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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

URL: http://hdl.handle.net/2027.42/113577

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/89612

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/133418

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/153455

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/155105

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/149954

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/163164

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/163034

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/163227

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/162867

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/155269

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/151420

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/86313

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/102314

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/151542

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/163206

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/110403

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/102336

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/93869

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/137049

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/111612

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/138695

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/133458

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/97795

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/107251

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

APA (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/145796

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/144034

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/97978

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/91580

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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

URL: http://hdl.handle.net/2027.42/99806

► 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 (6^{th} 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 (16^{th} 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 (7^{th} 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