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You searched for +publisher:"University of Michigan" +contributor:("Fidkowski, Krzysztof J"). Showing records 1 – 30 of 55 total matches.

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University of Michigan

1. Lung, Tyler B. Toward a Simple, Accurate Lagrangian Hydrocode.

Degree: PhD, Aerospace Engineering, 2015, University of Michigan

 Lagrangian hydrocodes play an important role in the computation of transient, compressible, multi-material flows. This research was aimed at developing a simply constructed cell-centered Lagrangian… (more)

Subjects/Keywords: Lagrangian hydrodynamics; temporal flux limiter; vorticity preserving Lax-Wendroff; mesh imprinting; linear acoustics; flux-corrected transport; Aerospace Engineering; Engineering

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APA (6th Edition):

Lung, T. B. (2015). Toward a Simple, Accurate Lagrangian Hydrocode. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/113577

Chicago Manual of Style (16th Edition):

Lung, Tyler B. “Toward a Simple, Accurate Lagrangian Hydrocode.” 2015. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/113577.

MLA Handbook (7th Edition):

Lung, Tyler B. “Toward a Simple, Accurate Lagrangian Hydrocode.” 2015. Web. 16 Apr 2021.

Vancouver:

Lung TB. Toward a Simple, Accurate Lagrangian Hydrocode. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/113577.

Council of Science Editors:

Lung TB. Toward a Simple, Accurate Lagrangian Hydrocode. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/113577


University of Michigan

2. Amur Varadarajan, Prasanna. Noise Transmission along Shock Waves.

Degree: PhD, Aerospace Engineering, 2011, University of Michigan

 Shocks at the inlet of scramjet engines are subject to perturbations from their interaction with turbulent boundary layer. DNS results for this interaction indicate the… (more)

Subjects/Keywords: Perturbations Along the Shocks Due to Vortex Interaction; Aerospace Engineering; Engineering

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APA (6th Edition):

Amur Varadarajan, P. (2011). Noise Transmission along Shock Waves. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/89612

Chicago Manual of Style (16th Edition):

Amur Varadarajan, Prasanna. “Noise Transmission along Shock Waves.” 2011. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/89612.

MLA Handbook (7th Edition):

Amur Varadarajan, Prasanna. “Noise Transmission along Shock Waves.” 2011. Web. 16 Apr 2021.

Vancouver:

Amur Varadarajan P. Noise Transmission along Shock Waves. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/89612.

Council of Science Editors:

Amur Varadarajan P. Noise Transmission along Shock Waves. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/89612


University of Michigan

3. Kast, Steven Michael. Methods for Optimal Output Prediction in Computational Fluid Dynamics.

Degree: PhD, Aerospace Engineering, 2016, University of Michigan

 In a Computational Fluid Dynamics (CFD) simulation, not all data is of equal importance. Instead, the goal of the user is often to compute certain… (more)

Subjects/Keywords: Unsteady adjoint; Output error estimation; Deforming domains; Discontinuous Galerkin; Discontinuous Petrov-Galerkin; Optimal test functions; Aerospace Engineering; Computer Science; Engineering

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APA (6th Edition):

Kast, S. M. (2016). Methods for Optimal Output Prediction in Computational Fluid Dynamics. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/133418

Chicago Manual of Style (16th Edition):

Kast, Steven Michael. “Methods for Optimal Output Prediction in Computational Fluid Dynamics.” 2016. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/133418.

MLA Handbook (7th Edition):

Kast, Steven Michael. “Methods for Optimal Output Prediction in Computational Fluid Dynamics.” 2016. Web. 16 Apr 2021.

Vancouver:

Kast SM. Methods for Optimal Output Prediction in Computational Fluid Dynamics. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/133418.

Council of Science Editors:

Kast SM. Methods for Optimal Output Prediction in Computational Fluid Dynamics. [Doctoral Dissertation]. University of Michigan; 2016. Available from: http://hdl.handle.net/2027.42/133418


University of Michigan

4. Medeiros, Renato. Model Order Reduction for Aeroelastic Analysis of Very Flexible Aircraft.

Degree: PhD, Aerospace Engineering, 2019, University of Michigan

 With increasing requirements for lower emissions and costs, next-generation transport aircraft are poised to deal with high-aspect-ratio wings. Long light-weight structures are naturally flexible, and… (more)

Subjects/Keywords: reduced order models; very flexible aircraft; aeroelastic analysis; Aerospace Engineering; Engineering

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APA (6th Edition):

Medeiros, R. (2019). Model Order Reduction for Aeroelastic Analysis of Very Flexible Aircraft. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/153455

Chicago Manual of Style (16th Edition):

Medeiros, Renato. “Model Order Reduction for Aeroelastic Analysis of Very Flexible Aircraft.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/153455.

MLA Handbook (7th Edition):

Medeiros, Renato. “Model Order Reduction for Aeroelastic Analysis of Very Flexible Aircraft.” 2019. Web. 16 Apr 2021.

Vancouver:

Medeiros R. Model Order Reduction for Aeroelastic Analysis of Very Flexible Aircraft. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/153455.

