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Dates: 2015 – 2019

You searched for subject:(Propulsion AND Power). Showing records 1 – 30 of 49 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Yeung TH. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2019. [cited 2020 Jan 18]. 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. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

McGehee WA. Design Principles and Preliminary Testing of a Micropropulsion Electrospray Thruster Research Platform. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 18]. 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


Utah State University

3. 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 January 18, 2020. https://digitalcommons.usu.edu/etd/7285.

MLA Handbook (7th Edition):

Chamberlain, Britany L. “Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion.” 2018. Web. 18 Jan 2020.

Vancouver:

Chamberlain BL. Additively-Manufactured Hybrid Rocket Consumable Structure for CubeSat Propulsion. [Internet] [Masters thesis]. Utah State University; 2018. [cited 2020 Jan 18]. 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


Cal Poly

4. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Powaser AM. Colloid Thruster to Teach Advance Electric Propulsion Techniques to Post-Secondary Students. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 18]. 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

5. 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 January 18, 2020. https://openprairie.sdstate.edu/etd/2953.

MLA Handbook (7th Edition):

Chikelu, Jennifer Onyinye. “Simulation of Non-premixed Ethylene-air Crossflow Jet Flame.” 2018. Web. 18 Jan 2020.

Vancouver:

Chikelu JO. Simulation of Non-premixed Ethylene-air Crossflow Jet Flame. [Internet] [Masters thesis]. South Dakota State University; 2018. [cited 2020 Jan 18]. 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

6. 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 January 18, 2020. 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. 18 Jan 2020.

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 2020 Jan 18]. 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


Cal Poly

7. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Barlog CM. Divergent Plume Reduction of a High-Efficiency Multistage Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2020 Jan 18]. 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

8. 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 January 18, 2020. 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. 18 Jan 2020.

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 2020 Jan 18]. 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

9. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Howe WB. DESIGN METHODS FOR REMOTELY POWERED UNMANNED AERIAL VEHICLES. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2020 Jan 18]. 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

10. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Welles AV. Hybrid Electric Distributed Propulsion for Vertical Takeoff and Landing Aircraft. [Internet] [Doctoral dissertation]. Syracuse University; 2018. [cited 2020 Jan 18]. 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

11. 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 January 18, 2020. 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. 18 Jan 2020.

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 2020 Jan 18]. 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


University of Tasmania

12. 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 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Shagar V. Transient suppression in hybrid electric ship power systems. [Internet] [Thesis]. University of Tasmania; 2019. [cited 2020 Jan 18]. Available from: 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: 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


Embry-Riddle Aeronautical University

13. 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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

De Angelo BA. Computational Investigation of Impingement Cooling for Regeneratively Cooled Rocket Nozzles. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2016. [cited 2020 Jan 18]. 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


Cal Poly

14. 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 (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 January 18, 2020. 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. 18 Jan 2020.

Vancouver:

Bughman LJ. Modeling and Testing Powerplant Subsystems of a Solar UAS. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 18]. 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


Cal Poly

15. King, Harrison Raymond. Electrode Geometry Effects in an Electrothermal Plasma Microthruster.

Degree: MS, Aerospace Engineering, 2018, Cal Poly

  Nanosatellites, such as Cubesats, are a rapidly growing sector of the space industry. Their popularity stems from their low development cost, short development cycle,… (more)

Subjects/Keywords: Pocket Rocket; capacitive; cubesat; secondary electron; ionization; argon; Propulsion and Power

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APA (6th Edition):

King, H. R. (2018). Electrode Geometry Effects in an Electrothermal Plasma Microthruster. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73

Chicago Manual of Style (16th Edition):

King, Harrison Raymond. “Electrode Geometry Effects in an Electrothermal Plasma Microthruster.” 2018. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73.

MLA Handbook (7th Edition):

King, Harrison Raymond. “Electrode Geometry Effects in an Electrothermal Plasma Microthruster.” 2018. Web. 18 Jan 2020.

Vancouver:

King HR. Electrode Geometry Effects in an Electrothermal Plasma Microthruster. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73.

Council of Science Editors:

King HR. Electrode Geometry Effects in an Electrothermal Plasma Microthruster. [Masters Thesis]. Cal Poly; 2018. Available from: https://digitalcommons.calpoly.edu/theses/1899 ; 10.15368/theses.2018.73


University of Toronto

16. 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 January 18, 2020. 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. 18 Jan 2020.

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 2020 Jan 18]. 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


Michigan Technological University

17. 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 January 18, 2020. https://digitalcommons.mtu.edu/etdr/886.

MLA Handbook (7th Edition):

Slabaugh, Tristan. “Cathode Coupling in a Low Power Hall Effect Thruster.” 2019. Web. 18 Jan 2020.

Vancouver:

Slabaugh T. Cathode Coupling in a Low Power Hall Effect Thruster. [Internet] [Masters thesis]. Michigan Technological University; 2019. [cited 2020 Jan 18]. 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 Tennessee – Knoxville

18. Fist, Andrew Steven. Development, Analysis, and Optimization of a Swirl-Promoting Mean Flow Solution for Solid Rocket Motors.

