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1. Diaconu, Dumitru. Mechanical Aspects of Design, Analysis and Testing of the Nanosatellite for Earth Monitoring and Observation – Aerosol Monitor (NEMO-AM).

Degree: 2014, University of Toronto

URL: http://hdl.handle.net/1807/44014

►

A next generation nanosatellite bus is under development at the *University* of Toronto’s Space Flight Laboratory (SFL), and is being used for the first time…
(more)

Subjects/Keywords: satellite; finite element modeling; satellite structure; finite element analysis; FEM; FEA; Earth observation; aerosol; nanosatellite; mechanical design; ground support equipment; microsatellite; 0538

…the *University* *of* *Toronto* Institute for Aerospace Studies
is a research facility that…

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APA (6^{th} Edition):

Diaconu, D. (2014). Mechanical Aspects of Design, Analysis and Testing of the Nanosatellite for Earth Monitoring and Observation – Aerosol Monitor (NEMO-AM). (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/44014

Chicago Manual of Style (16^{th} Edition):

Diaconu, Dumitru. “Mechanical Aspects of Design, Analysis and Testing of the Nanosatellite for Earth Monitoring and Observation – Aerosol Monitor (NEMO-AM).” 2014. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/44014.

MLA Handbook (7^{th} Edition):

Diaconu, Dumitru. “Mechanical Aspects of Design, Analysis and Testing of the Nanosatellite for Earth Monitoring and Observation – Aerosol Monitor (NEMO-AM).” 2014. Web. 21 Mar 2019.

Vancouver:

Diaconu D. Mechanical Aspects of Design, Analysis and Testing of the Nanosatellite for Earth Monitoring and Observation – Aerosol Monitor (NEMO-AM). [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/44014.

Council of Science Editors:

Diaconu D. Mechanical Aspects of Design, Analysis and Testing of the Nanosatellite for Earth Monitoring and Observation – Aerosol Monitor (NEMO-AM). [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/44014

2. Duivenvoorden, Rikky. Quadrotor Control in the Presence of Unknown Mass Properties.

Degree: 2016, University of Toronto

URL: http://hdl.handle.net/1807/74674

►

Quadrotor UAVs are popular due to their mechanical simplicity, as well as their capability to hover and vertically take-off and land. As applications diversify, quadrotors… (more)

Subjects/Keywords: Control Systems; L1 Adaptive Control; Quadrotor Dynamics; 0538

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APA (6^{th} Edition):

Duivenvoorden, R. (2016). Quadrotor Control in the Presence of Unknown Mass Properties. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/74674

Chicago Manual of Style (16^{th} Edition):

Duivenvoorden, Rikky. “Quadrotor Control in the Presence of Unknown Mass Properties.” 2016. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/74674.

MLA Handbook (7^{th} Edition):

Duivenvoorden, Rikky. “Quadrotor Control in the Presence of Unknown Mass Properties.” 2016. Web. 21 Mar 2019.

Vancouver:

Duivenvoorden R. Quadrotor Control in the Presence of Unknown Mass Properties. [Internet] [Masters thesis]. University of Toronto; 2016. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/74674.

Council of Science Editors:

Duivenvoorden R. Quadrotor Control in the Presence of Unknown Mass Properties. [Masters Thesis]. University of Toronto; 2016. Available from: http://hdl.handle.net/1807/74674

3. McCormick, Neil. The Development and Evaluation of a Fully-coupled Monolithic Approach to Aero-structural Analysis and Optimization.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/43217

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A monolithic approach to aero-structural analysis and optimization has been developed and implemented. In contrast to a partitioned approach which uses individual fluid and structural… (more)

Subjects/Keywords: CFD; optimiztion; aerodynamics; structural; monolithic; fluid-structure interaction; aero-structural; analysis; 0538

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APA (6^{th} Edition):

McCormick, N. (2013). The Development and Evaluation of a Fully-coupled Monolithic Approach to Aero-structural Analysis and Optimization. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43217

Chicago Manual of Style (16^{th} Edition):

McCormick, Neil. “The Development and Evaluation of a Fully-coupled Monolithic Approach to Aero-structural Analysis and Optimization.” 2013. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/43217.

MLA Handbook (7^{th} Edition):

McCormick, Neil. “The Development and Evaluation of a Fully-coupled Monolithic Approach to Aero-structural Analysis and Optimization.” 2013. Web. 21 Mar 2019.

Vancouver:

McCormick N. The Development and Evaluation of a Fully-coupled Monolithic Approach to Aero-structural Analysis and Optimization. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/43217.

Council of Science Editors:

McCormick N. The Development and Evaluation of a Fully-coupled Monolithic Approach to Aero-structural Analysis and Optimization. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43217

4. Risi, Benjamin. Propulsion System Development for the CanX-4 and CanX-5 Dual Nanosatellite Formation Flying Mission.

Degree: 2014, University of Toronto

URL: http://hdl.handle.net/1807/65601

►

The Canadian Nanosatellite Advanced Propulsion System is a liquefied cold-gas thruster system that provides propulsive capabilities to CanX-4/-5, the Canadian Advanced Nanospace eXperiment 4 and… (more)

Subjects/Keywords: aerospace; microsatellite; nanosatellite; propulsion; formation flying; canx4; canx5; canx-4; canx-5; canx-4/-5; SFL; UTIAS; cold-gas thruster; satellite; CNAPS; NANOPS; nano; sulfur hexafluoride; SF6; vibration testing; spacecraft environmental testing; propulsion testing; low earth orbit; canx2; canx-2; station keeping; orbit maneuver; orbital station-keeping; liquefied cold-gas propulsion; micropropulsion; engineering; space; canadian; space flight laboratory; canadian advanced nanospace experiment; PSLV; micro-propulsion; thruster; interferometry; ground moving target indicator; on-orbit servicing and inspection; 0538

