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You searched for +publisher:"University of Texas – Austin" +contributor:("Goldstein, David"). Showing records 1 – 30 of 35 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 January 24, 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. 24 Jan 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 Jan 24]. 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 January 24, 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. 24 Jan 2021.

Vancouver:

Tovar SA. Simulation of LCROSS hydroxyl band strength data. [Internet] [Masters thesis]. University of Texas – Austin; 2019. [cited 2021 Jan 24]. 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. -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 January 24, 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. 24 Jan 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 Jan 24]. 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

4. Cameron, Christopher Glenn. Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system.

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

 With the renewed interest in rigid, counter-rotating coaxial rotor designs, and the increased fidelity of fully coupled CFD/CSD simulations, there exists a lack of comprehensive… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Coaxial; Operational Modal Analysis; Aeroelasticity; Counter-rotating rotor systems; Rotor systems; Rotor designs

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APA (6th Edition):

Cameron, C. G. (2016). Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/47136

Chicago Manual of Style (16th Edition):

Cameron, Christopher Glenn. “Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/47136.

MLA Handbook (7th Edition):

Cameron, Christopher Glenn. “Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system.” 2016. Web. 24 Jan 2021.

Vancouver:

Cameron CG. Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/47136.

Council of Science Editors:

Cameron CG. Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/47136


University of Texas – Austin

5. Yang, Shan. A shape Hessian-based analysis of roughness effects on fluid flows.

Degree: PhD, Computational and Applied Mathematics, 2011, University of Texas – Austin

 The flow of fluids over solid surfaces is an integral part of many technologies, and the analysis of such flows is important to the design… (more)

Subjects/Keywords: Roughness analysis; Shape calculus; Navier-Stokes flow

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APA (6th Edition):

Yang, S. (2011). A shape Hessian-based analysis of roughness effects on fluid flows. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2011-08-4036

Chicago Manual of Style (16th Edition):

Yang, Shan. “A shape Hessian-based analysis of roughness effects on fluid flows.” 2011. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/ETD-UT-2011-08-4036.

MLA Handbook (7th Edition):

Yang, Shan. “A shape Hessian-based analysis of roughness effects on fluid flows.” 2011. Web. 24 Jan 2021.

Vancouver:

Yang S. A shape Hessian-based analysis of roughness effects on fluid flows. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/ETD-UT-2011-08-4036.

Council of Science Editors:

Yang S. A shape Hessian-based analysis of roughness effects on fluid flows. [Doctoral Dissertation]. University of Texas – Austin; 2011. Available from: http://hdl.handle.net/2152/ETD-UT-2011-08-4036


University of Texas – Austin

6. Uehara, Daiju. Estimation of helicopter rotor loads from blade structural response.

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

 Measuring the load distribution along a helicopter rotor blade has been one of the most challenging tasks in experimental aeromechanics. Conventional loads measurements with on-blade… (more)

Subjects/Keywords: Rotorcraft; Structural dynamics; Aeromechanics; Digital image correlation; Force reconstruction; Operational modal analysis

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APA (6th Edition):

Uehara, D. (2020). Estimation of helicopter rotor loads from blade structural response. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/8353

Chicago Manual of Style (16th Edition):

Uehara, Daiju. “Estimation of helicopter rotor loads from blade structural response.” 2020. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://dx.doi.org/10.26153/tsw/8353.

MLA Handbook (7th Edition):

Uehara, Daiju. “Estimation of helicopter rotor loads from blade structural response.” 2020. Web. 24 Jan 2021.

Vancouver:

Uehara D. Estimation of helicopter rotor loads from blade structural response. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2020. [cited 2021 Jan 24]. Available from: http://dx.doi.org/10.26153/tsw/8353.

Council of Science Editors:

Uehara D. Estimation of helicopter rotor loads from blade structural response. [Doctoral Dissertation]. University of Texas – Austin; 2020. Available from: http://dx.doi.org/10.26153/tsw/8353


University of Texas – Austin

7. Strand, James Stephen. Statistical methods for the analysis of DSMC simulations of hypersonic shocks.

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

 In this work, statistical techniques were employed to study the modeling of a hypersonic shock with the Direct Simulation Monte Carlo (DSMC) method, and to… (more)

Subjects/Keywords: DSMC; MCMC; Sensitivity analysis

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APA (6th Edition):

Strand, J. S. (2012). Statistical methods for the analysis of DSMC simulations of hypersonic shocks. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-05-5384

Chicago Manual of Style (16th Edition):

Strand, James Stephen. “Statistical methods for the analysis of DSMC simulations of hypersonic shocks.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/ETD-UT-2012-05-5384.

MLA Handbook (7th Edition):

Strand, James Stephen. “Statistical methods for the analysis of DSMC simulations of hypersonic shocks.” 2012. Web. 24 Jan 2021.

