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You searched for subject:(Propulsion AND Power). Showing records 1 – 30 of 137 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2019 Dec 06]. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Green MW. HAPSS, Hybrid Aircraft Propulsion System Synthesis. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Dec 06]. 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 December 06, 2019. 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. 06 Dec 2019.

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 2019 Dec 06]. 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. Croteau, Tyler J. MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  With an increased demand in Cube Satellite (CubeSat) development for low cost science and exploration missions, a push for the development of micro-propulsion technology… (more)

Subjects/Keywords: Propulsion; Electric Propulsion; Plasma; CubeSat; CFD; Nozzle; Propulsion and Power

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APA (6th Edition):

Croteau, T. J. (2018). MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1961

Chicago Manual of Style (16th Edition):

Croteau, Tyler J. “MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER.” 2018. Masters Thesis, Cal Poly. Accessed December 06, 2019. https://digitalcommons.calpoly.edu/theses/1961.

MLA Handbook (7th Edition):

Croteau, Tyler J. “MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER.” 2018. Web. 06 Dec 2019.

Vancouver:

Croteau TJ. MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/1961.

Council of Science Editors:

Croteau TJ. MICRO-NOZZLE SIMULATION AND TEST FOR AN ELECTROTHERMAL PLASMA THRUSTER. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1961


Cal Poly

5. 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

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 December 06, 2019. https://digitalcommons.calpoly.edu/theses/2064.

MLA Handbook (7th Edition):

McGehee, Will Alan. “Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform.” 2019. Web. 06 Dec 2019.

Vancouver:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/2064.

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


Embry-Riddle Aeronautical University

6. 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 http://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 December 06, 2019. http://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. 06 Dec 2019.

Vancouver:

Espa˜na-Heredia LEF. Investigation of Pulse Detonation Engine Flow Conditions for Turbomachinery Integration. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2019 Dec 06]. Available from: http://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: http://commons.erau.edu/edt/158


Utah State University

7. 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 December 06, 2019. https://digitalcommons.usu.edu/etd/7285.

MLA Handbook (7th Edition):

Chamberlain, Britany L. “Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.” 2018. Web. 06 Dec 2019.

Vancouver:

Chamberlain BL. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2019 Dec 06]. 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

8. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Thomas, Robert E. I. Development and Testing of a Gallium Electromagnetic (GEM) Thruster. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2011. [cited 2019 Dec 06]. 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

9. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Sykes HG. COLD FLOW PERFORMANCE OF A RAMJET ENGINE. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Dec 06]. 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

10. 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

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 December 06, 2019. https://digitalcommons.calpoly.edu/theses/2079.

MLA Handbook (7th Edition):

Powaser, Alexander M. “Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students.” 2019. Web. 06 Dec 2019.

Vancouver:

Powaser AM. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/2079.

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


Embry-Riddle Aeronautical University

11. 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 http://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 December 06, 2019. http://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. 06 Dec 2019.

Vancouver:

Harvey ML. The Effect of the 2-Dimensional Magnetic Field Profile in Hall Thrusters. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2014. [cited 2019 Dec 06]. Available from: http://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: http://commons.erau.edu/edt/160


Embry-Riddle Aeronautical University

12. 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 http://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 December 06, 2019. http://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. 06 Dec 2019.

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 2019 Dec 06]. Available from: http://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: http://commons.erau.edu/edt/270


University of Tennessee – Knoxville

13. 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 December 06, 2019. https://trace.tennessee.edu/utk_graddiss/1069.

MLA Handbook (7th Edition):

Conger, Scott Alexander. “Physical Activity Assessment in Wheelchair Users.” 2011. Web. 06 Dec 2019.

Vancouver:

Conger SA. Physical Activity Assessment in Wheelchair Users. [Internet] [Doctoral dissertation]. University of Tennessee – Knoxville; 2011. [cited 2019 Dec 06]. 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

14. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Quigley JN. Hybrid Rocket Design Study Utilizing Nozzle Cooling and Aft-End Vortex Oxidizer Injection. [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2019 Dec 06]. 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


Missouri University of Science and Technology

15. 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 http://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 December 06, 2019. http://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. 06 Dec 2019.

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 2019 Dec 06]. Available from: http://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: http://scholarsmine.mst.edu/masters_theses/6814

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

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 December 06, 2019. https://openprairie.sdstate.edu/etd/2953.

MLA Handbook (7th Edition):

Chikelu, Jennifer Onyinye. “Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.” 2018. Web. 06 Dec 2019.

Vancouver:

Chikelu JO. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. [Internet] [Masters thesis]. South Dakota State University; 2018. [cited 2019 Dec 06]. 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


Michigan Technological University

17. 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 http://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 December 06, 2019. http://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. 06 Dec 2019.

