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You searched for +publisher:"University of Texas – Austin" +contributor:("Raja, Laxminarayan L"). Showing records 1 – 29 of 29 total matches.

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1. Deconinck, Thomas Dominique, 1982-. Simulation studies of direct-current microdischarges for electric propulsion.

Degree: PhD, Aerospace Engineering, 2008, University of Texas – Austin

 The structure of direct-current microdischarges is investigated using a detailed two-dimensional multi-species continuum model. Microdischarges are directcurrent discharges that operate at a relatively high pressure… (more)

Subjects/Keywords: Direct-current microdischarges; Multi-species continuum model; Microthrusters; Satellite propulsion

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APA (6th Edition):

Deconinck, Thomas Dominique, 1. (2008). Simulation studies of direct-current microdischarges for electric propulsion. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/7518

Chicago Manual of Style (16th Edition):

Deconinck, Thomas Dominique, 1982-. “Simulation studies of direct-current microdischarges for electric propulsion.” 2008. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/7518.

MLA Handbook (7th Edition):

Deconinck, Thomas Dominique, 1982-. “Simulation studies of direct-current microdischarges for electric propulsion.” 2008. Web. 04 Mar 2021.

Vancouver:

Deconinck, Thomas Dominique 1. Simulation studies of direct-current microdischarges for electric propulsion. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2008. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/7518.

Council of Science Editors:

Deconinck, Thomas Dominique 1. Simulation studies of direct-current microdischarges for electric propulsion. [Doctoral Dissertation]. University of Texas – Austin; 2008. Available from: http://hdl.handle.net/2152/7518

2. Sitaraman, Hariswaran. Magneto-hydrodynamics simulation study of high density thermal plasmas in plasma acceleration devices.

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

 The development of a Magneto-hydrodynamics (MHD) numerical tool to study high density thermal plasmas in plasma acceleration devices is presented. The MHD governing equations represent… (more)

Subjects/Keywords: Magnetohydrodynamics; Electric propulsion; Finite volume methods; Sparse matrix solve; Plasma actuation

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APA (6th Edition):

Sitaraman, H. (2013). Magneto-hydrodynamics simulation study of high density thermal plasmas in plasma acceleration devices. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/21618

Chicago Manual of Style (16th Edition):

Sitaraman, Hariswaran. “Magneto-hydrodynamics simulation study of high density thermal plasmas in plasma acceleration devices.” 2013. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/21618.

MLA Handbook (7th Edition):

Sitaraman, Hariswaran. “Magneto-hydrodynamics simulation study of high density thermal plasmas in plasma acceleration devices.” 2013. Web. 04 Mar 2021.

Vancouver:

Sitaraman H. Magneto-hydrodynamics simulation study of high density thermal plasmas in plasma acceleration devices. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2013. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/21618.

Council of Science Editors:

Sitaraman H. Magneto-hydrodynamics simulation study of high density thermal plasmas in plasma acceleration devices. [Doctoral Dissertation]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/21618

3. Breden, Douglas Paul. Simulations of atmospheric pressure plasma discharges.

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

 This document presents a study of the numerical simulation of non-equilibrium plasma discharges in air mixtures in the atmospheric pressure regime. Such plasma is formed… (more)

Subjects/Keywords: Plasma; Actuator; APPJ; Non-equilibrium

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APA (6th Edition):

Breden, D. P. (2013). Simulations of atmospheric pressure plasma discharges. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/21588

Chicago Manual of Style (16th Edition):

Breden, Douglas Paul. “Simulations of atmospheric pressure plasma discharges.” 2013. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/21588.

MLA Handbook (7th Edition):

Breden, Douglas Paul. “Simulations of atmospheric pressure plasma discharges.” 2013. Web. 04 Mar 2021.

Vancouver:

Breden DP. Simulations of atmospheric pressure plasma discharges. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2013. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/21588.

Council of Science Editors:

Breden DP. Simulations of atmospheric pressure plasma discharges. [Doctoral Dissertation]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/21588

4. -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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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 04, 2021. http://dx.doi.org/10.26153/tsw/1069.

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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. 04 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 04]. 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

5. -7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.