Council of Science Editors:

Medeiros R. Model Order Reduction for Aeroelastic Analysis of Very Flexible Aircraft. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/153455


University of Michigan

5. Lin, Hsun-Chia. Thermal Hydraulics System-Level Code Validation and Transient Analyses for Fluoride Salt-Cooled High-Temperature Reactors.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2020, University of Michigan

 Verification and validation (V&V) of thermal hydraulics analysis codes for fluoride salt-cooled high-temperature reactors (FHRs) is identified as one of the key tasks that need… (more)

Subjects/Keywords: FHR; AHTR; RELAP5; SAM; natural circulation; DRACS; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Lin, H. (2020). Thermal Hydraulics System-Level Code Validation and Transient Analyses for Fluoride Salt-Cooled High-Temperature Reactors. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/155105

Chicago Manual of Style (16th Edition):

Lin, Hsun-Chia. “Thermal Hydraulics System-Level Code Validation and Transient Analyses for Fluoride Salt-Cooled High-Temperature Reactors.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/155105.

MLA Handbook (7th Edition):

Lin, Hsun-Chia. “Thermal Hydraulics System-Level Code Validation and Transient Analyses for Fluoride Salt-Cooled High-Temperature Reactors.” 2020. Web. 16 Apr 2021.

Vancouver:

Lin H. Thermal Hydraulics System-Level Code Validation and Transient Analyses for Fluoride Salt-Cooled High-Temperature Reactors. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/155105.

Council of Science Editors:

Lin H. Thermal Hydraulics System-Level Code Validation and Transient Analyses for Fluoride Salt-Cooled High-Temperature Reactors. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/155105


University of Michigan

6. Shimizu, Yukiko. Output-Based Error Estimation and Model Reduction for Chaotic Flows.

Degree: PhD, Aerospace Engineering, 2019, University of Michigan

 Turbulent flows are characterized by chaotic variations in state variables and are commonly found in many applications such as jet engine mixing and flow over… (more)

Subjects/Keywords: Computational Fluid Dynamics, Chaos; Aerospace Engineering; Engineering

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APA (6th Edition):

Shimizu, Y. (2019). Output-Based Error Estimation and Model Reduction for Chaotic Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/149954

Chicago Manual of Style (16th Edition):

Shimizu, Yukiko. “Output-Based Error Estimation and Model Reduction for Chaotic Flows.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/149954.

MLA Handbook (7th Edition):

Shimizu, Yukiko. “Output-Based Error Estimation and Model Reduction for Chaotic Flows.” 2019. Web. 16 Apr 2021.

Vancouver:

Shimizu Y. Output-Based Error Estimation and Model Reduction for Chaotic Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/149954.

Council of Science Editors:

Shimizu Y. Output-Based Error Estimation and Model Reduction for Chaotic Flows. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/149954


University of Michigan

7. Chen, Samuel. Modeling of Material-Environment Interactions for Hypersonic Thermal Protection Systems.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 Hypersonic vehicles operate in extreme conditions, experiencing high heating loads, gas temperatures often exceeding 10,000 K in the shock layer, and oxidizing environments. Thermal protection… (more)

Subjects/Keywords: material-environment interaction; hypersonics; ablation; ultra high temperature ceramic; silicon carbide; oxidation; Aerospace Engineering; Engineering

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APA (6th Edition):

Chen, S. (2020). Modeling of Material-Environment Interactions for Hypersonic Thermal Protection Systems. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163164

Chicago Manual of Style (16th Edition):

Chen, Samuel. “Modeling of Material-Environment Interactions for Hypersonic Thermal Protection Systems.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/163164.

MLA Handbook (7th Edition):

Chen, Samuel. “Modeling of Material-Environment Interactions for Hypersonic Thermal Protection Systems.” 2020. Web. 16 Apr 2021.

Vancouver:

Chen S. Modeling of Material-Environment Interactions for Hypersonic Thermal Protection Systems. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/163164.

Council of Science Editors:

Chen S. Modeling of Material-Environment Interactions for Hypersonic Thermal Protection Systems. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163164


University of Michigan

8. Chen, Guodong. Enabling Automated, Reliable and Efficient Aerodynamic Shape Optimization With Output-Based Adapted Meshes.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 Simulation-based aerodynamic shape optimization has been greatly pushed forward during the past several decades, largely due to the developments of computational fluid dynamics (CFD), geometry… (more)

Subjects/Keywords: Aerodynamic Optimization; Computational Fluid Dynamics; Error Estimation and Mesh Adaptation; Machine Learning; Aerospace Engineering; Engineering

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APA (6th Edition):

Chen, G. (2020). Enabling Automated, Reliable and Efficient Aerodynamic Shape Optimization With Output-Based Adapted Meshes. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163034

Chicago Manual of Style (16th Edition):

Chen, Guodong. “Enabling Automated, Reliable and Efficient Aerodynamic Shape Optimization With Output-Based Adapted Meshes.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/163034.

MLA Handbook (7th Edition):

Chen, Guodong. “Enabling Automated, Reliable and Efficient Aerodynamic Shape Optimization With Output-Based Adapted Meshes.” 2020. Web. 16 Apr 2021.

