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You searched for subject:(Propulsion AND Power). Showing records 1 – 30 of 159 total matches.

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Embry-Riddle Aeronautical University

1. Yeung, Tsz Him. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design.

Degree: MSin Aerospace Engineering, Graduate Studies, 2019, Embry-Riddle Aeronautical University

  This thesis focuses on electric propulsion technology associated with serial hybrid power plants most commonly associated with urban air mobility vehicles. While closed form… (more)

Subjects/Keywords: Propulsion and Power

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APA (6th Edition):

Yeung, T. H. (2019). Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/457

Chicago Manual of Style (16th Edition):

Yeung, Tsz Him. “Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design.” 2019. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/edt/457.

MLA Handbook (7th Edition):

Yeung, Tsz Him. “Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design.” 2019. Web. 08 May 2021.

Vancouver:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2021 May 08]. Available from: https://commons.erau.edu/edt/457.

Council of Science Editors:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Masters Thesis]. Embry-Riddle Aeronautical University; 2019. Available from: https://commons.erau.edu/edt/457


Cal Poly

2. Green, Michael W. HAPSS, Hybrid Aircraft Propulsion System Synthesis.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Hybrid Aircraft Propulsion System Synthesis (HAPSS) is a computer program that sizes and analyzes pure-series hybrid electric propulsion systems for aircraft. The development of… (more)

Subjects/Keywords: Propulsion and Power

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APA (6th Edition):

Green, M. W. (2012). HAPSS, Hybrid Aircraft Propulsion System Synthesis. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134

Chicago Manual of Style (16th Edition):

Green, Michael W. “HAPSS, Hybrid Aircraft Propulsion System Synthesis.” 2012. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134.

MLA Handbook (7th Edition):

Green, Michael W. “HAPSS, Hybrid Aircraft Propulsion System Synthesis.” 2012. Web. 08 May 2021.

Vancouver:

Green MW. HAPSS, Hybrid Aircraft Propulsion System Synthesis. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134.

Council of Science Editors:

Green MW. HAPSS, Hybrid Aircraft Propulsion System Synthesis. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/817 ; 10.15368/theses.2012.134


University of Tennessee – Knoxville

3. Sung, Rayne. A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet.

Degree: MS, Aerospace Engineering, 2013, University of Tennessee – Knoxville

  GasTurb 11 and the Gas Turbine Simulation Program (GSP) 11 are two commercially available gas turbine simulation programs used by industrial professionals and academic… (more)

Subjects/Keywords: Propulsion; Turbojet Engine; Thermodynamics; Propulsion and Power

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APA (6th Edition):

Sung, R. (2013). A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2466

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Sung, Rayne. “A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet.” 2013. Thesis, University of Tennessee – Knoxville. Accessed May 08, 2021. https://trace.tennessee.edu/utk_gradthes/2466.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Sung, Rayne. “A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet.” 2013. Web. 08 May 2021.

Vancouver:

Sung R. A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet. [Internet] [Thesis]. University of Tennessee – Knoxville; 2013. [cited 2021 May 08]. Available from: https://trace.tennessee.edu/utk_gradthes/2466.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Sung R. A Comparative Study of the Gas Turbine Simulation Program (GSP) 11 and GasTurb 11 on Their Respective Simulations for a Single-Spool Turbojet. [Thesis]. University of Tennessee – Knoxville; 2013. Available from: https://trace.tennessee.edu/utk_gradthes/2466

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Cal Poly

4. McGehee, Will Alan. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  The need for micropropulsion solutions for spacecraft has been steadily increasing as scientific payloads require higher accuracy maneuvers and as the use of small… (more)

Subjects/Keywords: Electrospray; Colloid; Thruster; Propulsion; Micropropulsion; Electric Propulsion; Propulsion and Power

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APA (6th Edition):

McGehee, W. A. (2019). Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93

Chicago Manual of Style (16th Edition):

McGehee, Will Alan. “Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.” 2019. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93.

MLA Handbook (7th Edition):

McGehee, Will Alan. “Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.” 2019. Web. 08 May 2021.

Vancouver:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93.

Council of Science Editors:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2064 ; 10.15368/theses.2019.93


Embry-Riddle Aeronautical University

5. Espa˜na-Heredia, Luis Estefano Ferrer-Vidal. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  Pressure gain combustion has been known to be more thermodynamically efficient than its constant pressure counterpart, which employs deflagration. Integration of pressure gain combustors… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Espa˜na-Heredia, L. E. F. (2014). Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/158

Chicago Manual of Style (16th Edition):

Espa˜na-Heredia, Luis Estefano Ferrer-Vidal. “Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/edt/158.

