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You searched for +publisher:"University of Michigan" +contributor:("Martins, Joaquim R R A"). Showing records 1 – 18 of 18 total matches.

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University of Michigan

1. Mbagwu, Chukwuka. Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles.

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

 High speed, air-breathing hypersonic vehicles encounter a varied range of engine and operating conditions traveling along cruise/ascent missions at high altitudes and dynamic pressures. Variations… (more)

Subjects/Keywords: hypersonic vehicles; scramjet; optimization; combustion; Aerospace Engineering; Engineering

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APA (6th Edition):

Mbagwu, C. (2017). Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/140954

Chicago Manual of Style (16th Edition):

Mbagwu, Chukwuka. “Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/140954.

MLA Handbook (7th Edition):

Mbagwu, Chukwuka. “Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles.” 2017. Web. 22 Apr 2021.

Vancouver:

Mbagwu C. Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/140954.

Council of Science Editors:

Mbagwu C. Combustion Efficiency, Flameout Operability Limits and General Design Optimization for Integrated Ramjet-Scramjet Hypersonic Vehicles. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/140954


University of Michigan

2. Jonsson, Eirikur. High-fidelity Aerostructural Optimization of Flexible Wings with Flutter Constraints.

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

 High-fidelity optimization of aircraft has the potential to produce more efficient designs and to further reduce the risk of late design changes. For the optimization… (more)

Subjects/Keywords: Aeroelastic optimization; Flutter constraint; Aerospace Engineering; Engineering

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APA (6th Edition):

Jonsson, E. (2020). High-fidelity Aerostructural Optimization of Flexible Wings with Flutter Constraints. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/162902

Chicago Manual of Style (16th Edition):

Jonsson, Eirikur. “High-fidelity Aerostructural Optimization of Flexible Wings with Flutter Constraints.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/162902.

MLA Handbook (7th Edition):

Jonsson, Eirikur. “High-fidelity Aerostructural Optimization of Flexible Wings with Flutter Constraints.” 2020. Web. 22 Apr 2021.

Vancouver:

Jonsson E. High-fidelity Aerostructural Optimization of Flexible Wings with Flutter Constraints. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/162902.

Council of Science Editors:

Jonsson E. High-fidelity Aerostructural Optimization of Flexible Wings with Flutter Constraints. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/162902


University of Michigan

3. Bons, Nicolas. High-Fidelity Wing Design Exploration with Gradient-Based Optimization.

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

 Numerical optimization has been applied to wing design problems for over 40 years. Over the decades, the scope and detail of optimization problems have advanced… (more)

Subjects/Keywords: multidisciplinary design optimization; aerostructural optimization; wing design optimization; multimodality in wing design; practical wing design optimization; Aerospace Engineering; Engineering

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APA (6th Edition):

Bons, N. (2020). High-Fidelity Wing Design Exploration with Gradient-Based Optimization. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163242

Chicago Manual of Style (16th Edition):

Bons, Nicolas. “High-Fidelity Wing Design Exploration with Gradient-Based Optimization.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/163242.

MLA Handbook (7th Edition):

Bons, Nicolas. “High-Fidelity Wing Design Exploration with Gradient-Based Optimization.” 2020. Web. 22 Apr 2021.

Vancouver:

Bons N. High-Fidelity Wing Design Exploration with Gradient-Based Optimization. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/163242.

Council of Science Editors:

Bons N. High-Fidelity Wing Design Exploration with Gradient-Based Optimization. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163242


University of Michigan

4. Lupp, Christopher. Inclusion of Geometrically Nonlinear Aeroelastic Effects into Gradient-Based Aircraft Optimization.

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

 While aircraft have largely featured flexible wings for decades, more recently, aircraft structures have rapidly become more flexible. The pursuit of longer ranges and higher… (more)

Subjects/Keywords: aeroelasticity; Aerospace Engineering; Engineering

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APA (6th Edition):

Lupp, C. (2020). Inclusion of Geometrically Nonlinear Aeroelastic Effects into Gradient-Based Aircraft Optimization. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/163259

Chicago Manual of Style (16th Edition):

Lupp, Christopher. “Inclusion of Geometrically Nonlinear Aeroelastic Effects into Gradient-Based Aircraft Optimization.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/163259.