Vancouver:

Strand JS. Statistical methods for the analysis of DSMC simulations of hypersonic shocks. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5384.

Council of Science Editors:

Strand JS. Statistical methods for the analysis of DSMC simulations of hypersonic shocks. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5384


University of Texas – Austin

8. 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 January 24, 2021. http://hdl.handle.net/2152/31343.

MLA Handbook (7th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Web. 24 Jan 2021.

Vancouver:

Karpatne A. Study of compressible flow through a rotating duct. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Jan 24]. 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

9. -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 January 24, 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. 24 Jan 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 Jan 24]. 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


University of Texas – Austin

10. -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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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-3840-5313. “The RailPAc arc.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/68944.

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

MLA Handbook (7th Edition):

-3840-5313. “The RailPAc arc.” 2018. Web. 24 Jan 2021.

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

Vancouver:

-3840-5313. The RailPAc arc. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2021 Jan 24]. 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

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


University of Texas – Austin

11. -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

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

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 January 24, 2021. http://dx.doi.org/10.26153/tsw/8862.

Note: this citation may be lacking information needed for this citation format:
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. 24 Jan 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 Jan 24]. Available from: http://dx.doi.org/10.26153/tsw/8862.

Note: this citation may be lacking information needed for this citation format:
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

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


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 January 24, 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. 24 Jan 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 Jan 24]. 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. 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 January 24, 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. 24 Jan 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 Jan 24]. 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

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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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 January 24, 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. 24 Jan 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 Jan 24]. Available from: http://hdl.handle.net/2152/69005.

Note: this citation may be lacking information needed for this citation format:
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. -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 January 24, 2021. http://hdl.handle.net/2152/32821.

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Author name may be incomplete

MLA Handbook (7th Edition):

-5890-8543. “Realistic simulation of Io's Pele plume and its effects on Io's atmosphere.” 2015. Web. 24 Jan 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 Jan 24]. 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

16. -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 January 24, 2021. http://hdl.handle.net/2152/71466.

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Author name may be incomplete

MLA Handbook (7th Edition):

-8909-3631. “Multi-physics computational modeling of electromagnetic acceleration devices.” 2018. Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
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 Jan 24]. Available from: http://hdl.handle.net/2152/71466.

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


University of Texas – Austin

17. -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 January 24, 2021. http://hdl.handle.net/2152/63474.

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Author name may be incomplete

MLA Handbook (7th Edition):

-3650-2649. “Rarefied gas dynamic simulations of planetary atmospheric systems.” 2018. Web. 24 Jan 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 Jan 24]. 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

18. Lamb, Justin Meredith. Parametric study of LCROSS impact plume.

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

 In 2009, NASA's LCROSS mission impacted Cabeus Crater near the Lunar South Pole with the spent Centaur upper stage rocket. The impact was observed by… (more)

Subjects/Keywords: LCROSS; Lunar; Moon; Parametric, NASA; Plume; Impact; Cabeus; Spectral; Grain; Radiance

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APA (6th Edition):

Lamb, J. M. (2013). Parametric study of LCROSS impact plume. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/23794

Chicago Manual of Style (16th Edition):

Lamb, Justin Meredith. “Parametric study of LCROSS impact plume.” 2013. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/23794.

MLA Handbook (7th Edition):

Lamb, Justin Meredith. “Parametric study of LCROSS impact plume.” 2013. Web. 24 Jan 2021.

Vancouver:

Lamb JM. Parametric study of LCROSS impact plume. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/23794.

Council of Science Editors:

Lamb JM. Parametric study of LCROSS impact plume. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/23794

19. Karpatne, Anand, 1987-. Investigation of tip vortex aperiodicity in hover.

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

 Previous research has indicated aperiodicity in the positions of tip vortices emitted from a helicopter rotor blade in hover. The objective of the current study… (more)

Subjects/Keywords: Rotor wake modeling; Tip vortices; Vortex rings; Jitter; Aperiodicity

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APA (6th Edition):

Karpatne, Anand, 1. (2012). Investigation of tip vortex aperiodicity in hover. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-08-6278

Chicago Manual of Style (16th Edition):

Karpatne, Anand, 1987-. “Investigation of tip vortex aperiodicity in hover.” 2012. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/ETD-UT-2012-08-6278.

MLA Handbook (7th Edition):

Karpatne, Anand, 1987-. “Investigation of tip vortex aperiodicity in hover.” 2012. Web. 24 Jan 2021.

Vancouver:

Karpatne, Anand 1. Investigation of tip vortex aperiodicity in hover. [Internet] [Masters thesis]. University of Texas – Austin; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-08-6278.