…Functional Test
Space Flight Laboratory
Thermal Vacuum
*University* *of* *Toronto* Institute for… …flying demonstration mission designed and built at the *University* *of* *Toronto*
Institute for… …built by the
Space Flight Laboratory (SFL) at the *University* *of* *Toronto* Institute…

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APA (6^{th} Edition):

Risi, B. (2014). Propulsion System Development for the CanX-4 and CanX-5 Dual Nanosatellite Formation Flying Mission. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/65601

Chicago Manual of Style (16^{th} Edition):

Risi, Benjamin. “Propulsion System Development for the CanX-4 and CanX-5 Dual Nanosatellite Formation Flying Mission.” 2014. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/65601.

MLA Handbook (7^{th} Edition):

Risi, Benjamin. “Propulsion System Development for the CanX-4 and CanX-5 Dual Nanosatellite Formation Flying Mission.” 2014. Web. 21 Mar 2019.

Vancouver:

Risi B. Propulsion System Development for the CanX-4 and CanX-5 Dual Nanosatellite Formation Flying Mission. [Internet] [Masters thesis]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/65601.

Council of Science Editors:

Risi B. Propulsion System Development for the CanX-4 and CanX-5 Dual Nanosatellite Formation Flying Mission. [Masters Thesis]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/65601

5. Aydin, Besim Tayfun. Controlling the Near-wake of a Circular Cylinder with a Single, Large-scale Tripwire.

Degree: PhD, 2014, University of Toronto

URL: http://hdl.handle.net/1807/68132

Control of the flow past a circular cylinder using a single tripwire on its surface has been studied experimentally as a function of the wire angular location for different wire-to-cylinder diameter ratios (0.029
*Advisors/Committee Members: Ekmekci, Alis, Aerospace Science and Engineering.*

Subjects/Keywords: circular cylinder; flow control; spanwise protrusion; tripwire; vortex shedding; 0538

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APA (6^{th} Edition):

Aydin, B. T. (2014). Controlling the Near-wake of a Circular Cylinder with a Single, Large-scale Tripwire. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/68132

Chicago Manual of Style (16^{th} Edition):

Aydin, Besim Tayfun. “Controlling the Near-wake of a Circular Cylinder with a Single, Large-scale Tripwire.” 2014. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/68132.

MLA Handbook (7^{th} Edition):

Aydin, Besim Tayfun. “Controlling the Near-wake of a Circular Cylinder with a Single, Large-scale Tripwire.” 2014. Web. 21 Mar 2019.

Vancouver:

Aydin BT. Controlling the Near-wake of a Circular Cylinder with a Single, Large-scale Tripwire. [Internet] [Doctoral dissertation]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/68132.

Council of Science Editors:

Aydin BT. Controlling the Near-wake of a Circular Cylinder with a Single, Large-scale Tripwire. [Doctoral Dissertation]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/68132

6.
Forbes, James Richard.
Extensions of Input-output Stability Theory and the Control of *Aerospace* Systems.

Degree: 2011, University of Toronto

URL: http://hdl.handle.net/1807/31751

►

This thesis is concerned with input-output stability theory. Within this framework, it is of interest how inputs map to outputs through an operator that represents… (more)

Subjects/Keywords: control theory; input-output stability; passivity-based control; control of flexible robotic manipulators; spacecraft attitude control; 0538

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APA (6^{th} Edition):

Forbes, J. R. (2011). Extensions of Input-output Stability Theory and the Control of Aerospace Systems. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/31751

Chicago Manual of Style (16^{th} Edition):

Forbes, James Richard. “Extensions of Input-output Stability Theory and the Control of Aerospace Systems.” 2011. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/31751.

MLA Handbook (7^{th} Edition):

Forbes, James Richard. “Extensions of Input-output Stability Theory and the Control of Aerospace Systems.” 2011. Web. 21 Mar 2019.

Vancouver:

Forbes JR. Extensions of Input-output Stability Theory and the Control of Aerospace Systems. [Internet] [Doctoral dissertation]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/31751.

Council of Science Editors:

Forbes JR. Extensions of Input-output Stability Theory and the Control of Aerospace Systems. [Doctoral Dissertation]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31751

7. LeBel, Stefan. Nonlinear Robust Control Synthesis Methods for Spacecraft Applications.

Degree: 2014, University of Toronto

URL: http://hdl.handle.net/1807/65678

►

This thesis focuses on practical methods for constructing robust nonlinear control systems. In general, the development of such control systems is characterized by the solution… (more)

Subjects/Keywords: Nonlinear; Robust; Control; Spacecraft; 0538

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APA (6^{th} Edition):

LeBel, S. (2014). Nonlinear Robust Control Synthesis Methods for Spacecraft Applications. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/65678

Chicago Manual of Style (16^{th} Edition):

LeBel, Stefan. “Nonlinear Robust Control Synthesis Methods for Spacecraft Applications.” 2014. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/65678.

MLA Handbook (7^{th} Edition):

LeBel, Stefan. “Nonlinear Robust Control Synthesis Methods for Spacecraft Applications.” 2014. Web. 21 Mar 2019.

Vancouver:

LeBel S. Nonlinear Robust Control Synthesis Methods for Spacecraft Applications. [Internet] [Doctoral dissertation]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/65678.