MLA Handbook (7th Edition):

Espa˜na-Heredia, Luis Estefano Ferrer-Vidal. “Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration.” 2014. Web. 08 May 2021.

Vancouver:

Espa˜na-Heredia LEF. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2021 May 08]. Available from: https://commons.erau.edu/edt/158.

Council of Science Editors:

Espa˜na-Heredia LEF. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/158


Utah State University

6. Chamberlain, Britany L. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.

Degree: MS, Mechanical and Aerospace Engineering, 2018, Utah State University

  Three-dimensional, additive printing has emerged as an exciting new technology for the design and manufacture of small spacecraft systems. Using 3-D printed thermoplastic materials,… (more)

Subjects/Keywords: hybrid rocket; propulsion; additive manufacturing; CubeSat; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Chamberlain, B. L. (2018). Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7285

Chicago Manual of Style (16th Edition):

Chamberlain, Britany L. “Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.” 2018. Masters Thesis, Utah State University. Accessed May 08, 2021. https://digitalcommons.usu.edu/etd/7285.

MLA Handbook (7th Edition):

Chamberlain, Britany L. “Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.” 2018. Web. 08 May 2021.

Vancouver:

Chamberlain BL. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2021 May 08]. Available from: https://digitalcommons.usu.edu/etd/7285.

Council of Science Editors:

Chamberlain BL. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. [Masters Thesis]. Utah State University; 2018. Available from: https://digitalcommons.usu.edu/etd/7285


University of Illinois – Urbana-Champaign

7. Thomas, Robert E., II. Development and Testing of a Gallium Electromagnetic (GEM) Thruster.

Degree: PhD, 4048, 2011, University of Illinois – Urbana-Champaign

 An ablative, quasi-steady electromagnetic plasma accelerator is tested to quantify various characteristics of its operation. An array of diagnostics are used to characterize a gallium… (more)

Subjects/Keywords: Electric Propulsion: Plasma Diagnostics: Space Propulsion: Pulsed Power

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APA (6th Edition):

Thomas, Robert E., I. (2011). Development and Testing of a Gallium Electromagnetic (GEM) Thruster. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/18547

Chicago Manual of Style (16th Edition):

Thomas, Robert E., II. “Development and Testing of a Gallium Electromagnetic (GEM) Thruster.” 2011. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed May 08, 2021. http://hdl.handle.net/2142/18547.

MLA Handbook (7th Edition):

Thomas, Robert E., II. “Development and Testing of a Gallium Electromagnetic (GEM) Thruster.” 2011. Web. 08 May 2021.

Vancouver:

Thomas, Robert E. I. Development and Testing of a Gallium Electromagnetic (GEM) Thruster. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2011. [cited 2021 May 08]. Available from: http://hdl.handle.net/2142/18547.

Council of Science Editors:

Thomas, Robert E. I. Development and Testing of a Gallium Electromagnetic (GEM) Thruster. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/18547


Cal Poly

8. Sykes, Harrison G. COLD FLOW PERFORMANCE OF A RAMJET ENGINE.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  The design process and construction of the initial modular ramjet attachment to the Cal Poly supersonic wind tunnel is presented. The design of a… (more)

Subjects/Keywords: Propulsion; Supersonic; Ramjet; Performance; Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Sykes, H. G. (2014). COLD FLOW PERFORMANCE OF A RAMJET ENGINE. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182

Chicago Manual of Style (16th Edition):

Sykes, Harrison G. “COLD FLOW PERFORMANCE OF A RAMJET ENGINE.” 2014. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182.

MLA Handbook (7th Edition):

Sykes, Harrison G. “COLD FLOW PERFORMANCE OF A RAMJET ENGINE.” 2014. Web. 08 May 2021.

Vancouver:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182.

Council of Science Editors:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1334 ; 10.15368/theses.2014.182


Cal Poly

9. Powaser, Alexander M. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  Colloid thrusters, and electrospray thrusters as a whole, have been around since the 1960s. When they were first developed, the high efficiency and fine… (more)

Subjects/Keywords: electric propulsion; electrospray thruster; colloid thruster; electrostatic thruster; Propulsion and Power

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APA (6th Edition):

Powaser, A. M. (2019). Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39

Chicago Manual of Style (16th Edition):

Powaser, Alexander M. “Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.” 2019. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39.