MLA Handbook (7th Edition):

Lupp, Christopher. “Inclusion of Geometrically Nonlinear Aeroelastic Effects into Gradient-Based Aircraft Optimization.” 2020. Web. 22 Apr 2021.

Vancouver:

Lupp C. Inclusion of Geometrically Nonlinear Aeroelastic Effects into Gradient-Based Aircraft Optimization. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/163259.

Council of Science Editors:

Lupp C. Inclusion of Geometrically Nonlinear Aeroelastic Effects into Gradient-Based Aircraft Optimization. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/163259


University of Michigan

5. 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 22, 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. 22 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 22]. 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

6. Chauhan, Shamsheer Singh. Optimization Studies for Aircraft Considering Propeller-Wing Interaction.

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

 Environmental concerns and advances in battery technology are currently fueling a widespread growth of interest in electric aircraft. Additionally, the fundamentally different nature of electric… (more)

Subjects/Keywords: Propeller-wing interaction; eVTOL; Trajectory optimization; Aerodynamic shape optimization; MDO; Aerospace Engineering; Engineering

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APA (6th Edition):

Chauhan, S. S. (2020). Optimization Studies for Aircraft Considering Propeller-Wing Interaction. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/166109

Chicago Manual of Style (16th Edition):

Chauhan, Shamsheer Singh. “Optimization Studies for Aircraft Considering Propeller-Wing Interaction.” 2020. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/166109.

MLA Handbook (7th Edition):

Chauhan, Shamsheer Singh. “Optimization Studies for Aircraft Considering Propeller-Wing Interaction.” 2020. Web. 22 Apr 2021.

Vancouver:

Chauhan SS. Optimization Studies for Aircraft Considering Propeller-Wing Interaction. [Internet] [Doctoral dissertation]. University of Michigan; 2020. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/166109.

Council of Science Editors:

Chauhan SS. Optimization Studies for Aircraft Considering Propeller-Wing Interaction. [Doctoral Dissertation]. University of Michigan; 2020. Available from: http://hdl.handle.net/2027.42/166109


University of Michigan

7. 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 22, 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. 22 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 22]. 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

8. Zhou, Yuqing. Gradient-Based Multi-Component Topology Optimization for Manufacturability.

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

 Topology optimization is a method where the distribution of materials within a design domain is optimized for a structural performance. Since the geometry is represented… (more)

Subjects/Keywords: topology optimization; multi-component structure; gradient-based optimization; design for manufacturability; composite structure; additive manufacturing; Mechanical Engineering; Engineering

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APA (6th Edition):

Zhou, Y. (2018). Gradient-Based Multi-Component Topology Optimization for Manufacturability. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/145989

Chicago Manual of Style (16th Edition):

Zhou, Yuqing. “Gradient-Based Multi-Component Topology Optimization for Manufacturability.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/145989.

MLA Handbook (7th Edition):

Zhou, Yuqing. “Gradient-Based Multi-Component Topology Optimization for Manufacturability.” 2018. Web. 22 Apr 2021.

Vancouver:

Zhou Y. Gradient-Based Multi-Component Topology Optimization for Manufacturability. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/145989.

Council of Science Editors:

Zhou Y. Gradient-Based Multi-Component Topology Optimization for Manufacturability. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/145989

9. Brooks, Timothy. Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites.

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

 In the last 30 years since their introduction into aerospace applications, composites have become increasingly used, making up as much as 50% of modern aircraft… (more)

Subjects/Keywords: Multi-disciplinary design optimization; Tow-steered composites; Aeroelastic wing design; Aerospace Engineering; Engineering

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APA (6th Edition):

Brooks, T. (2018). Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/145830

Chicago Manual of Style (16th Edition):

Brooks, Timothy. “Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/145830.

MLA Handbook (7th Edition):

Brooks, Timothy. “Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites.” 2018. Web. 22 Apr 2021.

Vancouver:

Brooks T. Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/145830.