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

 The goal of this research is to reduce the computational cost of a fully unsteady RANS simulation for the multibody interaction problems in the ship… (more)

Subjects/Keywords: Propeller hydrodynamics; BEM/RANS; Hull propeller interaction

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APA (6th Edition):

-7364-0506. (2018). Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68081

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-7364-0506. “Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/68081.

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Author name may be incomplete

MLA Handbook (7th Edition):

-7364-0506. “Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.” 2018. Web. 04 Mar 2021.

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Author name may be incomplete

Vancouver:

-7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/68081.

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Author name may be incomplete

Council of Science Editors:

-7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/68081

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Author name may be incomplete


University of Texas – Austin

6. Karpatne, Anand. Study of compressible flow through a rotating duct.

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

 Several rotorcraft applications such as circulation control and tip jet driven rotors involve internal spanwise flow along the interior of a rotor blade. This dissertation… (more)

Subjects/Keywords: Helicopter; Rotor; Internal flow

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APA (6th Edition):

Karpatne, A. (2015). Study of compressible flow through a rotating duct. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31343

Chicago Manual of Style (16th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/31343.

MLA Handbook (7th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Web. 04 Mar 2021.

Vancouver:

Karpatne A. Study of compressible flow through a rotating duct. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/31343.

Council of Science Editors:

Karpatne A. Study of compressible flow through a rotating duct. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31343


University of Texas – Austin

7. -1376-2608. Application of the three-dimensional viscous/inviscid interaction method on predicting the performance of propulsors with blunt trailing edges.

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

 In this study, a robust and efficient flow separation model coupled with the viscous/inviscid interaction method (VII) is presented to predict the performance of propulsors… (more)

Subjects/Keywords: Viscous/inviscid interaction method; Panel method; Flow separation; Propellers with blunt trailing edges; Propulsors

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APA (6th Edition):

-1376-2608. (2019). Application of the three-dimensional viscous/inviscid interaction method on predicting the performance of propulsors with blunt trailing edges. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/5349

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Chicago Manual of Style (16th Edition):

-1376-2608. “Application of the three-dimensional viscous/inviscid interaction method on predicting the performance of propulsors with blunt trailing edges.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://dx.doi.org/10.26153/tsw/5349.

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Author name may be incomplete

MLA Handbook (7th Edition):

-1376-2608. “Application of the three-dimensional viscous/inviscid interaction method on predicting the performance of propulsors with blunt trailing edges.” 2019. Web. 04 Mar 2021.

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

Vancouver:

-1376-2608. Application of the three-dimensional viscous/inviscid interaction method on predicting the performance of propulsors with blunt trailing edges. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2021 Mar 04]. Available from: http://dx.doi.org/10.26153/tsw/5349.

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

Council of Science Editors:

-1376-2608. Application of the three-dimensional viscous/inviscid interaction method on predicting the performance of propulsors with blunt trailing edges. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/5349

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Author name may be incomplete


University of Texas – Austin

8. -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 04, 2021. http://dx.doi.org/10.26153/tsw/9007.

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MLA Handbook (7th Edition):

-3357-9103. “Multi-physics modeling of electromagnetically driven surface plasma discharges.” 2019. Web. 04 Mar 2021.

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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 04]. Available from: http://dx.doi.org/10.26153/tsw/9007.

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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

9. -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

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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 04, 2021. http://hdl.handle.net/2152/63282.

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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. 04 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 04]. Available from: http://hdl.handle.net/2152/63282.

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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

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 04, 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. 04 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 04]. 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. -3840-5313. The RailPAc arc.

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

 This dissertation will detail work examining the plasma arc of the RailPAc magnetohydrodynamic flow actuator. Initial studies of the RailPAc arc have shown that the… (more)

Subjects/Keywords: Thermal plasma; Gliding arc; High intensity arc; Flow control; Aerospace; Oxidation; Plasma flow actuation

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APA (6th Edition):

-3840-5313. (2018). The RailPAc arc. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68944

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Chicago Manual of Style (16th Edition):

-3840-5313. “The RailPAc arc.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/68944.

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MLA Handbook (7th Edition):

-3840-5313. “The RailPAc arc.” 2018. Web. 04 Mar 2021.