MLA Handbook (7th Edition):

Powaser, Alexander M. “Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.” 2019. Web. 08 May 2021.

Vancouver:

Powaser AM. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39.

Council of Science Editors:

Powaser AM. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2079 ; 10.15368/theses.2019.39


Vanderbilt University

10. Turba, Ronald David. Design of a Nuclear Propulsion System for an Unmanned Aerial Vehicle.

Degree: MS, Mechanical Engineering, 2011, Vanderbilt University

 Much of today’s research in military assets is focused on remotely controlled designs and alternative energy. In this thesis, a modified design for a current… (more)

Subjects/Keywords: Propulsion; Nuclear Energy; Nuclear Power; Nuclear; UAV

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APA (6th Edition):

Turba, R. D. (2011). Design of a Nuclear Propulsion System for an Unmanned Aerial Vehicle. (Thesis). Vanderbilt University. Retrieved from http://hdl.handle.net/1803/10719

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Turba, Ronald David. “Design of a Nuclear Propulsion System for an Unmanned Aerial Vehicle.” 2011. Thesis, Vanderbilt University. Accessed May 08, 2021. http://hdl.handle.net/1803/10719.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Turba, Ronald David. “Design of a Nuclear Propulsion System for an Unmanned Aerial Vehicle.” 2011. Web. 08 May 2021.

Vancouver:

Turba RD. Design of a Nuclear Propulsion System for an Unmanned Aerial Vehicle. [Internet] [Thesis]. Vanderbilt University; 2011. [cited 2021 May 08]. Available from: http://hdl.handle.net/1803/10719.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Turba RD. Design of a Nuclear Propulsion System for an Unmanned Aerial Vehicle. [Thesis]. Vanderbilt University; 2011. Available from: http://hdl.handle.net/1803/10719

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Missouri University of Science and Technology

11. Spong, E. David. The numerical solution of two-dimensional fluid flow problems.

Degree: M.S. in Propulsion and Space Engineering, Propulsion and Space Engineering, Missouri University of Science and Technology

 "A numerical solution method is developed for the solution of two-dimensional, irrotational and compressible fluid flow problems. The partial differential equation, in terms of the… (more)

Subjects/Keywords: Propulsion and Power

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APA (6th Edition):

Spong, E. D. (n.d.). The numerical solution of two-dimensional fluid flow problems. (Masters Thesis). Missouri University of Science and Technology. Retrieved from https://scholarsmine.mst.edu/masters_theses/6814

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Chicago Manual of Style (16th Edition):

Spong, E David. “The numerical solution of two-dimensional fluid flow problems.” Masters Thesis, Missouri University of Science and Technology. Accessed May 08, 2021. https://scholarsmine.mst.edu/masters_theses/6814.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

MLA Handbook (7th Edition):

Spong, E David. “The numerical solution of two-dimensional fluid flow problems.” Web. 08 May 2021.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Spong ED. The numerical solution of two-dimensional fluid flow problems. [Internet] [Masters thesis]. Missouri University of Science and Technology; [cited 2021 May 08]. Available from: https://scholarsmine.mst.edu/masters_theses/6814.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Council of Science Editors:

Spong ED. The numerical solution of two-dimensional fluid flow problems. [Masters Thesis]. Missouri University of Science and Technology; Available from: https://scholarsmine.mst.edu/masters_theses/6814

Note: this citation may be lacking information needed for this citation format:
No year of publication.


Embry-Riddle Aeronautical University

12. Harvey, Megan Lewis. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters.

Degree: MSin Engineering Physics, Physical Sciences, 2014, Embry-Riddle Aeronautical University

  Electric propulsion engines, in particular Hall thrusters, provide the possibility of long-distance, low-cost space travel. The geometrical details of the Hall thrusters, especially the… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power; Space Vehicles

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APA (6th Edition):

Harvey, M. L. (2014). The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/160

Chicago Manual of Style (16th Edition):

Harvey, Megan Lewis. “The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/edt/160.

MLA Handbook (7th Edition):

Harvey, Megan Lewis. “The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters.” 2014. Web. 08 May 2021.

Vancouver:

Harvey ML. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2021 May 08]. Available from: https://commons.erau.edu/edt/160.