Council of Science Editors:

LeBel S. Nonlinear Robust Control Synthesis Methods for Spacecraft Applications. [Doctoral Dissertation]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/65678

8. Osusky, Lana. A Numerical Methodology for Aerodynamic Shape Optimization in Turbulent Flow Enabling Large Geometric Variation.

Degree: 2014, University of Toronto

URL: http://hdl.handle.net/1807/44125

►

The increase in the availability and power of computational resources over the last fifteen years has contributed to the development of many different types of… (more)

Subjects/Keywords: Optimization; Computational Aerodynamics; Numerical Methods; Turbulent Flows; 0538

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APA (6^{th} Edition):

Osusky, L. (2014). A Numerical Methodology for Aerodynamic Shape Optimization in Turbulent Flow Enabling Large Geometric Variation. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/44125

Chicago Manual of Style (16^{th} Edition):

Osusky, Lana. “A Numerical Methodology for Aerodynamic Shape Optimization in Turbulent Flow Enabling Large Geometric Variation.” 2014. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/44125.

MLA Handbook (7^{th} Edition):

Osusky, Lana. “A Numerical Methodology for Aerodynamic Shape Optimization in Turbulent Flow Enabling Large Geometric Variation.” 2014. Web. 21 Mar 2019.

Vancouver:

Osusky L. A Numerical Methodology for Aerodynamic Shape Optimization in Turbulent Flow Enabling Large Geometric Variation. [Internet] [Doctoral dissertation]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/44125.

Council of Science Editors:

Osusky L. A Numerical Methodology for Aerodynamic Shape Optimization in Turbulent Flow Enabling Large Geometric Variation. [Doctoral Dissertation]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/44125

9. Osusky, Michal. A Parallel Newton-Krylov-Schur Algorithm for the Reynolds-Averaged Navier-Stokes Equations.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/43684

►

Aerodynamic shape optimization and multidisciplinary optimization algorithms have the potential not only to improve conventional aircraft, but also to enable the design of novel configurations.… (more)

Subjects/Keywords: computational fluid dynamics; turbulent flow; numerical algorithms; Newton-Krylov; Approximate- Schur preconditioner; parallel computations; SBP-SAT discretization; 0538

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APA (6^{th} Edition):

Osusky, M. (2013). A Parallel Newton-Krylov-Schur Algorithm for the Reynolds-Averaged Navier-Stokes Equations. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/43684

Chicago Manual of Style (16^{th} Edition):

Osusky, Michal. “A Parallel Newton-Krylov-Schur Algorithm for the Reynolds-Averaged Navier-Stokes Equations.” 2013. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/43684.

MLA Handbook (7^{th} Edition):

Osusky, Michal. “A Parallel Newton-Krylov-Schur Algorithm for the Reynolds-Averaged Navier-Stokes Equations.” 2013. Web. 21 Mar 2019.

Vancouver:

Osusky M. A Parallel Newton-Krylov-Schur Algorithm for the Reynolds-Averaged Navier-Stokes Equations. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/43684.

Council of Science Editors:

Osusky M. A Parallel Newton-Krylov-Schur Algorithm for the Reynolds-Averaged Navier-Stokes Equations. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43684

10. Gatsis, John. Preconditioning Techniques for a Newton-Krylov Algorithm for the Compressible Navier-Stokes Equations.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/43576

►

An investigation of preconditioning techniques is presented for a Newton – Krylov algorithm that is used for the computation of steady, compressible, high Reynolds number flows… (more)

Subjects/Keywords: computational fluid dynamics; algorithms; preconditioning; nonlinear partial differential equations; 0538

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APA (6^{th} Edition):

Gatsis, J. (2013). Preconditioning Techniques for a Newton-Krylov Algorithm for the Compressible Navier-Stokes Equations. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/43576

Chicago Manual of Style (16^{th} Edition):

Gatsis, John. “Preconditioning Techniques for a Newton-Krylov Algorithm for the Compressible Navier-Stokes Equations.” 2013. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/43576.

MLA Handbook (7^{th} Edition):

Gatsis, John. “Preconditioning Techniques for a Newton-Krylov Algorithm for the Compressible Navier-Stokes Equations.” 2013. Web. 21 Mar 2019.

Vancouver:

Gatsis J. Preconditioning Techniques for a Newton-Krylov Algorithm for the Compressible Navier-Stokes Equations. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/43576.

Council of Science Editors:

Gatsis J. Preconditioning Techniques for a Newton-Krylov Algorithm for the Compressible Navier-Stokes Equations. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43576

11. Tong, Chi Hay. Laser-Based 3D Mapping and Navigation in Planetary Worksite Environments.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/43740

►

For robotic deployments in planetary worksite environments, map construction and navigation are essential for tasks such as base construction, scientific investigation, and in-situ resource utilization.… (more)

Subjects/Keywords: gaussian process gauss-newton; state estimation; slam; 0771

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APA (6^{th} Edition):

Tong, C. H. (2013). Laser-Based 3D Mapping and Navigation in Planetary Worksite Environments. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/43740

Chicago Manual of Style (16^{th} Edition):

Tong, Chi Hay. “Laser-Based 3D Mapping and Navigation in Planetary Worksite Environments.” 2013. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/43740.

MLA Handbook (7^{th} Edition):

Tong, Chi Hay. “Laser-Based 3D Mapping and Navigation in Planetary Worksite Environments.” 2013. Web. 21 Mar 2019.

Vancouver:

Tong CH. Laser-Based 3D Mapping and Navigation in Planetary Worksite Environments. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/43740.