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Author name may be incomplete

Vancouver:

-3840-5313. The RailPAc arc. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/68944.

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

Council of Science Editors:

-3840-5313. The RailPAc arc. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/68944

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Author name may be incomplete


University of Texas – Austin

12. -6239-8796. Modeling and simulation of electromagnetically-interacting low-temperature plasma discharges for actively controlled metamaterials.

Degree: PhD, Aerospace Engineering, 2020, University of Texas – Austin

 In this work, we present a framework for computational modeling of microwave-induced nonthermal plasma discharges interacting with dielectric and conducting structures, with applications to actively-controlled… (more)

Subjects/Keywords: Plasma physics; Electromagnetics; Metamaterials; Fluid modeling; Adaptive refinement; Computational physics

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APA (6th Edition):

-6239-8796. (2020). Modeling and simulation of electromagnetically-interacting low-temperature plasma discharges for actively controlled metamaterials. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/8862

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Chicago Manual of Style (16th Edition):

-6239-8796. “Modeling and simulation of electromagnetically-interacting low-temperature plasma discharges for actively controlled metamaterials.” 2020. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://dx.doi.org/10.26153/tsw/8862.

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Author name may be incomplete

MLA Handbook (7th Edition):

-6239-8796. “Modeling and simulation of electromagnetically-interacting low-temperature plasma discharges for actively controlled metamaterials.” 2020. Web. 04 Mar 2021.

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

Vancouver:

-6239-8796. Modeling and simulation of electromagnetically-interacting low-temperature plasma discharges for actively controlled metamaterials. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2020. [cited 2021 Mar 04]. Available from: http://dx.doi.org/10.26153/tsw/8862.

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Author name may be incomplete

Council of Science Editors:

-6239-8796. Modeling and simulation of electromagnetically-interacting low-temperature plasma discharges for actively controlled metamaterials. [Doctoral Dissertation]. University of Texas – Austin; 2020. Available from: http://dx.doi.org/10.26153/tsw/8862

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Author name may be incomplete


University of Texas – Austin

13. Fontanilla, Adrian Kristopher. Tokamak disruptions : investigations of symptoms and treatments.

Degree: PhD, Physics, 2019, University of Texas – Austin

 Plasma disruptions are a catastrophic loss of confinement that ultimately concludes with the release of the thermal and magnetic energy stored in the vessel containing… (more)

Subjects/Keywords: Plasma; Kinetic equation; Runaway electrons; Pellet ablation; Disruption

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APA (6th Edition):

Fontanilla, A. K. (2019). Tokamak disruptions : investigations of symptoms and treatments. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/5346

Chicago Manual of Style (16th Edition):

Fontanilla, Adrian Kristopher. “Tokamak disruptions : investigations of symptoms and treatments.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://dx.doi.org/10.26153/tsw/5346.

MLA Handbook (7th Edition):

Fontanilla, Adrian Kristopher. “Tokamak disruptions : investigations of symptoms and treatments.” 2019. Web. 04 Mar 2021.

Vancouver:

Fontanilla AK. Tokamak disruptions : investigations of symptoms and treatments. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2021 Mar 04]. Available from: http://dx.doi.org/10.26153/tsw/5346.

Council of Science Editors:

Fontanilla AK. Tokamak disruptions : investigations of symptoms and treatments. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/5346


University of Texas – Austin

14. -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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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 04, 2021. http://hdl.handle.net/2152/69005.

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MLA Handbook (7th Edition):

-0021-1302. “Monte Carlo sensitivity analyses of DSMC parameters for ionizing hypersonic flows.” 2018. Web. 04 Mar 2021.

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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 04]. Available from: http://hdl.handle.net/2152/69005.

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Author name may be incomplete

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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Author name may be incomplete


University of Texas – Austin

15. -6430-5266. A hybridized discontinuous Galerkin method for nonlinear dispersive water waves.