Council of Science Editors:

Brooks T. Design Optimization of Flexible Aircraft Wings Using Tow-steered Composites. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/145830

10. Marley, Christopher. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.

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

 Due to the large aerodynamic heating at high Mach numbers, Thermal Protection System (TPS) design considerations are critical for hypersonic vehicles, and engineers seek to… (more)

Subjects/Keywords: Hypersonic Cruise Vehicle; Active Thermal Protection System (TPS); Passive Thermal Protection System (TPS); Scramjet; Aerospace Engineering; Engineering

…scramjet-powered vehicle model developed at the University of Michigan. For a trimmed hypersonic… …AFRL by Bolender and Doman [5]. A third model was developed at the University of… …Aeroelasticity and Structures Research Lab (A2 SRL) directed by Cesnik at the University of… …Michigan that is called the MASIV (MichiganAFRL Scramjet In Vehicle) model. MASIV has… …Michigan. It was described by Falkiewicz and Cesnik in [16] and by Klock and Cesnik in… 

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APA (6th Edition):

Marley, C. (2018). Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/144038

Chicago Manual of Style (16th Edition):

Marley, Christopher. “Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/144038.

MLA Handbook (7th Edition):

Marley, Christopher. “Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.” 2018. Web. 22 Apr 2021.

Vancouver:

Marley C. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/144038.

Council of Science Editors:

Marley C. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/144038

11. Shinde, Siddhesh Dilip. A Computational Study of Flow Over a Wall-Mounted Cube in a Turbulent Boundary Layer Using Large Eddy Simulations.

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

 Flow over a wall-mounted cube in a turbulent boundary layer (TBL) is a canonical problem with applications in many engineering systems. Atmospheric flow over buildings… (more)

Subjects/Keywords: Computational Fluid Dynamics; Large Eddy Simulations; Flow over cubes; Mechanical Engineering; Engineering

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APA (6th Edition):

Shinde, S. D. (2018). A Computational Study of Flow Over a Wall-Mounted Cube in a Turbulent Boundary Layer Using Large Eddy Simulations. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/145901

Chicago Manual of Style (16th Edition):

Shinde, Siddhesh Dilip. “A Computational Study of Flow Over a Wall-Mounted Cube in a Turbulent Boundary Layer Using Large Eddy Simulations.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/145901.

MLA Handbook (7th Edition):

Shinde, Siddhesh Dilip. “A Computational Study of Flow Over a Wall-Mounted Cube in a Turbulent Boundary Layer Using Large Eddy Simulations.” 2018. Web. 22 Apr 2021.

Vancouver:

Shinde SD. A Computational Study of Flow Over a Wall-Mounted Cube in a Turbulent Boundary Layer Using Large Eddy Simulations. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/145901.

Council of Science Editors:

Shinde SD. A Computational Study of Flow Over a Wall-Mounted Cube in a Turbulent Boundary Layer Using Large Eddy Simulations. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/145901

12. Secco, Ney. Component-Based Aerodynamic Shape Optimization using Overset Meshes.

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

 Advances in computational power allow the increase in the fidelity level of analysis tools used in conceptual aircraft design and optimization. These tools not only… (more)

Subjects/Keywords: Aerodynamic Shape Optimization; Computational Fluid Dynamics; Mesh Generation and Manipulation; Aerospace Engineering; Engineering

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APA (6th Edition):

Secco, N. (2018). Component-Based Aerodynamic Shape Optimization using Overset Meshes. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/146042

Chicago Manual of Style (16th Edition):

Secco, Ney. “Component-Based Aerodynamic Shape Optimization using Overset Meshes.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/146042.

MLA Handbook (7th Edition):

Secco, Ney. “Component-Based Aerodynamic Shape Optimization using Overset Meshes.” 2018. Web. 22 Apr 2021.

Vancouver:

Secco N. Component-Based Aerodynamic Shape Optimization using Overset Meshes. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/146042.

Council of Science Editors:

Secco N. Component-Based Aerodynamic Shape Optimization using Overset Meshes. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/146042

13. Kosztowny, Cyrus. Unitized Stiffened Composite Textile Panels: Manufacturing, Characterization, Experiments, and Analysis.