Council of Science Editors:

Tong CH. Laser-Based 3D Mapping and Navigation in Planetary Worksite Environments. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43740

12. Kenway, Gaetan Kristian Wiscombe. A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/35861

►

This thesis presents new tools and techniques developed to address the challenging problem of high-fidelity aerostructural optimization with respect to large numbers of design variables.… (more)

Subjects/Keywords: Multidisciplinary Optimization; Aircraft Design; CFD; CSM; 0538

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APA (6^{th} Edition):

Kenway, G. K. W. (2013). A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/35861

Chicago Manual of Style (16^{th} Edition):

Kenway, Gaetan Kristian Wiscombe. “A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations.” 2013. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/35861.

MLA Handbook (7^{th} Edition):

Kenway, Gaetan Kristian Wiscombe. “A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations.” 2013. Web. 21 Mar 2019.

Vancouver:

Kenway GKW. A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/35861.

Council of Science Editors:

Kenway GKW. A Scalable, Parallel Approach for Multi-point, High-fidelity Aerostructural Optimization of Aircraft Configurations. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/35861

13. Martin, Adrian. A Framework for the Development of Scalable Heterogeneous Robot Teams with Dynamically Distributed Processing.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/35895

►

As the applications of mobile robotics evolve it has become increasingly less practical for researchers to design custom hardware and control systems for each problem.… (more)

Subjects/Keywords: robot teams; control system architecture; distributed; heterogeneous; failure recovery; SLAM; hardware-in-the-loop; 0771

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APA (6^{th} Edition):

Martin, A. (2013). A Framework for the Development of Scalable Heterogeneous Robot Teams with Dynamically Distributed Processing. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/35895

Chicago Manual of Style (16^{th} Edition):

Martin, Adrian. “A Framework for the Development of Scalable Heterogeneous Robot Teams with Dynamically Distributed Processing.” 2013. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/35895.

MLA Handbook (7^{th} Edition):

Martin, Adrian. “A Framework for the Development of Scalable Heterogeneous Robot Teams with Dynamically Distributed Processing.” 2013. Web. 21 Mar 2019.

Vancouver:

Martin A. A Framework for the Development of Scalable Heterogeneous Robot Teams with Dynamically Distributed Processing. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/35895.

Council of Science Editors:

Martin A. A Framework for the Development of Scalable Heterogeneous Robot Teams with Dynamically Distributed Processing. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/35895

14. Stenning, Braden Edward. Path/Action Planning for a Mobile Robot.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/36006

►

This thesis consists of two parts united by the theme of path/action planning for a mobile robot. Part I presents the Second Opinion Planner (SOP),… (more)

Subjects/Keywords: mobile robot; autonomy; field robotics; path planning; 0538; Robotics

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APA (6^{th} Edition):

Stenning, B. E. (2013). Path/Action Planning for a Mobile Robot. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/36006

Chicago Manual of Style (16^{th} Edition):

Stenning, Braden Edward. “Path/Action Planning for a Mobile Robot.” 2013. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/36006.

MLA Handbook (7^{th} Edition):

Stenning, Braden Edward. “Path/Action Planning for a Mobile Robot.” 2013. Web. 21 Mar 2019.

Vancouver:

Stenning BE. Path/Action Planning for a Mobile Robot. [Internet] [Doctoral dissertation]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/36006.

Council of Science Editors:

Stenning BE. Path/Action Planning for a Mobile Robot. [Doctoral Dissertation]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/36006

15. Furgale, Paul. Extensions to the Visual Odometry Pipeline for the Exploration of Planetary Surfaces.

Degree: 2011, University of Toronto

URL: http://hdl.handle.net/1807/31753

►

Mars represents one of the most important targets for space exploration in the next 10 to 30 years, particularly because of evidence of liquid water… (more)

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APA (6^{th} Edition):

Furgale, P. (2011). Extensions to the Visual Odometry Pipeline for the Exploration of Planetary Surfaces. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/31753

Chicago Manual of Style (16^{th} Edition):

Furgale, Paul. “Extensions to the Visual Odometry Pipeline for the Exploration of Planetary Surfaces.” 2011. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/31753.

MLA Handbook (7^{th} Edition):

Furgale, Paul. “Extensions to the Visual Odometry Pipeline for the Exploration of Planetary Surfaces.” 2011. Web. 21 Mar 2019.

Vancouver:

Furgale P. Extensions to the Visual Odometry Pipeline for the Exploration of Planetary Surfaces. [Internet] [Doctoral dissertation]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/31753.

Council of Science Editors:

Furgale P. Extensions to the Visual Odometry Pipeline for the Exploration of Planetary Surfaces. [Doctoral Dissertation]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31753

16. Gagnon, Hugo. Geometry Control System for Exploratory Shape Optimization Applied to High-fidelity Aerodynamic Design of Unconventional Aircraft.

Degree: PhD, 2015, University of Toronto

URL: http://hdl.handle.net/1807/69270

► This thesis represents a step forward to bring geometry parameterization and control on par with the disciplinary analyses involved in shape optimization, particularly high-fidelity aerodynamic…
(more)

Subjects/Keywords: aerodynamic shape optimization; aircraft design; geometry generation; induced drag; NURBS; shape exploration; 0538

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APA (6^{th} Edition):

Gagnon, H. (2015). Geometry Control System for Exploratory Shape Optimization Applied to High-fidelity Aerodynamic Design of Unconventional Aircraft. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/69270

Chicago Manual of Style (16^{th} Edition):

Gagnon, Hugo. “Geometry Control System for Exploratory Shape Optimization Applied to High-fidelity Aerodynamic Design of Unconventional Aircraft.” 2015. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/69270.