Council of Science Editors:

Harvey ML. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/160


Embry-Riddle Aeronautical University

13. Kapoor, Gaurav. Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2014, Embry-Riddle Aeronautical University

  The main purpose of this thesis is to conduct a parametric sensitivity study on the blade design of AOC 15/50 wind turbine based on… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Kapoor, G. (2014). Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/270

Chicago Manual of Style (16th Edition):

Kapoor, Gaurav. “Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade.” 2014. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/edt/270.

MLA Handbook (7th Edition):

Kapoor, Gaurav. “Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade.” 2014. Web. 08 May 2021.

Vancouver:

Kapoor G. Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2021 May 08]. Available from: https://commons.erau.edu/edt/270.

Council of Science Editors:

Kapoor G. Exploration of a Computational Fluid Dynamics Integrated Design Methodology for Potential Application to a Wind Turbine Blade. [Masters Thesis]. Embry-Riddle Aeronautical University; 2014. Available from: https://commons.erau.edu/edt/270


University of Tennessee – Knoxville

14. Conger, Scott Alexander. Physical Activity Assessment in Wheelchair Users.

Degree: 2011, University of Tennessee – Knoxville

 Purpose: To examine the relationship between hand rim propulsion power and energy expenditure during wheelchair locomotion. Methods: Fourteen individuals who used manual wheelchairs were included… (more)

Subjects/Keywords: energy expenditure; power; accelerometer; propulsion; Sports Sciences

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APA (6th Edition):

Conger, S. A. (2011). Physical Activity Assessment in Wheelchair Users. (Doctoral Dissertation). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_graddiss/1069

Chicago Manual of Style (16th Edition):

Conger, Scott Alexander. “Physical Activity Assessment in Wheelchair Users.” 2011. Doctoral Dissertation, University of Tennessee – Knoxville. Accessed May 08, 2021. https://trace.tennessee.edu/utk_graddiss/1069.

MLA Handbook (7th Edition):

Conger, Scott Alexander. “Physical Activity Assessment in Wheelchair Users.” 2011. Web. 08 May 2021.

Vancouver:

Conger SA. Physical Activity Assessment in Wheelchair Users. [Internet] [Doctoral dissertation]. University of Tennessee – Knoxville; 2011. [cited 2021 May 08]. Available from: https://trace.tennessee.edu/utk_graddiss/1069.

Council of Science Editors:

Conger SA. Physical Activity Assessment in Wheelchair Users. [Doctoral Dissertation]. University of Tennessee – Knoxville; 2011. Available from: https://trace.tennessee.edu/utk_graddiss/1069


University of Tennessee – Knoxville

15. Quigley, John Nicholas. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection.

Degree: MS, Aerospace Engineering, 2014, University of Tennessee – Knoxville

  The current study focused on two innovations intended to reduce the cost and enhance the performance of hybrid rockets. The majority of the emphasis… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Quigley, J. N. (2014). Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2843

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Quigley, John Nicholas. “Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection.” 2014. Thesis, University of Tennessee – Knoxville. Accessed May 08, 2021. https://trace.tennessee.edu/utk_gradthes/2843.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Quigley, John Nicholas. “Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection.” 2014. Web. 08 May 2021.

Vancouver:

Quigley JN. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2021 May 08]. Available from: https://trace.tennessee.edu/utk_gradthes/2843.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Quigley JN. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. [Thesis]. University of Tennessee – Knoxville; 2014. Available from: https://trace.tennessee.edu/utk_gradthes/2843

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

16. Chikelu, Jennifer Onyinye. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.

Degree: MS, Mechanical Engineering, 2018, South Dakota State University

  Computational fluid dynamics tool has been employed in the past to determine and analyze efficiency or performance in combustion engines and for combustion analysis.… (more)

Subjects/Keywords: Energy Systems; Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Chikelu, J. O. (2018). Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. (Masters Thesis). South Dakota State University. Retrieved from https://openprairie.sdstate.edu/etd/2953

Chicago Manual of Style (16th Edition):

Chikelu, Jennifer Onyinye. “Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.” 2018. Masters Thesis, South Dakota State University. Accessed May 08, 2021. https://openprairie.sdstate.edu/etd/2953.

MLA Handbook (7th Edition):

Chikelu, Jennifer Onyinye. “Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.” 2018. Web. 08 May 2021.

Vancouver:

Chikelu JO. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. [Internet] [Masters thesis]. South Dakota State University; 2018. [cited 2021 May 08]. Available from: https://openprairie.sdstate.edu/etd/2953.