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

 Use of carbon fiber textiles in complex manufacturing methods creates new implementations of structural components by increasing performance, lowering manufacturing costs, and making composites overall… (more)

Subjects/Keywords: composite structures; carbon fiber reinforced polymer; multiscaling; unitized structures; textiles; postbuckling; Aerospace Engineering; Engineering

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APA (6th Edition):

Kosztowny, C. (2017). Unitized Stiffened Composite Textile Panels: Manufacturing, Characterization, Experiments, and Analysis. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/136947

Chicago Manual of Style (16th Edition):

Kosztowny, Cyrus. “Unitized Stiffened Composite Textile Panels: Manufacturing, Characterization, Experiments, and Analysis.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/136947.

MLA Handbook (7th Edition):

Kosztowny, Cyrus. “Unitized Stiffened Composite Textile Panels: Manufacturing, Characterization, Experiments, and Analysis.” 2017. Web. 22 Apr 2021.

Vancouver:

Kosztowny C. Unitized Stiffened Composite Textile Panels: Manufacturing, Characterization, Experiments, and Analysis. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/136947.

Council of Science Editors:

Kosztowny C. Unitized Stiffened Composite Textile Panels: Manufacturing, Characterization, Experiments, and Analysis. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/136947

14. Garg, Nitin. High-Fidelity Hydrostructural Design Optimization of Lifting Surfaces.

Degree: PhD, Naval Architecture & Marine Engineering, 2017, University of Michigan

 Recent advances in high-performance computing and the efficiency of numerical solvers have made it possible to use sequential high-fidelity hydrodynamic and structural simulations to carry… (more)

Subjects/Keywords: Multipoint hydrostructural design optimization; Gradient-based optimization; Bend-twist coupling of composite hydrofoils; Cavitation constraint; Experimental investigation of optimized hydrofoil; Aerospace Engineering; Mechanical Engineering; Naval Architecture and Marine Engineering; Engineering

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APA (6th Edition):

Garg, N. (2017). High-Fidelity Hydrostructural Design Optimization of Lifting Surfaces. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/138569

Chicago Manual of Style (16th Edition):

Garg, Nitin. “High-Fidelity Hydrostructural Design Optimization of Lifting Surfaces.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/138569.

MLA Handbook (7th Edition):

Garg, Nitin. “High-Fidelity Hydrostructural Design Optimization of Lifting Surfaces.” 2017. Web. 22 Apr 2021.

Vancouver:

Garg N. High-Fidelity Hydrostructural Design Optimization of Lifting Surfaces. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/138569.

Council of Science Editors:

Garg N. High-Fidelity Hydrostructural Design Optimization of Lifting Surfaces. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/138569

15. Sanjaya, Devina. Towards Automated, Metric-Conforming, Mesh Optimization For High-Order, Finite-Element Methods.

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

 High-resolution flow simulations are becoming important for increasingly many engineering applications. While high-resolution simulations give us the accuracy needed for engineering purposes, they generally demand… (more)

Subjects/Keywords: computational fluid dyanmics; metric-based mesh adaptation; high-order mesh; high-order metric field; high-order, metric-conforming mesh; warped-element refinement method; Aerospace Engineering; Engineering

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APA (6th Edition):

Sanjaya, D. (2019). Towards Automated, Metric-Conforming, Mesh Optimization For High-Order, Finite-Element Methods. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/151619

Chicago Manual of Style (16th Edition):

Sanjaya, Devina. “Towards Automated, Metric-Conforming, Mesh Optimization For High-Order, Finite-Element Methods.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/151619.

MLA Handbook (7th Edition):

Sanjaya, Devina. “Towards Automated, Metric-Conforming, Mesh Optimization For High-Order, Finite-Element Methods.” 2019. Web. 22 Apr 2021.

Vancouver:

Sanjaya D. Towards Automated, Metric-Conforming, Mesh Optimization For High-Order, Finite-Element Methods. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/151619.

Council of Science Editors:

Sanjaya D. Towards Automated, Metric-Conforming, Mesh Optimization For High-Order, Finite-Element Methods. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/151619

16. Burdette Jr, David. High-Fidelity Aerostructural Design Optimization of Transport Aircraft with Continuous Morphing Trailing Edge Technology.