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 2019 Dec 06]. Available from: http://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: http://digitalcommons.mtu.edu/etdr/587

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 December 06, 2019. 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. 06 Dec 2019.

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 2019 Dec 06]. 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


Cal Poly

19. Younger, Coleman Thomas. THERMAL MODELS FOR A 3 CM MINIATURE XENON ION THRUSTER.

Degree: MS, Aerospace Engineering, 2010, Cal Poly

 In order to support UCLA’s development of the 3 cm Miniature Xenon Ion (MiXI) thruster, Cal Poly has a 3 cm thruster under development. This… (more)

Subjects/Keywords: electric propulsion; thermal modeling; micromachining; cathode; thruster; precision orbit control; Propulsion and Power

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APA (6th Edition):

Younger, C. T. (2010). THERMAL MODELS FOR A 3 CM MINIATURE XENON ION THRUSTER. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/413 ; 10.15368/theses.2010.177

Chicago Manual of Style (16th Edition):

Younger, Coleman Thomas. “THERMAL MODELS FOR A 3 CM MINIATURE XENON ION THRUSTER.” 2010. Masters Thesis, Cal Poly. Accessed December 06, 2019. https://digitalcommons.calpoly.edu/theses/413 ; 10.15368/theses.2010.177.

MLA Handbook (7th Edition):

Younger, Coleman Thomas. “THERMAL MODELS FOR A 3 CM MINIATURE XENON ION THRUSTER.” 2010. Web. 06 Dec 2019.

Vancouver:

Younger CT. THERMAL MODELS FOR A 3 CM MINIATURE XENON ION THRUSTER. [Internet] [Masters thesis]. Cal Poly; 2010. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/413 ; 10.15368/theses.2010.177.

Council of Science Editors:

Younger CT. THERMAL MODELS FOR A 3 CM MINIATURE XENON ION THRUSTER. [Masters Thesis]. Cal Poly; 2010. Available from: https://digitalcommons.calpoly.edu/theses/413 ; 10.15368/theses.2010.177


Cal Poly

20. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2019 Dec 06]. 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


Cal Poly

21. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Howe WB. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2019 Dec 06]. 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


Syracuse University

22. Welles, Andrew Voss. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft.

Degree: PhD, Mechanical and Aerospace Engineering, 2018, Syracuse University

  This research effort explores the interactions between aerodynamics and hybridelectric power system (HEPS) design and control for vertical takeoff and landing (VTOL) aircraft applications.… (more)

Subjects/Keywords: hybrid power; nonlinear control; power systems; Propulsion; transitional flight; VTOL; Engineering

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APA (6th Edition):

Welles, A. V. (2018). Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. (Doctoral Dissertation). Syracuse University. Retrieved from https://surface.syr.edu/etd/943

Chicago Manual of Style (16th Edition):

Welles, Andrew Voss. “Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft.” 2018. Doctoral Dissertation, Syracuse University. Accessed December 06, 2019. https://surface.syr.edu/etd/943.

MLA Handbook (7th Edition):

Welles, Andrew Voss. “Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft.” 2018. Web. 06 Dec 2019.

Vancouver:

Welles AV. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. [Internet] [Doctoral dissertation]. Syracuse University; 2018. [cited 2019 Dec 06]. Available from: https://surface.syr.edu/etd/943.

Council of Science Editors:

Welles AV. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. [Doctoral Dissertation]. Syracuse University; 2018. Available from: https://surface.syr.edu/etd/943

23. 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 December 06, 2019. 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. 06 Dec 2019.

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 2019 Dec 06]. 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


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 http://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 December 06, 2019. http://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. 06 Dec 2019.

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 2019 Dec 06]. Available from: http://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: http://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 http://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 December 06, 2019. http://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. 06 Dec 2019.

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 2019 Dec 06]. Available from: http://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: http://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 http://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 December 06, 2019. http://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. 06 Dec 2019.

Vancouver:

De Angelo BA. Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2019 Dec 06]. Available from: http://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: http://commons.erau.edu/edt/206


Ryerson University

27. 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 December 06, 2019. 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. 06 Dec 2019.