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

 Simulation of water waves near the coast is an important problem in different branches of engineering and mathematics. For mathematical models to be valid in… (more)

Subjects/Keywords: Discontinuous Galerkin; DG; Hybridized; HDG; Nonlinear shallow water; Green-Naghdi; NSWE; GN; Galerkin method; Water waves; Nonlinear water waves; Dispersive water waves; Water wave simulation; Coastal water waves modeling; Korteweg-de Vries equation

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APA (6th Edition):

-6430-5266. (2017). A hybridized discontinuous Galerkin method for nonlinear dispersive water waves. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/47354

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Chicago Manual of Style (16th Edition):

-6430-5266. “A hybridized discontinuous Galerkin method for nonlinear dispersive water waves.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/47354.

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MLA Handbook (7th Edition):

-6430-5266. “A hybridized discontinuous Galerkin method for nonlinear dispersive water waves.” 2017. Web. 04 Mar 2021.

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Author name may be incomplete

Vancouver:

-6430-5266. A hybridized discontinuous Galerkin method for nonlinear dispersive water waves. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/47354.

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Author name may be incomplete

Council of Science Editors:

-6430-5266. A hybridized discontinuous Galerkin method for nonlinear dispersive water waves. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/47354

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University of Texas – Austin

16. -5494-1880. Fast and scalable solvers for high-order hybridized discontinuous Galerkin methods with applications to fluid dynamics and magnetohydrodynamics.

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

 The hybridized discontinuous Galerkin methods (HDG) introduced a decade ago is a promising candidate for high-order spatial discretization combined with implicit/implicit-explicit time stepping. Roughly speaking,… (more)

Subjects/Keywords: Hybridized discontinuous Galerkin; Fast solvers; Multigrid; Multilevel; MHD; Domain decomposition

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APA (6th Edition):

-5494-1880. (2019). Fast and scalable solvers for high-order hybridized discontinuous Galerkin methods with applications to fluid dynamics and magnetohydrodynamics. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/5474

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-5494-1880. “Fast and scalable solvers for high-order hybridized discontinuous Galerkin methods with applications to fluid dynamics and magnetohydrodynamics.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://dx.doi.org/10.26153/tsw/5474.

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Author name may be incomplete

MLA Handbook (7th Edition):

-5494-1880. “Fast and scalable solvers for high-order hybridized discontinuous Galerkin methods with applications to fluid dynamics and magnetohydrodynamics.” 2019. Web. 04 Mar 2021.

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Author name may be incomplete

Vancouver:

-5494-1880. Fast and scalable solvers for high-order hybridized discontinuous Galerkin methods with applications to fluid dynamics and magnetohydrodynamics. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2021 Mar 04]. Available from: http://dx.doi.org/10.26153/tsw/5474.

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Author name may be incomplete

Council of Science Editors:

-5494-1880. Fast and scalable solvers for high-order hybridized discontinuous Galerkin methods with applications to fluid dynamics and magnetohydrodynamics. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/5474

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Author name may be incomplete


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 04, 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. 04 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 04]. 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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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 04, 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. 04 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 04]. 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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19. Berisford, Daniel Floyd. Thermal phenomena and power balance in a helicon plasma.

Degree: PhD, Aerospace Engineering, 2009, University of Texas – Austin

 This work is motivated by the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) experiment. This device uses a helicon antenna to generate a plasma inside a… (more)

Subjects/Keywords: Variable Specific Impulse Magnetoplasma Rocket; VASIMR; Helicon antenna; Plasma; Dielectric tube; Axial magnetic field; Ion cyclotron; Heat fluxes

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APA (6th Edition):

Berisford, D. F. (2009). Thermal phenomena and power balance in a helicon plasma. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/17289

Chicago Manual of Style (16th Edition):

Berisford, Daniel Floyd. “Thermal phenomena and power balance in a helicon plasma.” 2009. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/17289.

MLA Handbook (7th Edition):

Berisford, Daniel Floyd. “Thermal phenomena and power balance in a helicon plasma.” 2009. Web. 04 Mar 2021.

Vancouver:

Berisford DF. Thermal phenomena and power balance in a helicon plasma. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2009. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/17289.