MLA Handbook (7^{th} Edition):

Gagnon, Hugo. “Geometry Control System for Exploratory Shape Optimization Applied to High-fidelity Aerodynamic Design of Unconventional Aircraft.” 2015. Web. 21 Mar 2019.

Vancouver:

Gagnon H. Geometry Control System for Exploratory Shape Optimization Applied to High-fidelity Aerodynamic Design of Unconventional Aircraft. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/69270.

Council of Science Editors:

Gagnon H. Geometry Control System for Exploratory Shape Optimization Applied to High-fidelity Aerodynamic Design of Unconventional Aircraft. [Doctoral Dissertation]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/69270

17. Reichert, Todd. Kinematic Optimization in Birds, Bats and Ornithopters.

Degree: 2011, University of Toronto

URL: http://hdl.handle.net/1807/31913

►

Birds and bats employ a variety of advanced wing motions in the efficient production of thrust. The purpose of this thesis is to quantify the… (more)

Subjects/Keywords: Ornithopter; Unsteady aerodynamics; Aeroelasticity; Bird; Bat; Flapping wing flight; Optimization; Kinematics; Vortex panel method; Non-linear finite element; Propulsive efficiency; 0538

…*University* *of* *Toronto* Institute for Aerospace Studies
xix
Part I
Introduction
1
Chapter 1…

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APA (6^{th} Edition):

Reichert, T. (2011). Kinematic Optimization in Birds, Bats and Ornithopters. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/31913

Chicago Manual of Style (16^{th} Edition):

Reichert, Todd. “Kinematic Optimization in Birds, Bats and Ornithopters.” 2011. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/31913.

MLA Handbook (7^{th} Edition):

Reichert, Todd. “Kinematic Optimization in Birds, Bats and Ornithopters.” 2011. Web. 21 Mar 2019.

Vancouver:

Reichert T. Kinematic Optimization in Birds, Bats and Ornithopters. [Internet] [Doctoral dissertation]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/31913.

Council of Science Editors:

Reichert T. Kinematic Optimization in Birds, Bats and Ornithopters. [Doctoral Dissertation]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31913

18. Mu, Yarong. Development and Applications of 3D-DIVIMP(HC) Monte Carlo Impurity Modeling Code.

Degree: 2009, University of Toronto

URL: http://hdl.handle.net/1807/19205

►

A self-contained gas injection system for the Divertor Material Evaluation System (DiMES) on DIII-D, the Porous Plug Injector (PPI), has been employed by A. McLean… (more)

Subjects/Keywords: Nuclear Fusion; Boundary Physics; Plasma; Tokamaks; 0552; 0538; 0791

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APA (6^{th} Edition):

Mu, Y. (2009). Development and Applications of 3D-DIVIMP(HC) Monte Carlo Impurity Modeling Code. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/19205

Chicago Manual of Style (16^{th} Edition):

Mu, Yarong. “Development and Applications of 3D-DIVIMP(HC) Monte Carlo Impurity Modeling Code.” 2009. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/19205.

MLA Handbook (7^{th} Edition):

Mu, Yarong. “Development and Applications of 3D-DIVIMP(HC) Monte Carlo Impurity Modeling Code.” 2009. Web. 21 Mar 2019.

Vancouver:

Mu Y. Development and Applications of 3D-DIVIMP(HC) Monte Carlo Impurity Modeling Code. [Internet] [Doctoral dissertation]. University of Toronto; 2009. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/19205.

Council of Science Editors:

Mu Y. Development and Applications of 3D-DIVIMP(HC) Monte Carlo Impurity Modeling Code. [Doctoral Dissertation]. University of Toronto; 2009. Available from: http://hdl.handle.net/1807/19205

19. Rumpfkeil, Markus Peer. Airfoil Optimization for Unsteady Flows with Application to High-lift Noise Reduction.

Degree: 2008, University of Toronto

URL: http://hdl.handle.net/1807/17241

►

The use of steady-state aerodynamic optimization methods in the computational fluid dynamic (CFD) community is fairly well established. In particular, the use of adjoint methods… (more)

Subjects/Keywords: unsteady discrete adjoint; unsteady optimization; hybrid acoustic predictions; computational fluid dynamic; airframe-generated noise; optimal control; gradient-based optimization; Ffowcs Williams and Hawkings equation; 0538

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APA (6^{th} Edition):

Rumpfkeil, M. P. (2008). Airfoil Optimization for Unsteady Flows with Application to High-lift Noise Reduction. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/17241

Chicago Manual of Style (16^{th} Edition):

Rumpfkeil, Markus Peer. “Airfoil Optimization for Unsteady Flows with Application to High-lift Noise Reduction.” 2008. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/17241.

MLA Handbook (7^{th} Edition):

Rumpfkeil, Markus Peer. “Airfoil Optimization for Unsteady Flows with Application to High-lift Noise Reduction.” 2008. Web. 21 Mar 2019.

Vancouver:

Rumpfkeil MP. Airfoil Optimization for Unsteady Flows with Application to High-lift Noise Reduction. [Internet] [Doctoral dissertation]. University of Toronto; 2008. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/17241.

Council of Science Editors:

Rumpfkeil MP. Airfoil Optimization for Unsteady Flows with Application to High-lift Noise Reduction. [Doctoral Dissertation]. University of Toronto; 2008. Available from: http://hdl.handle.net/1807/17241

20. Lanewala, Hasnain. Multi-dimensional Nitric Oxide Emissions Predictor for Preliminary Gas Turbine Combustor Design Optimization.