Council of Science Editors:

Chikelu JO. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. [Masters Thesis]. South Dakota State University; 2018. Available from: https://openprairie.sdstate.edu/etd/2953


Cal Poly

17. Barlog, Christopher M. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster.

Degree: MS, Aerospace Engineering, 2015, Cal Poly

  High Efficiency Multistage Plasma Thrusters (HEMPTs) are a relatively new form of electric propulsion that show promise for use on a variety of missions… (more)

Subjects/Keywords: HEMPT; EP; Electric Propulsion; Magnetic Field; Thruster; Hall Thruster; Ion Thruster; Propulsion and Power

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APA (6th Edition):

Barlog, C. M. (2015). Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179

Chicago Manual of Style (16th Edition):

Barlog, Christopher M. “Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster.” 2015. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179.

MLA Handbook (7th Edition):

Barlog, Christopher M. “Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster.” 2015. Web. 08 May 2021.

Vancouver:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179.

Council of Science Editors:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Masters Thesis]. Cal Poly; 2015. Available from: https://digitalcommons.calpoly.edu/theses/1530 ; 10.15368/theses.2015.179

18. Baris, Engin. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.

Degree: MS, Mechanical & Aerospace Engineering, 2017, Old Dominion University

  Distributed electric propulsion systems benefit from the inherent scale independence of electric propulsion. This property allows the designer to place multiple small electric motors… (more)

Subjects/Keywords: Design of experiments; Distributed; Electric; Low Reynolds; Propulsion; Small UAV; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Baris, E. (2017). An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. (Thesis). Old Dominion University. Retrieved from 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Baris, Engin. “An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.” 2017. Thesis, Old Dominion University. Accessed May 08, 2021. 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Baris, Engin. “An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.” 2017. Web. 08 May 2021.

Vancouver:

Baris E. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. [Internet] [Thesis]. Old Dominion University; 2017. [cited 2021 May 08]. Available from: 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Baris E. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. [Thesis]. Old Dominion University; 2017. Available from: 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Michigan Technological University

19. Jackson, Brandon. Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability.

Degree: PhD, Department of Mechanical Engineering-Engineering Mechanics, 2018, Michigan Technological University

  This dissertation presents three studies on the electrospray of ionic liquid ferrofluid. Ionic liquid ferrofluids are electrically conductive super-paramagnetic fluids which respond strongly in… (more)

Subjects/Keywords: ferrofluid; electrospray; ionic liquid; electric satellite propulsion; ferromagnetisim; Other Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Jackson, B. (2018). Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability. (Doctoral Dissertation). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etdr/587

Chicago Manual of Style (16th Edition):

Jackson, Brandon. “Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability.” 2018. Doctoral Dissertation, Michigan Technological University. Accessed May 08, 2021. https://digitalcommons.mtu.edu/etdr/587.

MLA Handbook (7th Edition):

Jackson, Brandon. “Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability.” 2018. Web. 08 May 2021.

Vancouver:

Jackson B. Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability. [Internet] [Doctoral dissertation]. Michigan Technological University; 2018. [cited 2021 May 08]. Available from: https://digitalcommons.mtu.edu/etdr/587.

Council of Science Editors:

Jackson B. Meniscus Modeling and Emission Studies of an Ionic Liquid Ferrofluid Electrospray Source Emitting from a Magneto-Electric Instability. [Doctoral Dissertation]. Michigan Technological University; 2018. Available from: https://digitalcommons.mtu.edu/etdr/587


Cal Poly

20. Howe, William Beaman. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES.

Degree: MS, Aerospace Engineering, 2015, Cal Poly

  A method for sizing remotely powered unmanned aerial vehicles is presented to augment the conventional design process. This method allows for unconventionally powered aircraft… (more)

Subjects/Keywords: UAV; wireless; power; design; Aeronautical Vehicles; Propulsion and Power

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APA (6th Edition):

Howe, W. B. (2015). DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27

Chicago Manual of Style (16th Edition):

Howe, William Beaman. “DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES.” 2015. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27.

MLA Handbook (7th Edition):

Howe, William Beaman. “DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES.” 2015. Web. 08 May 2021.

Vancouver:

Howe WB. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27.