Council of Science Editors:

Berisford DF. Thermal phenomena and power balance in a helicon plasma. [Doctoral Dissertation]. University of Texas – Austin; 2009. Available from: http://hdl.handle.net/2152/17289

20. Chen, Guangye, 1976-. A self-consistent model of helicon discharge.

Degree: PhD, Aerospace Engineering, 2008, University of Texas – Austin

 We developed a self-consistent model of helicon discharges, motivated by a number of applications. One example is a plasma-based space propulsion system that employs a… (more)

Subjects/Keywords: Whistlers (Radio meteorology); Electromagnetic waves; Plasma (Ionized gases)

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APA (6th Edition):

Chen, Guangye, 1. (2008). A self-consistent model of helicon discharge. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/17789

Chicago Manual of Style (16th Edition):

Chen, Guangye, 1976-. “A self-consistent model of helicon discharge.” 2008. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/17789.

MLA Handbook (7th Edition):

Chen, Guangye, 1976-. “A self-consistent model of helicon discharge.” 2008. Web. 04 Mar 2021.

Vancouver:

Chen, Guangye 1. A self-consistent model of helicon discharge. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2008. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/17789.

Council of Science Editors:

Chen, Guangye 1. A self-consistent model of helicon discharge. [Doctoral Dissertation]. University of Texas – Austin; 2008. Available from: http://hdl.handle.net/2152/17789


University of Texas – Austin

21. Kothnur, Prashanth Srinivasa. Simulation of direct current microdischarges for microthruster applications.

Degree: PhD, Aerospace Engineering, 2005, University of Texas – Austin

 The structure of direct-current microdischarges (MDs) is investigated using a detailed two-dimensional multispecies continuum model. MDs are direct-current (DC) discharges that operate at pressures of… (more)

Subjects/Keywords: Space vehicles – Propulsion systems

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APA (6th Edition):

Kothnur, P. S. (2005). Simulation of direct current microdischarges for microthruster applications. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/2254

Chicago Manual of Style (16th Edition):

Kothnur, Prashanth Srinivasa. “Simulation of direct current microdischarges for microthruster applications.” 2005. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/2254.

MLA Handbook (7th Edition):

Kothnur, Prashanth Srinivasa. “Simulation of direct current microdischarges for microthruster applications.” 2005. Web. 04 Mar 2021.

Vancouver:

Kothnur PS. Simulation of direct current microdischarges for microthruster applications. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2005. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/2254.

Council of Science Editors:

Kothnur PS. Simulation of direct current microdischarges for microthruster applications. [Doctoral Dissertation]. University of Texas – Austin; 2005. Available from: http://hdl.handle.net/2152/2254

22. Smith, Colin Healey. Studies of rich and ultra-rich combustion for syngas production.

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

 Syngas is a mixture of hydrogen (H2), carbon monoxide (CO) and other species including nitrogen (N2), water (H2O), methane (CH4) and higher hydrocarbons. Syngas is… (more)

Subjects/Keywords: Combustion; Syngas; Jet fuel; Butanol; Laminar flames; Preheated flames

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APA (6th Edition):

Smith, C. H. (2012). Studies of rich and ultra-rich combustion for syngas production. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/19578

Chicago Manual of Style (16th Edition):

Smith, Colin Healey. “Studies of rich and ultra-rich combustion for syngas production.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/19578.

MLA Handbook (7th Edition):

Smith, Colin Healey. “Studies of rich and ultra-rich combustion for syngas production.” 2012. Web. 04 Mar 2021.

Vancouver:

Smith CH. Studies of rich and ultra-rich combustion for syngas production. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/19578.

Council of Science Editors:

Smith CH. Studies of rich and ultra-rich combustion for syngas production. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/19578

23. Baker, Chad Allan. Simulation, design, and experimental characterization of catalytic and thermoelectric systems for removing emissions and recovering waste energy from engine exhaust.

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

 An analytical transport/reaction model was developed to simulate the catalytic performance of ZnO nanowires as a catalyst support. ZnO nanowires were chosen because they have… (more)

Subjects/Keywords: Thermoelectric; Automotive; Catalyst; Waste heat recovery; Analytical model; Heat exchanger

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APA (6th Edition):

Baker, C. A. (2012). Simulation, design, and experimental characterization of catalytic and thermoelectric systems for removing emissions and recovering waste energy from engine exhaust. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-12-296

Chicago Manual of Style (16th Edition):

Baker, Chad Allan. “Simulation, design, and experimental characterization of catalytic and thermoelectric systems for removing emissions and recovering waste energy from engine exhaust.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/ETD-UT-2012-12-296.