Degree: 2013, University of Toronto

URL: http://hdl.handle.net/1807/43987

►

This thesis pertains to development of preliminary combustor design tools for prediction of NOx emissions from aircraft gas turbine combustors. These tools are developed in… (more)

Subjects/Keywords: Emissions; NOx; Modeling; Combustor; Combustion; ICAO; Reactor; Network; 0538

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APA (6^{th} Edition):

Lanewala, H. (2013). Multi-dimensional Nitric Oxide Emissions Predictor for Preliminary Gas Turbine Combustor Design Optimization. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43987

Chicago Manual of Style (16^{th} Edition):

Lanewala, Hasnain. “Multi-dimensional Nitric Oxide Emissions Predictor for Preliminary Gas Turbine Combustor Design Optimization.” 2013. Masters Thesis, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/43987.

MLA Handbook (7^{th} Edition):

Lanewala, Hasnain. “Multi-dimensional Nitric Oxide Emissions Predictor for Preliminary Gas Turbine Combustor Design Optimization.” 2013. Web. 21 Mar 2019.

Vancouver:

Lanewala H. Multi-dimensional Nitric Oxide Emissions Predictor for Preliminary Gas Turbine Combustor Design Optimization. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/43987.

Council of Science Editors:

Lanewala H. Multi-dimensional Nitric Oxide Emissions Predictor for Preliminary Gas Turbine Combustor Design Optimization. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43987

21. Northrup, Scott Andrew. A Parallel Implicit Adaptive Mesh Refinement Algorithm for Predicting Unsteady Fully-compressible Reactive Flows.

Degree: 2014, University of Toronto

URL: http://hdl.handle.net/1807/65709

►

A new parallel implicit adaptive mesh refinement (AMR) algorithm is developed for the prediction of unsteady behaviour of laminar flames. The scheme is applied to… (more)

Subjects/Keywords: CFD; Newton-Krylov-Schwarz; Laminar Flames; 0538

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APA (6^{th} Edition):

Northrup, S. A. (2014). A Parallel Implicit Adaptive Mesh Refinement Algorithm for Predicting Unsteady Fully-compressible Reactive Flows. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/65709

Chicago Manual of Style (16^{th} Edition):

Northrup, Scott Andrew. “A Parallel Implicit Adaptive Mesh Refinement Algorithm for Predicting Unsteady Fully-compressible Reactive Flows.” 2014. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/65709.

MLA Handbook (7^{th} Edition):

Northrup, Scott Andrew. “A Parallel Implicit Adaptive Mesh Refinement Algorithm for Predicting Unsteady Fully-compressible Reactive Flows.” 2014. Web. 21 Mar 2019.

Vancouver:

Northrup SA. A Parallel Implicit Adaptive Mesh Refinement Algorithm for Predicting Unsteady Fully-compressible Reactive Flows. [Internet] [Doctoral dissertation]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/65709.

Council of Science Editors:

Northrup SA. A Parallel Implicit Adaptive Mesh Refinement Algorithm for Predicting Unsteady Fully-compressible Reactive Flows. [Doctoral Dissertation]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/65709

22. Chhabra, Robin. A Unified Geometric Framework for Kinematics, Dynamics and Concurrent Control of Free-base, Open-chain Multi-body Systems with Holonomic and Nonholonomic Constraints.

Degree: 2014, University of Toronto

URL: http://hdl.handle.net/1807/65650

►

This thesis presents a geometric approach to studying kinematics, dynamics and controls of open-chain multi-body systems with non-zero momentum and multi-degree-of-freedom joints subject to holonomic… (more)

Subjects/Keywords: Open-chain multi-body systems; Kinematics; Hamiltonian dynamics; Differential geometry; Lie groups; Concurrent control; 0771; 0538

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APA (6^{th} Edition):

Chhabra, R. (2014). A Unified Geometric Framework for Kinematics, Dynamics and Concurrent Control of Free-base, Open-chain Multi-body Systems with Holonomic and Nonholonomic Constraints. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/65650

Chicago Manual of Style (16^{th} Edition):

Chhabra, Robin. “A Unified Geometric Framework for Kinematics, Dynamics and Concurrent Control of Free-base, Open-chain Multi-body Systems with Holonomic and Nonholonomic Constraints.” 2014. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/65650.

MLA Handbook (7^{th} Edition):

Chhabra, Robin. “A Unified Geometric Framework for Kinematics, Dynamics and Concurrent Control of Free-base, Open-chain Multi-body Systems with Holonomic and Nonholonomic Constraints.” 2014. Web. 21 Mar 2019.

Vancouver:

Chhabra R. A Unified Geometric Framework for Kinematics, Dynamics and Concurrent Control of Free-base, Open-chain Multi-body Systems with Holonomic and Nonholonomic Constraints. [Internet] [Doctoral dissertation]. University of Toronto; 2014. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/65650.

Council of Science Editors:

Chhabra R. A Unified Geometric Framework for Kinematics, Dynamics and Concurrent Control of Free-base, Open-chain Multi-body Systems with Holonomic and Nonholonomic Constraints. [Doctoral Dissertation]. University of Toronto; 2014. Available from: http://hdl.handle.net/1807/65650

23. Kennedy, Graeme. Aerostructural Analysis and Design Optimization of Composite Aircraft.

Degree: 2012, University of Toronto

URL: http://hdl.handle.net/1807/34078

►

High-performance composite materials exhibit both anisotropic strength and stiffness properties. These anisotropic properties can be used to produce highly-tailored aircraft structures that meet stringent performance… (more)

Subjects/Keywords: Aerostructural; Optimization; 0538

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APA (6^{th} Edition):

Kennedy, G. (2012). Aerostructural Analysis and Design Optimization of Composite Aircraft. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/34078

Chicago Manual of Style (16^{th} Edition):

Kennedy, Graeme. “Aerostructural Analysis and Design Optimization of Composite Aircraft.” 2012. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/34078.