Vancouver:

Chen G. Enabling Automated, Reliable and Efficient Aerodynamic Shape Optimization With Output-Based Adapted Meshes. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/163034.

Council of Science Editors:

Chen G. Enabling Automated, Reliable and Efficient Aerodynamic Shape Optimization With Output-Based Adapted Meshes. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163034


University of Michigan

9. Singh, Puneet. Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 Coaxial rotor helicopters are a candidate for the next generation of rotorcraft due to their ability to achieve high speeds without compromising hover performance. Coaxial… (more)

Subjects/Keywords: helicopter; rotorcraft; aeromechanics; aeroelasticity; viscous vortex particle method; Aerospace Engineering; Engineering

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APA (6th Edition):

Singh, P. (2020). Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163227

Chicago Manual of Style (16th Edition):

Singh, Puneet. “Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/163227.

MLA Handbook (7th Edition):

Singh, Puneet. “Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method.” 2020. Web. 16 Apr 2021.

Vancouver:

Singh P. Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/163227.

Council of Science Editors:

Singh P. Aeromechanics of Coaxial Rotor Helicopters using the Viscous Vortex Particle Method. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163227


University of Michigan

10. Ye, Haixuan. Development of A Direct-Forcing Immersed-Boundary Method on Unstructured Meshes for Multi-Body Interactions in Air-Water Two-Phase Flows.

Degree: PhD, Naval Architecture & Marine Engineering, 2020, University of Michigan

 A direct-forcing immersed boundary method (IBM) is developed in the framework of a finite-volume incompressible solver for high-Reynolds-number flows. The method solves governing equations on… (more)

Subjects/Keywords: Immersed Boundary Method; Finite Volume Method; Reynolds-Averaged Navier-Stokes Equations; Wall Function; Air-water Two-phase Incompressible Flows; OpenFOAM; Naval Architecture and Marine Engineering; Engineering

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APA (6th Edition):

Ye, H. (2020). Development of A Direct-Forcing Immersed-Boundary Method on Unstructured Meshes for Multi-Body Interactions in Air-Water Two-Phase Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/162867

Chicago Manual of Style (16th Edition):

Ye, Haixuan. “Development of A Direct-Forcing Immersed-Boundary Method on Unstructured Meshes for Multi-Body Interactions in Air-Water Two-Phase Flows.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/162867.

MLA Handbook (7th Edition):

Ye, Haixuan. “Development of A Direct-Forcing Immersed-Boundary Method on Unstructured Meshes for Multi-Body Interactions in Air-Water Two-Phase Flows.” 2020. Web. 16 Apr 2021.

Vancouver:

Ye H. Development of A Direct-Forcing Immersed-Boundary Method on Unstructured Meshes for Multi-Body Interactions in Air-Water Two-Phase Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/162867.

Council of Science Editors:

Ye H. Development of A Direct-Forcing Immersed-Boundary Method on Unstructured Meshes for Multi-Body Interactions in Air-Water Two-Phase Flows. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/162867


University of Michigan

11. Jasa, John. Multidisciplinary Design Optimization of an Aircraft Considering Path-Dependent Performance.

Degree: PhD, Aerospace Engineering, 2020, University of Michigan

 Aircraft are multidisciplinary systems that are challenging to design due to interactions between the subsystems. The relevant disciplines, such as aerodynamic, thermal, and propulsion systems,… (more)

Subjects/Keywords: Multidisciplinary design optimization; Aircraft design; Numerical simulation and optimization; Aerospace Engineering; Engineering

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APA (6th Edition):

Jasa, J. (2020). Multidisciplinary Design Optimization of an Aircraft Considering Path-Dependent Performance. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/155269

Chicago Manual of Style (16th Edition):

Jasa, John. “Multidisciplinary Design Optimization of an Aircraft Considering Path-Dependent Performance.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/155269.

MLA Handbook (7th Edition):

Jasa, John. “Multidisciplinary Design Optimization of an Aircraft Considering Path-Dependent Performance.” 2020. Web. 16 Apr 2021.

Vancouver:

Jasa J. Multidisciplinary Design Optimization of an Aircraft Considering Path-Dependent Performance. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/155269.

Council of Science Editors:

Jasa J. Multidisciplinary Design Optimization of an Aircraft Considering Path-Dependent Performance. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/155269


University of Michigan

12. Zhou, Haining. Sparse Functional Expansion Based Method for Solving High-dimensional Uncertainty Quantification Problems and Its Application to the Nuclear Transient Test Reactor (TREAT).

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2019, University of Michigan

 The uncertainty quantification (UQ) in computational calculations is to quantitatively characterize the uncertainties in the quantities of interest resulted from input parameter uncertainties. UQ is… (more)

Subjects/Keywords: Uncertainty quantification of high-dimensional problems; adaptive feature selection based on lasso regularization; orthogonal polynomials and the generalized polynomial chaos method; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Zhou, H. (2019). Sparse Functional Expansion Based Method for Solving High-dimensional Uncertainty Quantification Problems and Its Application to the Nuclear Transient Test Reactor (TREAT). (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/151420

Chicago Manual of Style (16th Edition):

Zhou, Haining. “Sparse Functional Expansion Based Method for Solving High-dimensional Uncertainty Quantification Problems and Its Application to the Nuclear Transient Test Reactor (TREAT).” 2019. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/151420.