Council of Science Editors:

Howe WB. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. [Masters Thesis]. Cal Poly; 2015. Available from: https://digitalcommons.calpoly.edu/theses/1386 ; 10.15368/theses.2015.27

21. Grimaud, Lou. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.

Degree: Docteur es, Physique, 2018, Université d'Orléans

Les propulseurs de Hall sont l’une des techniques de propulsion fusée par plasma les plus utilisés. Ils possèdent une impulsion spécifique moyenne et un haut… (more)

Subjects/Keywords: Propulsion spatiale electrique; Propulsion par plasma; Propulseur de Hall; Écrantage magnétique; Electric space propulsion; Plasma propulsion; Hall thruster; Magnetic shielding; Laser induced fluorescence; Alternative materials; Low power; 621.46

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APA (6th Edition):

Grimaud, L. (2018). Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. (Doctoral Dissertation). Université d'Orléans. Retrieved from http://www.theses.fr/2018ORLE2046

Chicago Manual of Style (16th Edition):

Grimaud, Lou. “Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.” 2018. Doctoral Dissertation, Université d'Orléans. Accessed May 08, 2021. http://www.theses.fr/2018ORLE2046.

MLA Handbook (7th Edition):

Grimaud, Lou. “Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance.” 2018. Web. 08 May 2021.

Vancouver:

Grimaud L. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. [Internet] [Doctoral dissertation]. Université d'Orléans; 2018. [cited 2021 May 08]. Available from: http://www.theses.fr/2018ORLE2046.

Council of Science Editors:

Grimaud L. Magnetic shielding topology applied to low power Hall thrusters : Topologie d’écrantage magnétique appliquée aux moteurs de Hall faible puissance. [Doctoral Dissertation]. Université d'Orléans; 2018. Available from: http://www.theses.fr/2018ORLE2046


Ryerson University

22. Hayek, Daniel. Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion.

Degree: 2010, Ryerson University

 Laser propulsion is a relatively new technology being researched for its vast potential. A test apparatus was developed to measure small forces using piezoelectric films… (more)

Subjects/Keywords: Laser ablation; Laser ablation  – Testing; Propulsion systems; High power lasers; Lasers

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APA (6th Edition):

Hayek, D. (2010). Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1755

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Hayek, Daniel. “Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion.” 2010. Thesis, Ryerson University. Accessed May 08, 2021. https://digital.library.ryerson.ca/islandora/object/RULA%3A1755.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Hayek, Daniel. “Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion.” 2010. Web. 08 May 2021.

Vancouver:

Hayek D. Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion. [Internet] [Thesis]. Ryerson University; 2010. [cited 2021 May 08]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1755.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hayek D. Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion. [Thesis]. Ryerson University; 2010. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1755

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

23. Svatos, Adam Ladislav. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.

Degree: 2017, University of Toronto

This thesis describes the author's contributions to three separate projects. The bus of the NORSAT-2 satellite was developed by the Space Flight Laboratory (SFL) for… (more)

Subjects/Keywords: electronic; Hall effect; power; propulsion; space; thruster; 0538

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APA (6th Edition):

Svatos, A. L. (2017). Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79053

Chicago Manual of Style (16th Edition):

Svatos, Adam Ladislav. “Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.” 2017. Masters Thesis, University of Toronto. Accessed May 08, 2021. http://hdl.handle.net/1807/79053.

MLA Handbook (7th Edition):

Svatos, Adam Ladislav. “Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer.” 2017. Web. 08 May 2021.

Vancouver:

Svatos AL. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2021 May 08]. Available from: http://hdl.handle.net/1807/79053.

Council of Science Editors:

Svatos AL. Design, assembly, integration, and testing of a power processing unit for a cylindrical Hall thruster, the NORSAT-2 flatsat, and the Vector Gravimeter for Asteroids instrument computer. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79053


Embry-Riddle Aeronautical University

24. Ho, Joon Fui. The Static Thrust Characterization of the Quatra Aerrow Q100XL Engine for Flight Performance Prediction of the 1/3-scaled Cessna 172P Model.

Degree: Master of Aerospace Engineering, Aerospace Engineering, 2000, Embry-Riddle Aeronautical University

  The purpose of this research is to predict the thrust as a function of forward flight velocity required for the one-third-scaled Cessna 172P. This… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Ho, J. F. (2000). The Static Thrust Characterization of the Quatra Aerrow Q100XL Engine for Flight Performance Prediction of the 1/3-scaled Cessna 172P Model. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/84

Chicago Manual of Style (16th Edition):

Ho, Joon Fui. “The Static Thrust Characterization of the Quatra Aerrow Q100XL Engine for Flight Performance Prediction of the 1/3-scaled Cessna 172P Model.” 2000. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/db-theses/84.