MLA Handbook (7^{th} Edition):

Kennedy, Graeme. “Aerostructural Analysis and Design Optimization of Composite Aircraft.” 2012. Web. 21 Mar 2019.

Vancouver:

Kennedy G. Aerostructural Analysis and Design Optimization of Composite Aircraft. [Internet] [Doctoral dissertation]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/34078.

Council of Science Editors:

Kennedy G. Aerostructural Analysis and Design Optimization of Composite Aircraft. [Doctoral Dissertation]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/34078

24. James, Kai A. Aerostructural Shape and Topology Optimization of Aircraft Wings.

Degree: 2012, University of Toronto

URL: http://hdl.handle.net/1807/32745

►

A series of novel algorithms for performing aerostructural shape and topology optimization are introduced and applied to the design of aircraft wings. An isoparametric level… (more)

Subjects/Keywords: Multidisciplinary Design Optimization; Topology Optimization; 0538

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

APA (6^{th} Edition):

James, K. A. (2012). Aerostructural Shape and Topology Optimization of Aircraft Wings. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/32745

Chicago Manual of Style (16^{th} Edition):

James, Kai A. “Aerostructural Shape and Topology Optimization of Aircraft Wings.” 2012. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/32745.

MLA Handbook (7^{th} Edition):

James, Kai A. “Aerostructural Shape and Topology Optimization of Aircraft Wings.” 2012. Web. 21 Mar 2019.

Vancouver:

James KA. Aerostructural Shape and Topology Optimization of Aircraft Wings. [Internet] [Doctoral dissertation]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/32745.

Council of Science Editors:

James KA. Aerostructural Shape and Topology Optimization of Aircraft Wings. [Doctoral Dissertation]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/32745

25. Leung, Keith Yu Kit. Cooperative Localization and Mapping in Sparsely-communicating Robot Networks.

Degree: 2012, University of Toronto

URL: http://hdl.handle.net/1807/32809

►

This thesis examines the use of multiple robots in cooperative simultaneous localization and mapping (SLAM), where each robot must estimate the poses of all robots… (more)

Subjects/Keywords: Multi-robot System; Simultaneous Localization and Mapping (SLAM); Mobile Robotics; Networked Robotics; 0771

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APA (6^{th} Edition):

Leung, K. Y. K. (2012). Cooperative Localization and Mapping in Sparsely-communicating Robot Networks. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/32809

Chicago Manual of Style (16^{th} Edition):

Leung, Keith Yu Kit. “Cooperative Localization and Mapping in Sparsely-communicating Robot Networks.” 2012. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/32809.

MLA Handbook (7^{th} Edition):

Leung, Keith Yu Kit. “Cooperative Localization and Mapping in Sparsely-communicating Robot Networks.” 2012. Web. 21 Mar 2019.

Vancouver:

Leung KYK. Cooperative Localization and Mapping in Sparsely-communicating Robot Networks. [Internet] [Doctoral dissertation]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/32809.

Council of Science Editors:

Leung KYK. Cooperative Localization and Mapping in Sparsely-communicating Robot Networks. [Doctoral Dissertation]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/32809

26. McDonald, James Gerald. Extended Fluid-dynamic Modelling for Numerical Solution of Micro-Scale Flows.

Degree: 2011, University of Toronto

URL: http://hdl.handle.net/1807/27593

►

This study is concerned with the development of extended fluid-dynamic models for the prediction of micro-scale flows. When compared to classical fluid descriptions, such models… (more)

Subjects/Keywords: Moment Closures; Mico-Scale Flows; 0538

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APA (6^{th} Edition):

McDonald, J. G. (2011). Extended Fluid-dynamic Modelling for Numerical Solution of Micro-Scale Flows. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/27593

Chicago Manual of Style (16^{th} Edition):

McDonald, James Gerald. “Extended Fluid-dynamic Modelling for Numerical Solution of Micro-Scale Flows.” 2011. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/27593.

MLA Handbook (7^{th} Edition):

McDonald, James Gerald. “Extended Fluid-dynamic Modelling for Numerical Solution of Micro-Scale Flows.” 2011. Web. 21 Mar 2019.

Vancouver:

McDonald JG. Extended Fluid-dynamic Modelling for Numerical Solution of Micro-Scale Flows. [Internet] [Doctoral dissertation]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/27593.

Council of Science Editors:

McDonald JG. Extended Fluid-dynamic Modelling for Numerical Solution of Micro-Scale Flows. [Doctoral Dissertation]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/27593

27. Roszell, John Patrick Town. The Effect of Ion Energy and Substrate Temperature on Deuterium Trapping in Tungsten.

Degree: 2012, University of Toronto

URL: http://hdl.handle.net/1807/34868

►

Tungsten is a candidate plasma facing material for next generation magnetic fusion devices such as ITER and there are major operational and safety issues associated… (more)

Subjects/Keywords: Deuterium Retention; Plasma Materials Interactions

…al. [37] on the linear accelerator facility at the
*University* *of* *Toronto*. All…

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APA (6^{th} Edition):

Roszell, J. P. T. (2012). The Effect of Ion Energy and Substrate Temperature on Deuterium Trapping in Tungsten. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/34868

Chicago Manual of Style (16^{th} Edition):

Roszell, John Patrick Town. “The Effect of Ion Energy and Substrate Temperature on Deuterium Trapping in Tungsten.” 2012. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/34868.