MLA Handbook (7th Edition):

Zhou, Haining. “Sparse Functional Expansion Based Method for Solving High-dimensional Uncertainty Quantification Problems and Its Application to the Nuclear Transient Test Reactor (TREAT).” 2019. Web. 16 Apr 2021.

Vancouver:

Zhou H. Sparse Functional Expansion Based Method for Solving High-dimensional Uncertainty Quantification Problems and Its Application to the Nuclear Transient Test Reactor (TREAT). [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/151420.

Council of Science Editors:

Zhou H. Sparse Functional Expansion Based Method for Solving High-dimensional Uncertainty Quantification Problems and Its Application to the Nuclear Transient Test Reactor (TREAT). [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/151420

13. Lo, Kwok Ho Marcus. A Space-Time Discontinuous Galerkin Method for Navier-Stokes with Recovery.

Degree: PhD, Aerospace Engineering, 2011, University of Michigan

 This thesis tells the story of two new members of a new generation of discontinuous Galerkin (DG) methods. Although DG, as a spatial discretization, has… (more)

Subjects/Keywords: Computational Fluid Dynamics; Recovery-based Discontinuous Galerkin Method (RDG); Space-time Advection-diffusion; High Order; Aerospace Engineering; Engineering

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APA (6th Edition):

Lo, K. H. M. (2011). A Space-Time Discontinuous Galerkin Method for Navier-Stokes with Recovery. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/86313

Chicago Manual of Style (16th Edition):

Lo, Kwok Ho Marcus. “A Space-Time Discontinuous Galerkin Method for Navier-Stokes with Recovery.” 2011. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/86313.

MLA Handbook (7th Edition):

Lo, Kwok Ho Marcus. “A Space-Time Discontinuous Galerkin Method for Navier-Stokes with Recovery.” 2011. Web. 16 Apr 2021.

Vancouver:

Lo KHM. A Space-Time Discontinuous Galerkin Method for Navier-Stokes with Recovery. [Internet] [Doctoral dissertation]. University of Michigan; 2011. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/86313.

Council of Science Editors:

Lo KHM. A Space-Time Discontinuous Galerkin Method for Navier-Stokes with Recovery. [Doctoral Dissertation]. University of Michigan; 2011. Available from: http://hdl.handle.net/2027.42/86313


University of Michigan

14. Ortiz-Soto, Elliott Alexander. Combustion Modeling of Spark Assisted Compression Ignition for Experimental Analysis and Engine System Simulations.

Degree: PhD, Mechanical Engineering, 2013, University of Michigan

 Advanced combustion strategies provide significant efficiency and emissions benefits compared to conventional spark ignited (SI) combustion, but challenges related to combustion control and load limits… (more)

Subjects/Keywords: Spark Assisted Compression Ignition, Saci; Homogeneous Charge Compression Ignition, Hcci, Spark Ignition, Si, Knock; Advanced Combustion Engines; Combustion Modeling; Engine Simulation; Efficiency, Fuel Economy, Load Extension, Load Expansion; Mechanical Engineering; Engineering

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APA (6th Edition):

Ortiz-Soto, E. A. (2013). Combustion Modeling of Spark Assisted Compression Ignition for Experimental Analysis and Engine System Simulations. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/102314

Chicago Manual of Style (16th Edition):

Ortiz-Soto, Elliott Alexander. “Combustion Modeling of Spark Assisted Compression Ignition for Experimental Analysis and Engine System Simulations.” 2013. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/102314.

MLA Handbook (7th Edition):

Ortiz-Soto, Elliott Alexander. “Combustion Modeling of Spark Assisted Compression Ignition for Experimental Analysis and Engine System Simulations.” 2013. Web. 16 Apr 2021.

Vancouver:

Ortiz-Soto EA. Combustion Modeling of Spark Assisted Compression Ignition for Experimental Analysis and Engine System Simulations. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/102314.

Council of Science Editors:

Ortiz-Soto EA. Combustion Modeling of Spark Assisted Compression Ignition for Experimental Analysis and Engine System Simulations. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/102314


University of Michigan

15. Johnson, Philip. A Recovery-Assisted Discontinuous Galerkin Method for Direct Numerical Simulation of Compressible Turbulence.

Degree: PhD, Mechanical Engineering, 2019, University of Michigan

 Computational Fluid Dynamics (CFD) serves as a valuable complement to analytical and experimental methods in the study of fluid mechanics. However, the engineering and fundamental… (more)

Subjects/Keywords: Discontinuous Galerkin; Recovery; Compressible Navier-Stokes; Mechanical Engineering; Engineering

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APA (6th Edition):

Johnson, P. (2019). A Recovery-Assisted Discontinuous Galerkin Method for Direct Numerical Simulation of Compressible Turbulence. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/151542

Chicago Manual of Style (16th Edition):

Johnson, Philip. “A Recovery-Assisted Discontinuous Galerkin Method for Direct Numerical Simulation of Compressible Turbulence.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/151542.