MLA Handbook (7th Edition):

Ho, Joon Fui. “The Static Thrust Characterization of the Quatra Aerrow Q100XL Engine for Flight Performance Prediction of the 1/3-scaled Cessna 172P Model.” 2000. Web. 08 May 2021.

Vancouver:

Ho JF. The Static Thrust Characterization of the Quatra Aerrow Q100XL Engine for Flight Performance Prediction of the 1/3-scaled Cessna 172P Model. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2000. [cited 2021 May 08]. Available from: https://commons.erau.edu/db-theses/84.

Council of Science Editors:

Ho JF. The Static Thrust Characterization of the Quatra Aerrow Q100XL Engine for Flight Performance Prediction of the 1/3-scaled Cessna 172P Model. [Masters Thesis]. Embry-Riddle Aeronautical University; 2000. Available from: https://commons.erau.edu/db-theses/84


Embry-Riddle Aeronautical University

25. Kaplan, Brian J. The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 1996, Embry-Riddle Aeronautical University

  In order to provide a means for testing noise reduction techniques in propellers and fans, a low-speed, low-turbulence, anechoic wind tunnel was designed, fabricated… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Kaplan, B. J. (1996). The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/91

Chicago Manual of Style (16th Edition):

Kaplan, Brian J. “The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel.” 1996. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/db-theses/91.

MLA Handbook (7th Edition):

Kaplan, Brian J. “The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel.” 1996. Web. 08 May 2021.

Vancouver:

Kaplan BJ. The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 1996. [cited 2021 May 08]. Available from: https://commons.erau.edu/db-theses/91.

Council of Science Editors:

Kaplan BJ. The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel. [Masters Thesis]. Embry-Riddle Aeronautical University; 1996. Available from: https://commons.erau.edu/db-theses/91


Embry-Riddle Aeronautical University

26. De Angelo, Bianca A. Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles.

Degree: MSin Aerospace Engineering, Graduate Studies, 2016, Embry-Riddle Aeronautical University

  Jet impingement cooling is an internal cooling configuration used in the thermal management of temperature sensitive systems. With rocket engine combustion temperatures rising as… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

De Angelo, B. A. (2016). Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/206

Chicago Manual of Style (16th Edition):

De Angelo, Bianca A. “Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles.” 2016. Masters Thesis, Embry-Riddle Aeronautical University. Accessed May 08, 2021. https://commons.erau.edu/edt/206.

MLA Handbook (7th Edition):

De Angelo, Bianca A. “Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles.” 2016. Web. 08 May 2021.

Vancouver:

De Angelo BA. Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2021 May 08]. Available from: https://commons.erau.edu/edt/206.

Council of Science Editors:

De Angelo BA. Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles. [Masters Thesis]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/206


Delft University of Technology

27. Ang, A.W.X. (author). Hybrid Electric Propulsion Systems: Integrated performance analysis applied on short-range aircraft.

Degree: 2016, Delft University of Technology

The growing level of environmental implications of aviation and a significant increase in air traffic have been driving technological advancements in the aerospace industry. The… (more)

Subjects/Keywords: power management strategy; performance sizing; Hybrid Electric Propulsion System; HEPS

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APA (6th Edition):

Ang, A. W. X. (. (2016). Hybrid Electric Propulsion Systems: Integrated performance analysis applied on short-range aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5148aafa-91ed-485d-ac7a-2883394ec0a4

Chicago Manual of Style (16th Edition):

Ang, A W X (author). “Hybrid Electric Propulsion Systems: Integrated performance analysis applied on short-range aircraft.” 2016. Masters Thesis, Delft University of Technology. Accessed May 08, 2021. http://resolver.tudelft.nl/uuid:5148aafa-91ed-485d-ac7a-2883394ec0a4.

MLA Handbook (7th Edition):

Ang, A W X (author). “Hybrid Electric Propulsion Systems: Integrated performance analysis applied on short-range aircraft.” 2016. Web. 08 May 2021.

Vancouver:

Ang AWX(. Hybrid Electric Propulsion Systems: Integrated performance analysis applied on short-range aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 May 08]. Available from: http://resolver.tudelft.nl/uuid:5148aafa-91ed-485d-ac7a-2883394ec0a4.