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

 Adaptive morphing trailing edge technology offers the potential to decrease the fuel burn of transonic commercial transport aircraft by allowing wings to dynamically adjust to… (more)

Subjects/Keywords: multidisciplinary design optimization; aerostructural optimization; morphing trailing edge; Aerospace Engineering; Engineering

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APA (6th Edition):

Burdette Jr, D. (2017). High-Fidelity Aerostructural Design Optimization of Transport Aircraft with Continuous Morphing Trailing Edge Technology. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/140858

Chicago Manual of Style (16th Edition):

Burdette Jr, David. “High-Fidelity Aerostructural Design Optimization of Transport Aircraft with Continuous Morphing Trailing Edge Technology.” 2017. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/140858.

MLA Handbook (7th Edition):

Burdette Jr, David. “High-Fidelity Aerostructural Design Optimization of Transport Aircraft with Continuous Morphing Trailing Edge Technology.” 2017. Web. 22 Apr 2021.

Vancouver:

Burdette Jr D. High-Fidelity Aerostructural Design Optimization of Transport Aircraft with Continuous Morphing Trailing Edge Technology. [Internet] [Doctoral dissertation]. University of Michigan; 2017. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/140858.

Council of Science Editors:

Burdette Jr D. High-Fidelity Aerostructural Design Optimization of Transport Aircraft with Continuous Morphing Trailing Edge Technology. [Doctoral Dissertation]. University of Michigan; 2017. Available from: http://hdl.handle.net/2027.42/140858

17. Huang, Daning. Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels.

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

 In the past decade, there has been a strong interest in reusable air-breathing hypersonic vehicles for in both civil and military applications. However, there are… (more)

Subjects/Keywords: Hypersonic aerothermoelasticity; Numerical scaling laws; Fluid-structural-thermal interaction; Reduced order modeling; Stability analysis; Multi-objective Bayesian optimization; Aerospace Engineering; Engineering

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

APA (6th Edition):

Huang, D. (2019). Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/151461

Chicago Manual of Style (16th Edition):

Huang, Daning. “Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels.” 2019. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/151461.

MLA Handbook (7th Edition):

Huang, Daning. “Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels.” 2019. Web. 22 Apr 2021.

Vancouver:

Huang D. Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels. [Internet] [Doctoral dissertation]. University of Michigan; 2019. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/151461.

Council of Science Editors:

Huang D. Development of a Hypersonic Aerothermoelastic Framework and Its Application to Flutter and Aerothermoelastic Scaling of Skin Panels. [Doctoral Dissertation]. University of Michigan; 2019. Available from: http://hdl.handle.net/2027.42/151461

18. Gray, Justin. Design Optimization of a Boundary Layer Ingestion Propulsor Using a Coupled Aeropropulsive Model.

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

 Within a few years of the first jet engine powered aircraft entering military service, engineers proposed a tightly coupled aeropropulsive concept called boundary layer ingestion… (more)

Subjects/Keywords: optimization; multidisciplinary design optimization; aeropropulsive; Aerospace Engineering; Engineering

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

APA (6th Edition):

Gray, J. (2018). Design Optimization of a Boundary Layer Ingestion Propulsor Using a Coupled Aeropropulsive Model. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/147625

Chicago Manual of Style (16th Edition):

Gray, Justin. “Design Optimization of a Boundary Layer Ingestion Propulsor Using a Coupled Aeropropulsive Model.” 2018. Doctoral Dissertation, University of Michigan. Accessed April 22, 2021. http://hdl.handle.net/2027.42/147625.

MLA Handbook (7th Edition):

Gray, Justin. “Design Optimization of a Boundary Layer Ingestion Propulsor Using a Coupled Aeropropulsive Model.” 2018. Web. 22 Apr 2021.

Vancouver:

Gray J. Design Optimization of a Boundary Layer Ingestion Propulsor Using a Coupled Aeropropulsive Model. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2021 Apr 22]. Available from: http://hdl.handle.net/2027.42/147625.

Council of Science Editors:

Gray J. Design Optimization of a Boundary Layer Ingestion Propulsor Using a Coupled Aeropropulsive Model. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/147625

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