MLA Handbook (7th Edition):

Johnson, Philip. “A Recovery-Assisted Discontinuous Galerkin Method for Direct Numerical Simulation of Compressible Turbulence.” 2019. Web. 16 Apr 2021.

Vancouver:

Johnson P. A Recovery-Assisted Discontinuous Galerkin Method for Direct Numerical Simulation of Compressible Turbulence. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/151542.

Council of Science Editors:

Johnson P. A Recovery-Assisted Discontinuous Galerkin Method for Direct Numerical Simulation of Compressible Turbulence. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/151542


University of Michigan

16. Tandon, Suyash. Large-Scale Simulations of Complex Turbulent Flows: Modulation of Turbulent Boundary Layer Separation and Optimization of Discontinuous Galerkin Methods for Next-Generation HPC Platforms.

Degree: PhD, Mechanical Engineering, 2020, University of Michigan

 The separation of spatially evolving turbulent boundary layer flow near regions of adverse pressure gradients has been the subject of numerous studies in the context… (more)

Subjects/Keywords: Turbulent boundary layers; Large-eddy simulations; passive flow control; discontinuous Galerkin methods; extreme-scale computations; arithmetic intensity and power-performance balance; Aerospace Engineering; Computer Science; Mechanical Engineering; Mathematics; Physics; Engineering; Science

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APA (6th Edition):

Tandon, S. (2020). Large-Scale Simulations of Complex Turbulent Flows: Modulation of Turbulent Boundary Layer Separation and Optimization of Discontinuous Galerkin Methods for Next-Generation HPC Platforms. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163206

Chicago Manual of Style (16th Edition):

Tandon, Suyash. “Large-Scale Simulations of Complex Turbulent Flows: Modulation of Turbulent Boundary Layer Separation and Optimization of Discontinuous Galerkin Methods for Next-Generation HPC Platforms.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/163206.

MLA Handbook (7th Edition):

Tandon, Suyash. “Large-Scale Simulations of Complex Turbulent Flows: Modulation of Turbulent Boundary Layer Separation and Optimization of Discontinuous Galerkin Methods for Next-Generation HPC Platforms.” 2020. Web. 16 Apr 2021.

Vancouver:

Tandon S. Large-Scale Simulations of Complex Turbulent Flows: Modulation of Turbulent Boundary Layer Separation and Optimization of Discontinuous Galerkin Methods for Next-Generation HPC Platforms. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/163206.

Council of Science Editors:

Tandon S. Large-Scale Simulations of Complex Turbulent Flows: Modulation of Turbulent Boundary Layer Separation and Optimization of Discontinuous Galerkin Methods for Next-Generation HPC Platforms. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163206

17. Wiebenga, Jonathan E. High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows.

Degree: PhD, Aerospace Engineering, 2014, University of Michigan

 The development of a numerical code capable of simulating the multidimensional thermal and structural response of materials exposed to hypersonic flow is presented. The control… (more)

Subjects/Keywords: Aerothermoelasticity; Hypersonic; Aerospace Engineering; Engineering

…Stokes code developed at the University of Michigan for use on hypersonic problems. The… 

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APA (6th Edition):

Wiebenga, J. E. (2014). High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/110403

Chicago Manual of Style (16th Edition):

Wiebenga, Jonathan E. “High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows.” 2014. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/110403.

MLA Handbook (7th Edition):

Wiebenga, Jonathan E. “High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows.” 2014. Web. 16 Apr 2021.

Vancouver:

Wiebenga JE. High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/110403.

Council of Science Editors:

Wiebenga JE. High-Fidelity Material Response Modeling as Part of an Aerothermoelastic Framework for Hypersonic Flows. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/110403

18. Drzewiecki, Timothy J. Adjoint Based Uncertainty Quantification and Sensitivity Analysis for Nuclear Thermal-Fluids Codes.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2013, University of Michigan

 In this thesis the various methods of obtaining sensitivity derivatives are explored in order to highlight the significant contributors of uncertainty, and the adjoint approach… (more)

Subjects/Keywords: Adjoint; Uncertainty Quantification; Sensitivity Analysis; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Drzewiecki, T. J. (2013). Adjoint Based Uncertainty Quantification and Sensitivity Analysis for Nuclear Thermal-Fluids Codes. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/102336

Chicago Manual of Style (16th Edition):

Drzewiecki, Timothy J. “Adjoint Based Uncertainty Quantification and Sensitivity Analysis for Nuclear Thermal-Fluids Codes.” 2013. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/102336.

MLA Handbook (7th Edition):

Drzewiecki, Timothy J. “Adjoint Based Uncertainty Quantification and Sensitivity Analysis for Nuclear Thermal-Fluids Codes.” 2013. Web. 16 Apr 2021.

Vancouver:

Drzewiecki TJ. Adjoint Based Uncertainty Quantification and Sensitivity Analysis for Nuclear Thermal-Fluids Codes. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/102336.