Vancouver:

Hayek D. Using A High Repetition Rate Nd: YAG Laser For Pulsed Laser Ablation Propulsion. [Internet] [Thesis]. Ryerson University; 2010. [cited 2019 Dec 06]. 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

28. Popish, Martin Roy. Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket.

Degree: MS, Aerospace Engineering, 2012, Cal Poly

  Experiments were conducted on the Cal Poly air augmented rocket (AAR) in order to characterize two-dimensional flowfield phenomenon occurring in the mixing duct. The… (more)

Subjects/Keywords: Propulsion and Power

power. Figure 1-1 below shows the potential of both the TBCC and RBCC propulsion systems, and… …integrated hypersonic vehicle. The focus of this thesis is on the propulsion systems of the… …built to cruise for a short time at hypersonic speeds using a Scramjet propulsion system2. The… …100psi source as well as a power source. During testing, the valve was controlled via its… 

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APA (6th Edition):

Popish, M. R. (2012). Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/766 ; 10.15368/theses.2012.52

Chicago Manual of Style (16th Edition):

Popish, Martin Roy. “Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket.” 2012. Masters Thesis, Cal Poly. Accessed December 06, 2019. https://digitalcommons.calpoly.edu/theses/766 ; 10.15368/theses.2012.52.

MLA Handbook (7th Edition):

Popish, Martin Roy. “Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket.” 2012. Web. 06 Dec 2019.

Vancouver:

Popish MR. Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket. [Internet] [Masters thesis]. Cal Poly; 2012. [cited 2019 Dec 06]. Available from: https://digitalcommons.calpoly.edu/theses/766 ; 10.15368/theses.2012.52.

Council of Science Editors:

Popish MR. Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket. [Masters Thesis]. Cal Poly; 2012. Available from: https://digitalcommons.calpoly.edu/theses/766 ; 10.15368/theses.2012.52

29. Mbithi, Florence M. Design and Evaluation of a Propulsion System for Small, Compact, Low-speed Maneuvering Underwater Vehicles.

Degree: MS, Mechatronics Systems Engineering, 2014, U of Denver

  Underwater vehicles used to perform precision inspection and non-destructive evaluation in tightly constrained or delicate underwater environments must be small, have low-speed maneuverability and… (more)

Subjects/Keywords: Electrical and Computer Engineering; Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Mbithi, F. M. (2014). Design and Evaluation of a Propulsion System for Small, Compact, Low-speed Maneuvering Underwater Vehicles. (Thesis). U of Denver. Retrieved from https://digitalcommons.du.edu/etd/414

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):

Mbithi, Florence M. “Design and Evaluation of a Propulsion System for Small, Compact, Low-speed Maneuvering Underwater Vehicles.” 2014. Thesis, U of Denver. Accessed December 06, 2019. https://digitalcommons.du.edu/etd/414.

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

MLA Handbook (7th Edition):

Mbithi, Florence M. “Design and Evaluation of a Propulsion System for Small, Compact, Low-speed Maneuvering Underwater Vehicles.” 2014. Web. 06 Dec 2019.

Vancouver:

Mbithi FM. Design and Evaluation of a Propulsion System for Small, Compact, Low-speed Maneuvering Underwater Vehicles. [Internet] [Thesis]. U of Denver; 2014. [cited 2019 Dec 06]. Available from: https://digitalcommons.du.edu/etd/414.

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

Council of Science Editors:

Mbithi FM. Design and Evaluation of a Propulsion System for Small, Compact, Low-speed Maneuvering Underwater Vehicles. [Thesis]. U of Denver; 2014. Available from: https://digitalcommons.du.edu/etd/414

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


University of Tennessee – Knoxville

30. Hutchings, Rick. Effects of Supercooled Water Ingestion on Engine Performance.

Degree: MS, Mechanical Engineering, 2011, University of Tennessee – Knoxville

  An aircraft will encounter freezing rain, snow, and ice during ground operation and flight. In cold conditions, ice may form on th einlet and… (more)

Subjects/Keywords: Engine; Performance; Icing; Other Mechanical Engineering; Propulsion and Power

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

APA (6th Edition):

Hutchings, R. (2011). Effects of Supercooled Water Ingestion on Engine Performance. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/981

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):

Hutchings, Rick. “Effects of Supercooled Water Ingestion on Engine Performance.” 2011. Thesis, University of Tennessee – Knoxville. Accessed December 06, 2019. https://trace.tennessee.edu/utk_gradthes/981.

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

MLA Handbook (7th Edition):

Hutchings, Rick. “Effects of Supercooled Water Ingestion on Engine Performance.” 2011. Web. 06 Dec 2019.

Vancouver:

Hutchings R. Effects of Supercooled Water Ingestion on Engine Performance. [Internet] [Thesis]. University of Tennessee – Knoxville; 2011. [cited 2019 Dec 06]. Available from: https://trace.tennessee.edu/utk_gradthes/981.

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

Council of Science Editors:

Hutchings R. Effects of Supercooled Water Ingestion on Engine Performance. [Thesis]. University of Tennessee – Knoxville; 2011. Available from: https://trace.tennessee.edu/utk_gradthes/981

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

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