynamics; Structure; Jupiter; Satellites; Jovian plasma torus

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APA (6th Edition):

Walker, A. C. (2012). A comprehensive numerical model of Io's chemically-reacting sublimation-driven atmosphere and its interaction with the Jovian plasma torus. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-05-5269

Chicago Manual of Style (16th Edition):

Walker, Andrew Charles. “A comprehensive numerical model of Io's chemically-reacting sublimation-driven atmosphere and its interaction with the Jovian plasma torus.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2012-05-5269.

MLA Handbook (7th Edition):

Walker, Andrew Charles. “A comprehensive numerical model of Io's chemically-reacting sublimation-driven atmosphere and its interaction with the Jovian plasma torus.” 2012. Web. 03 Mar 2021.

Vancouver:

Walker AC. A comprehensive numerical model of Io's chemically-reacting sublimation-driven atmosphere and its interaction with the Jovian plasma torus. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5269.

Council of Science Editors:

Walker AC. A comprehensive numerical model of Io's chemically-reacting sublimation-driven atmosphere and its interaction with the Jovian plasma torus. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5269

29. Morris, Aaron Benjamin. Simulation of rocket plume impingement and dust dispersal on the lunar surface.

Degree: PhD, Aerospace Engineering, 2012, University of Texas – Austin

 When a lander approaches a dusty surface, the plume from the descent engine impinges on the ground and entrains loose regolith into a high velocity… (more)

Subjects/Keywords: Plume-impingement; Direct simulation Monte Carlo; Rarefied gases; Two-phase flow; Granular flow

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APA (6th Edition):

Morris, A. B. (2012). Simulation of rocket plume impingement and dust dispersal on the lunar surface. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-12-6718

Chicago Manual of Style (16th Edition):

Morris, Aaron Benjamin. “Simulation of rocket plume impingement and dust dispersal on the lunar surface.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://hdl.handle.net/2152/ETD-UT-2012-12-6718.

MLA Handbook (7th Edition):

Morris, Aaron Benjamin. “Simulation of rocket plume impingement and dust dispersal on the lunar surface.” 2012. Web. 03 Mar 2021.

Vancouver:

Morris AB. Simulation of rocket plume impingement and dust dispersal on the lunar surface. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-12-6718.

Council of Science Editors:

Morris AB. Simulation of rocket plume impingement and dust dispersal on the lunar surface. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-12-6718

30. -4528-2705. Flame-flow interaction during premixed and stratified swirl flame flashback in an annular swirl combustor.

Degree: PhD, Aerospace Engineering, 2019, University of Texas – Austin

 The interaction between a propagating flame and the approach flow is critical to the understanding of boundary layer flashback of swirling flames. In this work,… (more)

Subjects/Keywords: Flashback; Flame-flow interaction

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APA (6th Edition):

-4528-2705. (2019). Flame-flow interaction during premixed and stratified swirl flame flashback in an annular swirl combustor. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/2074

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Chicago Manual of Style (16th Edition):

-4528-2705. “Flame-flow interaction during premixed and stratified swirl flame flashback in an annular swirl combustor.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed March 03, 2021. http://dx.doi.org/10.26153/tsw/2074.

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MLA Handbook (7th Edition):

-4528-2705. “Flame-flow interaction during premixed and stratified swirl flame flashback in an annular swirl combustor.” 2019. Web. 03 Mar 2021.

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Author name may be incomplete

Vancouver:

-4528-2705. Flame-flow interaction during premixed and stratified swirl flame flashback in an annular swirl combustor. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2021 Mar 03]. Available from: http://dx.doi.org/10.26153/tsw/2074.

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

Council of Science Editors:

-4528-2705. Flame-flow interaction during premixed and stratified swirl flame flashback in an annular swirl combustor. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/2074

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

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