Council of Science Editors:

Drzewiecki TJ. Adjoint Based Uncertainty Quantification and Sensitivity Analysis for Nuclear Thermal-Fluids Codes. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/102336

19. Khieu, Loc Huu. Solid-Boundary Treatment for Moment Systems.

Degree: PhD, Aerospace Engineering, 2012, University of Michigan

 Hyperbolic-relaxation systems for describing fluid flow, such as Grad's 13-moment (13M) system, are an alternative to the systems generated by the Chapman-Enskog expansion. The former… (more)

Subjects/Keywords: Computational Fluid Dynamics (CFD); Rarefied Gas Dynamics; Slip Flow Regime; Slip Boundary Condition; Extended Hydrodynamics; Moment System; Aerospace Engineering; Engineering

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APA (6th Edition):

Khieu, L. H. (2012). Solid-Boundary Treatment for Moment Systems. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/93869

Chicago Manual of Style (16th Edition):

Khieu, Loc Huu. “Solid-Boundary Treatment for Moment Systems.” 2012. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/93869.

MLA Handbook (7th Edition):

Khieu, Loc Huu. “Solid-Boundary Treatment for Moment Systems.” 2012. Web. 16 Apr 2021.

Vancouver:

Khieu LH. Solid-Boundary Treatment for Moment Systems. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/93869.

Council of Science Editors:

Khieu LH. Solid-Boundary Treatment for Moment Systems. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/93869

20. Neitzel, Kevin. Thermochemical Modeling of Nonequilibrium Oxygen Flows.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 The development of hypersonic vehicles leans heavily on computational simulation due to the high enthalpy flow conditions that are expensive and technically challenging to replicate… (more)

Subjects/Keywords: Hypersonics; Nonequilibrium; Oxygen; CFD; Aerospace Engineering; Engineering

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APA (6th Edition):

Neitzel, K. (2017). Thermochemical Modeling of Nonequilibrium Oxygen Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/137049

Chicago Manual of Style (16th Edition):

Neitzel, Kevin. “Thermochemical Modeling of Nonequilibrium Oxygen Flows.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/137049.

MLA Handbook (7th Edition):

Neitzel, Kevin. “Thermochemical Modeling of Nonequilibrium Oxygen Flows.” 2017. Web. 16 Apr 2021.

Vancouver:

Neitzel K. Thermochemical Modeling of Nonequilibrium Oxygen Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/137049.

Council of Science Editors:

Neitzel K. Thermochemical Modeling of Nonequilibrium Oxygen Flows. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/137049

21. Asher, Isaac M. Building Fully Adaptive Stochastic Models for Multiphase Blowdown Simulations.

Degree: PhD, Aerospace Engineering, 2015, University of Michigan

 A new method for uncertainty quantification (UQ) that combines adaptivity in the physical (deterministic) space and the stochastic space is presented. The sampling-based method adaptively… (more)

Subjects/Keywords: uncertainty quantification; stochastic modeling; adjoint; multiphase flow; adaptation; error estimation; Aerospace Engineering; Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Asher, I. M. (2015). Building Fully Adaptive Stochastic Models for Multiphase Blowdown Simulations. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/111612

Chicago Manual of Style (16th Edition):

Asher, Isaac M. “Building Fully Adaptive Stochastic Models for Multiphase Blowdown Simulations.” 2015. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/111612.

MLA Handbook (7th Edition):

Asher, Isaac M. “Building Fully Adaptive Stochastic Models for Multiphase Blowdown Simulations.” 2015. Web. 16 Apr 2021.

Vancouver:

Asher IM. Building Fully Adaptive Stochastic Models for Multiphase Blowdown Simulations. [Internet] [Doctoral dissertation]. University of Michigan; 2015. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/111612.

Council of Science Editors:

Asher IM. Building Fully Adaptive Stochastic Models for Multiphase Blowdown Simulations. [Doctoral Dissertation]. University of Michigan; 2015. Available from: http://hdl.handle.net/2027.42/111612

22. Maeng, Jungyeoul. On the Advective Component of Active Flux Schemes for Nonlinear Hyperbolic Conservation Laws.

Degree: PhD, Aerospace Engineering, 2017, University of Michigan

 A new class of numerical methods called Active Flux (AF) is investigated for nonlinear hyperbolic conservation laws. The AF method is designed specifically to address… (more)

Subjects/Keywords: Active Flux Schemes; High-order numerical method; Advection schemes; Aerospace Engineering; Engineering

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APA (6th Edition):

Maeng, J. (2017). On the Advective Component of Active Flux Schemes for Nonlinear Hyperbolic Conservation Laws. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/138695

Chicago Manual of Style (16th Edition):

Maeng, Jungyeoul. “On the Advective Component of Active Flux Schemes for Nonlinear Hyperbolic Conservation Laws.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/138695.

MLA Handbook (7th Edition):

Maeng, Jungyeoul. “On the Advective Component of Active Flux Schemes for Nonlinear Hyperbolic Conservation Laws.” 2017. Web. 16 Apr 2021.

Vancouver:

Maeng J. On the Advective Component of Active Flux Schemes for Nonlinear Hyperbolic Conservation Laws. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/138695.

Council of Science Editors:

Maeng J. On the Advective Component of Active Flux Schemes for Nonlinear Hyperbolic Conservation Laws. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/138695

23. Henry de Frahan, Marc T. Numerical Simulations of Shock and Rarefaction Waves Interacting With Interfaces in Compressible Multiphase Flows.