Council of Science Editors:

Karpatne, Anand 1. Investigation of tip vortex aperiodicity in hover. [Masters Thesis]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-08-6278

20. Berg, Jared James. Simulating water vapor plumes on Europa.

Degree: MSin Engineering, Aerospace engineering, 2015, University of Texas – Austin

 A computational investigation of water vapor plumes on the Jovian moon Europa was performed with a focus on characteristics relevant to observation and spacecraft mission… (more)

Subjects/Keywords: Europa; Plume; DSMC

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APA (6th Edition):

Berg, J. J. (2015). Simulating water vapor plumes on Europa. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/34041

Chicago Manual of Style (16th Edition):

Berg, Jared James. “Simulating water vapor plumes on Europa.” 2015. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/34041.

MLA Handbook (7th Edition):

Berg, Jared James. “Simulating water vapor plumes on Europa.” 2015. Web. 24 Jan 2021.

Vancouver:

Berg JJ. Simulating water vapor plumes on Europa. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/34041.

Council of Science Editors:

Berg JJ. Simulating water vapor plumes on Europa. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/34041

21. Doolittle, Charles Jae, 1985-. Near-field flow structures and transient growth due to subcritical surface roughness.

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

 An immersed boundary spectral method is used to simulate laminar boundary layer flow over a periodic array of cylindrical surface roughness elements. Direct comparisons are… (more)

Subjects/Keywords: Fluid dynamics; Transition; Surface roughness; DNS; Direct numerical simulation

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APA (6th Edition):

Doolittle, Charles Jae, 1. (2010). Near-field flow structures and transient growth due to subcritical surface roughness. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2010-05-1456

Chicago Manual of Style (16th Edition):

Doolittle, Charles Jae, 1985-. “Near-field flow structures and transient growth due to subcritical surface roughness.” 2010. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/ETD-UT-2010-05-1456.

MLA Handbook (7th Edition):

Doolittle, Charles Jae, 1985-. “Near-field flow structures and transient growth due to subcritical surface roughness.” 2010. Web. 24 Jan 2021.

Vancouver:

Doolittle, Charles Jae 1. Near-field flow structures and transient growth due to subcritical surface roughness. [Internet] [Masters thesis]. University of Texas – Austin; 2010. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1456.

Council of Science Editors:

Doolittle, Charles Jae 1. Near-field flow structures and transient growth due to subcritical surface roughness. [Masters Thesis]. University of Texas – Austin; 2010. Available from: http://hdl.handle.net/2152/ETD-UT-2010-05-1456

22. Drews, Scott David, 1987-. Direct numerical simulations of flow past quasi-random distributed roughness.

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

 low about a periodic array of quasi-random distributed roughness is examined using an immersed boundary spectral method. Verification of the code used in the simulations… (more)

Subjects/Keywords: Boundary layer transition; DNS; Roughness induced transition; Laminar transition

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APA (6th Edition):

Drews, Scott David, 1. (2012). Direct numerical simulations of flow past quasi-random distributed roughness. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/ETD-UT-2012-05-5333

Chicago Manual of Style (16th Edition):

Drews, Scott David, 1987-. “Direct numerical simulations of flow past quasi-random distributed roughness.” 2012. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/ETD-UT-2012-05-5333.

MLA Handbook (7th Edition):

Drews, Scott David, 1987-. “Direct numerical simulations of flow past quasi-random distributed roughness.” 2012. Web. 24 Jan 2021.

Vancouver:

Drews, Scott David 1. Direct numerical simulations of flow past quasi-random distributed roughness. [Internet] [Masters thesis]. University of Texas – Austin; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5333.

Council of Science Editors:

Drews, Scott David 1. Direct numerical simulations of flow past quasi-random distributed roughness. [Masters Thesis]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/ETD-UT-2012-05-5333

23. Agrawal, Aayush. Sublimation and photodissociation in the LCROSS ejecta plume : effects of lunar material.

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

 The National Aeronautics and Space Administration (NASA) launched the Lunar Crater Observing and Sensing Satellite (LCROSS) mission to confirm the presence/absence of water ice and… (more)

Subjects/Keywords: LCROSS; Lunar Crater Observing and Sensing Satellite; Ice photodissociation; LCROSS ejecta plume; Lunar regolith; Regolith inclusions; Observed hydroxyl; Impact plume

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APA (6th Edition):

Agrawal, A. (2019). Sublimation and photodissociation in the LCROSS ejecta plume : effects of lunar material. (Masters Thesis). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/2863

Chicago Manual of Style (16th Edition):

Agrawal, Aayush. “Sublimation and photodissociation in the LCROSS ejecta plume : effects of lunar material.” 2019. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://dx.doi.org/10.26153/tsw/2863.

MLA Handbook (7th Edition):

Agrawal, Aayush. “Sublimation and photodissociation in the LCROSS ejecta plume : effects of lunar material.” 2019. Web. 24 Jan 2021.