MLA Handbook (7^{th} Edition):

Roszell, John Patrick Town. “The Effect of Ion Energy and Substrate Temperature on Deuterium Trapping in Tungsten.” 2012. Web. 21 Mar 2019.

Vancouver:

Roszell JPT. The Effect of Ion Energy and Substrate Temperature on Deuterium Trapping in Tungsten. [Internet] [Doctoral dissertation]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/34868.

Council of Science Editors:

Roszell JPT. The Effect of Ion Energy and Substrate Temperature on Deuterium Trapping in Tungsten. [Doctoral Dissertation]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/34868

28. Jha, Pradeep Kumar. Modelling Detailed-chemistry Effects on Turbulent Diffusion Flames using a Parallel Solution-adaptive Scheme.

Degree: 2011, University of Toronto

URL: http://hdl.handle.net/1807/31791

►

Capturing the effects of detailed-chemistry on turbulent combustion processes is a central challenge faced by the numerical combustion community. However, the inherent complexity and non-linear… (more)

Subjects/Keywords: Computational Fluid Dynamics; Computational Combustion; 0538

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APA (6^{th} Edition):

Jha, P. K. (2011). Modelling Detailed-chemistry Effects on Turbulent Diffusion Flames using a Parallel Solution-adaptive Scheme. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/31791

Chicago Manual of Style (16^{th} Edition):

Jha, Pradeep Kumar. “Modelling Detailed-chemistry Effects on Turbulent Diffusion Flames using a Parallel Solution-adaptive Scheme.” 2011. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/31791.

MLA Handbook (7^{th} Edition):

Jha, Pradeep Kumar. “Modelling Detailed-chemistry Effects on Turbulent Diffusion Flames using a Parallel Solution-adaptive Scheme.” 2011. Web. 21 Mar 2019.

Vancouver:

Jha PK. Modelling Detailed-chemistry Effects on Turbulent Diffusion Flames using a Parallel Solution-adaptive Scheme. [Internet] [Doctoral dissertation]. University of Toronto; 2011. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/31791.

Council of Science Editors:

Jha PK. Modelling Detailed-chemistry Effects on Turbulent Diffusion Flames using a Parallel Solution-adaptive Scheme. [Doctoral Dissertation]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31791

29. Mader, Charles. Stability-constrained Aerodynamic Shape Optimization with Applications to Flying Wings.

Degree: 2012, University of Toronto

URL: http://hdl.handle.net/1807/32758

►

A set of techniques is developed that allows the incorporation of flight dynamics metrics as an additional discipline in a high-fidelity aerodynamic optimization. Specifically, techniques… (more)

Subjects/Keywords: optimization; MDO; design optimization; aerodynamic shape optimization; flying wings; aircraft design; stability; aerospace; 0538

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APA (6^{th} Edition):

Mader, C. (2012). Stability-constrained Aerodynamic Shape Optimization with Applications to Flying Wings. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/32758

Chicago Manual of Style (16^{th} Edition):

Mader, Charles. “Stability-constrained Aerodynamic Shape Optimization with Applications to Flying Wings.” 2012. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/32758.

MLA Handbook (7^{th} Edition):

Mader, Charles. “Stability-constrained Aerodynamic Shape Optimization with Applications to Flying Wings.” 2012. Web. 21 Mar 2019.

Vancouver:

Mader C. Stability-constrained Aerodynamic Shape Optimization with Applications to Flying Wings. [Internet] [Doctoral dissertation]. University of Toronto; 2012. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/32758.

Council of Science Editors:

Mader C. Stability-constrained Aerodynamic Shape Optimization with Applications to Flying Wings. [Doctoral Dissertation]. University of Toronto; 2012. Available from: http://hdl.handle.net/1807/32758

30. Lambe, Andrew Borean. A Matrix-free Algorithm for Multidisciplinary Design Optimization.

Degree: PhD, 2015, University of Toronto

URL: http://hdl.handle.net/1807/69350

► Multidisciplinary design optimization (MDO) is an approach to *engineering* design that exploits the coupling between components or knowledge disciplines in a complex system to improve…
(more)

Subjects/Keywords: aerostructural optimization; matrix-free; MDO architectures; multidisciplinary design optimization (MDO); nonlinear optimization; 0538

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APA (6^{th} Edition):

Lambe, A. B. (2015). A Matrix-free Algorithm for Multidisciplinary Design Optimization. (Doctoral Dissertation). University of Toronto. Retrieved from http://hdl.handle.net/1807/69350

Chicago Manual of Style (16^{th} Edition):

Lambe, Andrew Borean. “A Matrix-free Algorithm for Multidisciplinary Design Optimization.” 2015. Doctoral Dissertation, University of Toronto. Accessed March 21, 2019. http://hdl.handle.net/1807/69350.

MLA Handbook (7^{th} Edition):

Lambe, Andrew Borean. “A Matrix-free Algorithm for Multidisciplinary Design Optimization.” 2015. Web. 21 Mar 2019.

Vancouver:

Lambe AB. A Matrix-free Algorithm for Multidisciplinary Design Optimization. [Internet] [Doctoral dissertation]. University of Toronto; 2015. [cited 2019 Mar 21]. Available from: http://hdl.handle.net/1807/69350.

Council of Science Editors:

Lambe AB. A Matrix-free Algorithm for Multidisciplinary Design Optimization. [Doctoral Dissertation]. University of Toronto; 2015. Available from: http://hdl.handle.net/1807/69350