Degree: PhD, Mechanical Engineering, 2016, University of Michigan

 Developing a highly accurate numerical framework to study multiphase mixing in high speed flows containing shear layers, shocks, and strong accelerations is critical to many… (more)

Subjects/Keywords: computational fluid dynamics of multiphase flows; hydrodynamic instabilities: Richtmyer-Meshkov, Rayleigh-Taylor; discontinuous Galerkin methods; high performance computing with graphics processing units; strength models for materials in high strain rate and pressure regimes; mixing in multiphase and multicomponent flows; Mechanical Engineering; Engineering

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APA (6th Edition):

Henry de Frahan, M. T. (2016). Numerical Simulations of Shock and Rarefaction Waves Interacting With Interfaces in Compressible Multiphase Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/133458

Chicago Manual of Style (16th Edition):

Henry de Frahan, Marc T. “Numerical Simulations of Shock and Rarefaction Waves Interacting With Interfaces in Compressible Multiphase Flows.” 2016. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/133458.

MLA Handbook (7th Edition):

Henry de Frahan, Marc T. “Numerical Simulations of Shock and Rarefaction Waves Interacting With Interfaces in Compressible Multiphase Flows.” 2016. Web. 16 Apr 2021.

Vancouver:

Henry de Frahan MT. Numerical Simulations of Shock and Rarefaction Waves Interacting With Interfaces in Compressible Multiphase Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2016. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/133458.

Council of Science Editors:

Henry de Frahan MT. Numerical Simulations of Shock and Rarefaction Waves Interacting With Interfaces in Compressible Multiphase Flows. [Doctoral Dissertation]. University of Michigan; 2016. Available from: http://hdl.handle.net/2027.42/133458

24. Ceze, Marco Antonio de Barros. A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Quantitatively accurate results from realistic Computational Fluid Dynamics (CFD) simulations are often accompanied by high computational expense. Higher-order methods are good candidates for providing accurate… (more)

Subjects/Keywords: Computational Fluid Dynamics CFD; Mesh Adaptation; Adjoint Method; Output Error Estimation; Drag Prediction Workshop; Discontinuous Galerkin; Aerospace Engineering; Engineering

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APA (6th Edition):

Ceze, M. A. d. B. (2013). A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/97795

Chicago Manual of Style (16th Edition):

Ceze, Marco Antonio de Barros. “A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows.” 2013. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/97795.

MLA Handbook (7th Edition):

Ceze, Marco Antonio de Barros. “A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows.” 2013. Web. 16 Apr 2021.

Vancouver:

Ceze MAdB. A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/97795.

Council of Science Editors:

Ceze MAdB. A Robust hp-Adaptation Method for Discontinuous Galerkin Discretizations Applied to Aerodynamic Flows. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/97795

25. Li, David S. Bubble Dynamics and Acoustic Droplet Vaporization in Gas Embolotherapy.

Degree: PhD, Biomedical Engineering, 2014, University of Michigan

 Gas embolotherapy is a twist on traditional catheter based embolotherapy approaches. Localized gas bubbles generated are used in place of solid emboli normally used to… (more)

Subjects/Keywords: Gas Embolotherapy; Acoustic Droplet Vaporization; Therapeutic Ultrasound; Fluid Mechanics; Bubble Dynamics; Biomedical Engineering; Engineering

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APA (6th Edition):

Li, D. S. (2014). Bubble Dynamics and Acoustic Droplet Vaporization in Gas Embolotherapy. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/107251

Chicago Manual of Style (16th Edition):

Li, David S. “Bubble Dynamics and Acoustic Droplet Vaporization in Gas Embolotherapy.” 2014. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/107251.

MLA Handbook (7th Edition):

Li, David S. “Bubble Dynamics and Acoustic Droplet Vaporization in Gas Embolotherapy.” 2014. Web. 16 Apr 2021.

Vancouver:

Li DS. Bubble Dynamics and Acoustic Droplet Vaporization in Gas Embolotherapy. [Internet] [Doctoral dissertation]. University of Michigan; 2014. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/107251.

Council of Science Editors:

Li DS. Bubble Dynamics and Acoustic Droplet Vaporization in Gas Embolotherapy. [Doctoral Dissertation]. University of Michigan; 2014. Available from: http://hdl.handle.net/2027.42/107251

26. Bassett, Brody. Meshless Methods for the Neutron Transport Equation.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2018, University of Michigan

 Mesh-based methods for the numerical solution of partial differential equations (PDEs) require the division of the problem domain into non-overlapping, contiguous subdomains that conform to… (more)

Subjects/Keywords: meshless local Petrov-Galerkin (MLPG); discrete ordinates neutron transport; streamline upwind Petrov-Galerkin (SUPG); k-eigenvalue; moving least squares (MLS); radial basis function (RBF); Nuclear Engineering and Radiological Sciences; Engineering

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APA (6th Edition):

Bassett, B. (2018). Meshless Methods for the Neutron Transport Equation. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/145796

Chicago Manual of Style (16th Edition):

Bassett, Brody. “Meshless Methods for the Neutron Transport Equation.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/145796.