Vancouver:

Agrawal A. Sublimation and photodissociation in the LCROSS ejecta plume : effects of lunar material. [Internet] [Masters thesis]. University of Texas – Austin; 2019. [cited 2021 Jan 24]. Available from: http://dx.doi.org/10.26153/tsw/2863.

Council of Science Editors:

Agrawal A. Sublimation and photodissociation in the LCROSS ejecta plume : effects of lunar material. [Masters Thesis]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/2863

24. -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 January 24, 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. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
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 Jan 24]. 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

25. Lee, Conrad Yuan Yuen. Direct numerical simulation of microjets for turbulent boundary layer control.

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

 A direct numerical simulation approach is used to simulate an array of MEMS slot jets in a turbulent boundary layer for the purposes of flow… (more)

Subjects/Keywords: Boundary layer control – Simulation methods; Turbulent boundary layer – Simulation methods; Jets – Simulation methods; Actuators

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APA (6th Edition):

Lee, C. Y. Y. (2004). Direct numerical simulation of microjets for turbulent boundary layer control. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/1229

Chicago Manual of Style (16th Edition):

Lee, Conrad Yuan Yuen. “Direct numerical simulation of microjets for turbulent boundary layer control.” 2004. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/1229.

MLA Handbook (7th Edition):

Lee, Conrad Yuan Yuen. “Direct numerical simulation of microjets for turbulent boundary layer control.” 2004. Web. 24 Jan 2021.

Vancouver:

Lee CYY. Direct numerical simulation of microjets for turbulent boundary layer control. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2004. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/1229.

Council of Science Editors:

Lee CYY. Direct numerical simulation of microjets for turbulent boundary layer control. [Doctoral Dissertation]. University of Texas – Austin; 2004. Available from: http://hdl.handle.net/2152/1229

26. Rojo, Raymondo Mendivil, III. End-effects regime study in full-scale and laboratory scale setups.

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

 Full-scale launch data from a cluster of three rocket engines employing a Thrust Optimized Parabolic contour nozzle and hot gas was compared with a laboratory-scale… (more)

Subjects/Keywords: Acoustics; Rocket; Fluid dynamics; Nozzle; Full scale

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APA (6th Edition):

Rojo, Raymondo Mendivil, I. (2015). End-effects regime study in full-scale and laboratory scale setups. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/32846

Chicago Manual of Style (16th Edition):

Rojo, Raymondo Mendivil, III. “End-effects regime study in full-scale and laboratory scale setups.” 2015. Masters Thesis, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/32846.

MLA Handbook (7th Edition):

Rojo, Raymondo Mendivil, III. “End-effects regime study in full-scale and laboratory scale setups.” 2015. Web. 24 Jan 2021.

Vancouver:

Rojo, Raymondo Mendivil I. End-effects regime study in full-scale and laboratory scale setups. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/32846.

Council of Science Editors:

Rojo, Raymondo Mendivil I. End-effects regime study in full-scale and laboratory scale setups. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/32846

27. Donde, Pratik Prakash. LES/PDF approach for turbulent reacting flows.

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

 The probability density function (PDF) approach is a powerful technique for large eddy simulation (LES) based modeling of turbulent reacting flows. In this approach, the… (more)

Subjects/Keywords: Probability density function approach; Large eddy simulation; Supersonic combustion modeling; Soot modeling; Turbulent reacting flows; Direct quadrature method of moments; Semi-discrete quadrature method of moments; Quadrature based methods; Lagrangian Monte Carlo methods; Supersonic combustors; Flame stabilization; Polycyclic aromatic hydrocarbons; Soot-turbulence-chemistry interactions; Shock-turbulence-chemistry interactions

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APA (6th Edition):

Donde, P. P. (2012). LES/PDF approach for turbulent reacting flows. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/19481

Chicago Manual of Style (16th Edition):

Donde, Pratik Prakash. “LES/PDF approach for turbulent reacting flows.” 2012. Doctoral Dissertation, University of Texas – Austin. Accessed January 24, 2021. http://hdl.handle.net/2152/19481.

MLA Handbook (7th Edition):

Donde, Pratik Prakash. “LES/PDF approach for turbulent reacting flows.” 2012. Web. 24 Jan 2021.

Vancouver:

Donde PP. LES/PDF approach for turbulent reacting flows. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2152/19481.

Council of Science Editors:

Donde PP. LES/PDF approach for turbulent reacting flows. [Doctoral Dissertation]. University of Texas – Austin; 2012. Available from: http://hdl.handle.net/2152/19481

28. 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 January 24, 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. 24 Jan 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 Jan 24]. 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

29. 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 January 24, 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. 24 Jan 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 Jan 24]. 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

30. 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 January 24, 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. 24 Jan 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 Jan 24]. 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

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