Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for +publisher:"University of Toronto" +contributor:("Aerospace Science and Engineering"). Showing records 1 – 30 of 339 total matches.

[1] [2] [3] [4] [5] … [12]

Search Limiters

Last 2 Years | English Only

Levels

▼ Search Limiters

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

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… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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)

Subjects/Keywords: 0538; 0771

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Page 1 Page 2 Page 3 Page 4 Page 5

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th 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 (16th 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 (7th 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

[1] [2] [3] [4] [5] … [12]

.