Council of Science Editors:

Ang AWX(. Hybrid Electric Propulsion Systems: Integrated performance analysis applied on short-range aircraft. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:5148aafa-91ed-485d-ac7a-2883394ec0a4


Michigan Technological University

28. Slabaugh, Tristan. Cathode Coupling in a Low Power Hall Effect Thruster.

Degree: MS, Department of Mechanical Engineering-Engineering Mechanics, 2019, Michigan Technological University

  This work explores the effects of cathode position on Orbion Space Technology’s Aurora thruster performance and ignition characteristics. The cathode was moved to points… (more)

Subjects/Keywords: Hall effect thruster; Cathode Coupling; Propulsion and Power

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APA (6th Edition):

Slabaugh, T. (2019). Cathode Coupling in a Low Power Hall Effect Thruster. (Masters Thesis). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etdr/886

Chicago Manual of Style (16th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Masters Thesis, Michigan Technological University. Accessed May 08, 2021. https://digitalcommons.mtu.edu/etdr/886.

MLA Handbook (7th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Web. 08 May 2021.

Vancouver:

Slabaugh T. Cathode Coupling in a Low Power Hall Effect Thruster. [Internet] [Masters thesis]. Michigan Technological University; 2019. [cited 2021 May 08]. Available from: https://digitalcommons.mtu.edu/etdr/886.

Council of Science Editors:

Slabaugh T. Cathode Coupling in a Low Power Hall Effect Thruster. [Masters Thesis]. Michigan Technological University; 2019. Available from: https://digitalcommons.mtu.edu/etdr/886


University of Tasmania

29. Shagar, V. Transient suppression in hybrid electric ship power systems.

Degree: 2019, University of Tasmania

 The requirements for power quality in ship power systems have been increasing over the years. This is an essential consequence of improving the efficiency of… (more)

Subjects/Keywords: Power systems; electrical transients; energy storage; hybrid propulsion

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APA (6th Edition):

Shagar, V. (2019). Transient suppression in hybrid electric ship power systems. (Thesis). University of Tasmania. Retrieved from https://eprints.utas.edu.au/31901/1/Shagar_whole_thesis.pdf ; Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Shagar, V. “Transient suppression in hybrid electric ship power systems.” 2019. Thesis, University of Tasmania. Accessed May 08, 2021. https://eprints.utas.edu.au/31901/1/Shagar_whole_thesis.pdf ; Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania..

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Shagar, V. “Transient suppression in hybrid electric ship power systems.” 2019. Web. 08 May 2021.

Vancouver:

Shagar V. Transient suppression in hybrid electric ship power systems. [Internet] [Thesis]. University of Tasmania; 2019. [cited 2021 May 08]. Available from: https://eprints.utas.edu.au/31901/1/Shagar_whole_thesis.pdf ; Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania..

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Shagar V. Transient suppression in hybrid electric ship power systems. [Thesis]. University of Tasmania; 2019. Available from: https://eprints.utas.edu.au/31901/1/Shagar_whole_thesis.pdf ; Shagar, V ORCID: 0000-0001-7933-0958 <https://orcid.org/0000-0001-7933-0958> 2019 , 'Transient suppression in hybrid electric ship power systems', PhD thesis, University of Tasmania.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Cal Poly

30. Bughman, Luke J. Modeling and Testing Powerplant Subsystems of a Solar UAS.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  In order to accurately conduct the preliminary and detailed design of solar powered Unmanned Aerial Systems (UAS), it is necessary to have a thorough… (more)

Subjects/Keywords: Solar; UAS; Powerplant; Modeling; Testing; Aeronautical Vehicles; Propulsion and Power

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

APA (6th Edition):

Bughman, L. J. (2019). Modeling and Testing Powerplant Subsystems of a Solar UAS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98

Chicago Manual of Style (16th Edition):

Bughman, Luke J. “Modeling and Testing Powerplant Subsystems of a Solar UAS.” 2019. Masters Thesis, Cal Poly. Accessed May 08, 2021. https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98.

MLA Handbook (7th Edition):

Bughman, Luke J. “Modeling and Testing Powerplant Subsystems of a Solar UAS.” 2019. Web. 08 May 2021.

Vancouver:

Bughman LJ. Modeling and Testing Powerplant Subsystems of a Solar UAS. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2021 May 08]. Available from: https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98.

Council of Science Editors:

Bughman LJ. Modeling and Testing Powerplant Subsystems of a Solar UAS. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2082 ; 10.15368/theses.2019.98

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