MLA Handbook (7th Edition):

Baker, Chad Allan. “Simulation, design, and experimental characterization of catalytic and thermoelectric systems for removing emissions and recovering waste energy from engine exhaust.” 2012. Web. 04 Mar 2021.

Vancouver:

Baker CA. Simulation, design, and experimental characterization of catalytic and thermoelectric systems for removing emissions and recovering waste energy from engine exhaust. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-12-296.

Council of Science Editors:

Baker CA. Simulation, design, and experimental characterization of catalytic and thermoelectric systems for removing emissions and recovering waste energy from engine exhaust. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-12-296

24. -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 04, 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. 04 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 04]. Available from: http://dx.doi.org/10.26153/tsw/2074.

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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

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25. -8369-8587. DSMC simulations of volatile transport in a transient lunar atmosphere and ice deposition in cold traps after a comet impact.

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

 Over the years, a number of missions have detected signs of water and other volatiles in cold, permanently shadowed regions near the lunar poles, where… (more)

Subjects/Keywords: DSMC; Moon; Volatiles; Comet impacts; Transient lunar atmosphere; Ice deposition; Cold traps; Lunar water transport; Lunar water sequestration; Lunar comet impacts; Impact-delivered volatiles; Volatile-rich impact; Lunar atmosphere; Lunar impact simulations; Antipodal vapor; Lunar water distribution; Lunar rough surface temperature model; Lunar radiative heat transfer; Lunar impact-delivered water

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APA (6th Edition):

-8369-8587. (2017). DSMC simulations of volatile transport in a transient lunar atmosphere and ice deposition in cold traps after a comet impact. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/47280

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Chicago Manual of Style (16th Edition):

-8369-8587. “DSMC simulations of volatile transport in a transient lunar atmosphere and ice deposition in cold traps after a comet impact.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/47280.

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Author name may be incomplete

MLA Handbook (7th Edition):

-8369-8587. “DSMC simulations of volatile transport in a transient lunar atmosphere and ice deposition in cold traps after a comet impact.” 2017. Web. 04 Mar 2021.

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

Vancouver:

-8369-8587. DSMC simulations of volatile transport in a transient lunar atmosphere and ice deposition in cold traps after a comet impact. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/47280.

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Author name may be incomplete

Council of Science Editors:

-8369-8587. DSMC simulations of volatile transport in a transient lunar atmosphere and ice deposition in cold traps after a comet impact. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/47280

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University of Texas – Austin

26. Min, Timothy T. Computational studies of electron transport and reaction rate models for argon plasma.

Degree: MSin Engineering, Aerospace Engineering, 2010, University of Texas – Austin

 A validation study was performed on a capacitively coupled argon discharge to determine the most suitable models for chemistry and electron transport. Chemical reaction rate… (more)

Subjects/Keywords: Argon; Capacitively coupled plasma discharge; Modeling; Models; Glow discharge; Electron transport

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APA (6th Edition):

Min, T. T. (2010). Computational studies of electron transport and reaction rate models for argon plasma. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2010-08-1877

Chicago Manual of Style (16th Edition):

Min, Timothy T. “Computational studies of electron transport and reaction rate models for argon plasma.” 2010. Masters Thesis, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/ETD-UT-2010-08-1877.

MLA Handbook (7th Edition):

Min, Timothy T. “Computational studies of electron transport and reaction rate models for argon plasma.” 2010. Web. 04 Mar 2021.

Vancouver:

Min TT. Computational studies of electron transport and reaction rate models for argon plasma. [Internet] [Masters thesis]. University of Texas – Austin; 2010. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/ETD-UT-2010-08-1877.