MLA Handbook (7th Edition):

Bassett, Brody. “Meshless Methods for the Neutron Transport Equation.” 2018. Web. 16 Apr 2021.

Vancouver:

Bassett B. Meshless Methods for the Neutron Transport Equation. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/145796.

Council of Science Editors:

Bassett B. Meshless Methods for the Neutron Transport Equation. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/145796

27. Singh, Anand Pratap. A Framework to improve Turbulence Models using Full-field Inversion and Machine Learning.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 Accurate prediction of turbulent flows remains a barrier to the widespread use of computational fluid dynamics in analysis and design. Since practical wall-bounded turbulent flows… (more)

Subjects/Keywords: turbulence modeling; machine learning; Aerospace Engineering; Engineering

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APA (6th Edition):

Singh, A. P. (2018). A Framework to improve Turbulence Models using Full-field Inversion and Machine Learning. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/144034

Chicago Manual of Style (16th Edition):

Singh, Anand Pratap. “A Framework to improve Turbulence Models using Full-field Inversion and Machine Learning.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/144034.

MLA Handbook (7th Edition):

Singh, Anand Pratap. “A Framework to improve Turbulence Models using Full-field Inversion and Machine Learning.” 2018. Web. 16 Apr 2021.

Vancouver:

Singh AP. A Framework to improve Turbulence Models using Full-field Inversion and Machine Learning. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/144034.

Council of Science Editors:

Singh AP. A Framework to improve Turbulence Models using Full-field Inversion and Machine Learning. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/144034

28. Irvine, Adam Glenn. High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Scramjets are a type of air breathing propulsion system that have the potential to efficiently provide thrust for atmospheric vehicles at high speeds. Defining the… (more)

Subjects/Keywords: High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System; Aerospace Engineering; Engineering

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APA (6th Edition):

Irvine, A. G. (2013). High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/97978

Chicago Manual of Style (16th Edition):

Irvine, Adam Glenn. “High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System.” 2013. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/97978.

MLA Handbook (7th Edition):

Irvine, Adam Glenn. “High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System.” 2013. Web. 16 Apr 2021.

Vancouver:

Irvine AG. High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/97978.

Council of Science Editors:

Irvine AG. High Fidelity Radiative Thermal Transport Simulations of a Scramjet Propulsion System. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/97978

29. Alkandry, Hicham. Aerodynamic Interactions of Propulsive Deceleration and Reaction Control System Jets on Mars-Entry Aeroshells.

Degree: PhD, Aerospace Engineering and Scientific Computing, 2012, University of Michigan

 Future missions to Mars, including sample-return and human-exploration missions, may require alternative entry, descent, and landing technologies in order to perform pinpoint landing of heavy… (more)

Subjects/Keywords: Propulsive Deceleration; Reaction Control System; Computational Fluid Dynamics; Hypersonic Flow; Aerospace Engineering; Engineering

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APA (6th Edition):

Alkandry, H. (2012). Aerodynamic Interactions of Propulsive Deceleration and Reaction Control System Jets on Mars-Entry Aeroshells. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/91580

Chicago Manual of Style (16th Edition):

Alkandry, Hicham. “Aerodynamic Interactions of Propulsive Deceleration and Reaction Control System Jets on Mars-Entry Aeroshells.” 2012. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/91580.

MLA Handbook (7th Edition):

Alkandry, Hicham. “Aerodynamic Interactions of Propulsive Deceleration and Reaction Control System Jets on Mars-Entry Aeroshells.” 2012. Web. 16 Apr 2021.

Vancouver:

Alkandry H. Aerodynamic Interactions of Propulsive Deceleration and Reaction Control System Jets on Mars-Entry Aeroshells. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/91580.

Council of Science Editors:

Alkandry H. Aerodynamic Interactions of Propulsive Deceleration and Reaction Control System Jets on Mars-Entry Aeroshells. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/91580

30. Lamorte, Nicolas Etienne. Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis.

Degree: PhD, Aerospace Engineering, 2013, University of Michigan

 Hypersonic vehicles face a challenging flight environment. The aerothermoelastic analysis of its components requires numerous simplifying approximations. Identifying and quantifying the effect of uncertainties pushes… (more)

Subjects/Keywords: Hypersonic Aerothermoelasticity; Uncertainty Propagation; Aerospace Engineering; Engineering

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APA (6th Edition):

Lamorte, N. E. (2013). Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/99806

Chicago Manual of Style (16th Edition):

Lamorte, Nicolas Etienne. “Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis.” 2013. Doctoral Dissertation, University of Michigan. Accessed April 16, 2021. http://hdl.handle.net/2027.42/99806.

MLA Handbook (7th Edition):

Lamorte, Nicolas Etienne. “Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis.” 2013. Web. 16 Apr 2021.

Vancouver:

Lamorte NE. Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis. [Internet] [Doctoral dissertation]. University of Michigan; 2013. [cited 2021 Apr 16]. Available from: http://hdl.handle.net/2027.42/99806.

Council of Science Editors:

Lamorte NE. Uncertainty Propagation in Hypersonic Vehicle Aerothermoelastic Analysis. [Doctoral Dissertation]. University of Michigan; 2013. Available from: http://hdl.handle.net/2027.42/99806

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