Council of Science Editors:

Min TT. Computational studies of electron transport and reaction rate models for argon plasma. [Masters Thesis]. University of Texas – Austin; 2010. Available from: http://hdl.handle.net/2152/ETD-UT-2010-08-1877


University of Texas – Austin

27. Narayanaswamy, Venkateswa. Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control.

Degree: PhD, Aerospace Engineering, 2010, University of Texas – Austin

 A pulsed-plasma jet (called a "spark-jet" by other researchers), is a high-speed synthetic jet that is generated by striking an electrical discharge in a small… (more)

Subjects/Keywords: Shock wave boundary layer interaction; Plasma flow control; Pulsed jets; Spark-jet; Pulsed-plasma jet; Supersonic flow control; Flow control; Separation shock

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APA (6th Edition):

Narayanaswamy, V. (2010). Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2010-05-1400

Chicago Manual of Style (16th Edition):

Narayanaswamy, Venkateswa. “Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control.” 2010. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/ETD-UT-2010-05-1400.

MLA Handbook (7th Edition):

Narayanaswamy, Venkateswa. “Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control.” 2010. Web. 04 Mar 2021.

Vancouver:

Narayanaswamy V. Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2010. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1400.

Council of Science Editors:

Narayanaswamy V. Investigation of a pulsed-plasma jet for separation shock/boundary layer interaction control. [Doctoral Dissertation]. University of Texas – Austin; 2010. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1400


University of Texas – Austin

28. Gamba, Mirko. Volumetric PIV and OH PLIF imaging in the far field of nonpremixed jet flames.

Degree: PhD, Aerospace Engineering, 2009, University of Texas – Austin

 Cinematographic stereoscopic PIV, combined with Taylor's frozen flow hypothesis, is used to generate three-dimensional (3D) quasi-instantaneous pseudo volumes of the three-component (3C) velocity field in… (more)

Subjects/Keywords: Volumetric PIV OH PLIF Nonpremixed flame

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APA (6th Edition):

Gamba, M. (2009). Volumetric PIV and OH PLIF imaging in the far field of nonpremixed jet flames. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2009-05-161

Chicago Manual of Style (16th Edition):

Gamba, Mirko. “Volumetric PIV and OH PLIF imaging in the far field of nonpremixed jet flames.” 2009. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/ETD-UT-2009-05-161.

MLA Handbook (7th Edition):

Gamba, Mirko. “Volumetric PIV and OH PLIF imaging in the far field of nonpremixed jet flames.” 2009. Web. 04 Mar 2021.

Vancouver:

Gamba M. Volumetric PIV and OH PLIF imaging in the far field of nonpremixed jet flames. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2009. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/ETD-UT-2009-05-161.

Council of Science Editors:

Gamba M. Volumetric PIV and OH PLIF imaging in the far field of nonpremixed jet flames. [Doctoral Dissertation]. University of Texas – Austin; 2009. Available from: http://hdl.handle.net/2152/ETD-UT-2009-05-161


University of Texas – Austin

29. Mahadevan, Shankar, 1982-. Simulation of direct-current surface plasma discharges in air for supersonic flow control.

Degree: PhD, Aerospace Engineering, 2010, University of Texas – Austin

 Computational simulations of air glow discharge plasma in the presence of supersonic flow are presented. The glow discharge model is based on a self-consistent, multi-species,… (more)

Subjects/Keywords: Plasma flow control; Plasma simulation; Glow discharges

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APA (6th Edition):

Mahadevan, Shankar, 1. (2010). Simulation of direct-current surface plasma discharges in air for supersonic flow control. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2010-05-1365

Chicago Manual of Style (16th Edition):

Mahadevan, Shankar, 1982-. “Simulation of direct-current surface plasma discharges in air for supersonic flow control.” 2010. Doctoral Dissertation, University of Texas – Austin. Accessed March 04, 2021. http://hdl.handle.net/2152/ETD-UT-2010-05-1365.

MLA Handbook (7th Edition):

Mahadevan, Shankar, 1982-. “Simulation of direct-current surface plasma discharges in air for supersonic flow control.” 2010. Web. 04 Mar 2021.

Vancouver:

Mahadevan, Shankar 1. Simulation of direct-current surface plasma discharges in air for supersonic flow control. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2010. [cited 2021 Mar 04]. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1365.

Council of Science Editors:

Mahadevan, Shankar 1. Simulation of direct-current surface plasma discharges in air for supersonic flow control. [Doctoral Dissertation]. University of Texas – Austin; 2010. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1365

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