Degree: MS, Mechanical Engineering, 2016, University of Tennessee – Knoxville

  This work demonstrates and analyses a new flow candidate for describing the internal gaseous motion in simulated rocket motors. The fundamental features of this… (more)

Subjects/Keywords: Fluid Mechanics; Inviscid Flows; Propulsion; Rockets; Aerodynamics and Fluid Mechanics; Applied Mechanics; Engineering Physics; Propulsion and Power; Space Vehicles

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APA (6th Edition):

Fist, A. S. (2016). Development, Analysis, and Optimization of a Swirl-Promoting Mean Flow Solution for Solid Rocket Motors. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/4264

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):

Fist, Andrew Steven. “Development, Analysis, and Optimization of a Swirl-Promoting Mean Flow Solution for Solid Rocket Motors.” 2016. Thesis, University of Tennessee – Knoxville. Accessed January 18, 2020. https://trace.tennessee.edu/utk_gradthes/4264.

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

MLA Handbook (7th Edition):

Fist, Andrew Steven. “Development, Analysis, and Optimization of a Swirl-Promoting Mean Flow Solution for Solid Rocket Motors.” 2016. Web. 18 Jan 2020.

Vancouver:

Fist AS. Development, Analysis, and Optimization of a Swirl-Promoting Mean Flow Solution for Solid Rocket Motors. [Internet] [Thesis]. University of Tennessee – Knoxville; 2016. [cited 2020 Jan 18]. Available from: https://trace.tennessee.edu/utk_gradthes/4264.

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

Council of Science Editors:

Fist AS. Development, Analysis, and Optimization of a Swirl-Promoting Mean Flow Solution for Solid Rocket Motors. [Thesis]. University of Tennessee – Knoxville; 2016. Available from: https://trace.tennessee.edu/utk_gradthes/4264

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


Cal Poly

19. Lunde, Dominic Charles. A Homegrown DSMC-PIC Model for Electric Propulsion.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  Powering spacecraft with electric propulsion is becoming more common, especially in CubeSat-class satellites. On account of the risk of spacecraft interactions, it is important… (more)

Subjects/Keywords: DSMC; PIC; CFD; Plasma; Space; Propulsion; Aerodynamics and Fluid Mechanics; Propulsion and Power; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Lunde, D. C. (2019). A Homegrown DSMC-PIC Model for Electric Propulsion. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48

Chicago Manual of Style (16th Edition):

Lunde, Dominic Charles. “A Homegrown DSMC-PIC Model for Electric Propulsion.” 2019. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48.

MLA Handbook (7th Edition):

Lunde, Dominic Charles. “A Homegrown DSMC-PIC Model for Electric Propulsion.” 2019. Web. 18 Jan 2020.

Vancouver:

Lunde DC. A Homegrown DSMC-PIC Model for Electric Propulsion. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48.

Council of Science Editors:

Lunde DC. A Homegrown DSMC-PIC Model for Electric Propulsion. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2066 ; 10.15368/theses.2019.48

20. 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

…for micro-propulsion options with thrust F , specific impulse Isp , and required power P… …differentiates a propulsion system is its use of electrical power [1, 8]. Split into two… …supply of power for operation, while non-electric, or chemical propulsion systems, may require… …propulsion systems, which may only have < 20 W of total spacecraft power available [5]… …the Pocket Rocket thruster began in the Space Plasma, Power, and Propulsion laboratory at… 

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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 ; 10.15368/theses.2018.143

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 January 18, 2020. https://digitalcommons.calpoly.edu/theses/1961 ; 10.15368/theses.2018.143.

MLA Handbook (7th Edition):

Croteau, Tyler J. “Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster.” 2018. Web. 18 Jan 2020.

Vancouver:

Croteau TJ. Micro-Nozzle Simulation and Test for an Electrothermal Plasma Thruster. [Internet] [Masters thesis]. Cal Poly; 2018. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1961 ; 10.15368/theses.2018.143.

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 ; 10.15368/theses.2018.143


University of Tennessee – Knoxville

21. Williams, Nehemiah Joel. Numerical Investigations of a High Frequency Pulsed Gaseous Fuel Jet Injection into a Supersonic Crossflow.

Degree: 2016, University of Tennessee – Knoxville

 The investigation of fuel delivery mechanisms is a critical design point in the development of supersonic combustion ramjet (scramjet) technology. Primary challenges include proper penetration… (more)

Subjects/Keywords: Pulsed Injection; Supersonic Crossflows; Scramjet Fuel Injection; Aerodynamics and Fluid Mechanics; Propulsion and Power

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APA (6th Edition):

Williams, N. J. (2016). Numerical Investigations of a High Frequency Pulsed Gaseous Fuel Jet Injection into a Supersonic Crossflow. (Doctoral Dissertation). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_graddiss/3979

Chicago Manual of Style (16th Edition):

Williams, Nehemiah Joel. “Numerical Investigations of a High Frequency Pulsed Gaseous Fuel Jet Injection into a Supersonic Crossflow.” 2016. Doctoral Dissertation, University of Tennessee – Knoxville. Accessed January 18, 2020. https://trace.tennessee.edu/utk_graddiss/3979.

MLA Handbook (7th Edition):

Williams, Nehemiah Joel. “Numerical Investigations of a High Frequency Pulsed Gaseous Fuel Jet Injection into a Supersonic Crossflow.” 2016. Web. 18 Jan 2020.

Vancouver:

Williams NJ. Numerical Investigations of a High Frequency Pulsed Gaseous Fuel Jet Injection into a Supersonic Crossflow. [Internet] [Doctoral dissertation]. University of Tennessee – Knoxville; 2016. [cited 2020 Jan 18]. Available from: https://trace.tennessee.edu/utk_graddiss/3979.

Council of Science Editors:

Williams NJ. Numerical Investigations of a High Frequency Pulsed Gaseous Fuel Jet Injection into a Supersonic Crossflow. [Doctoral Dissertation]. University of Tennessee – Knoxville; 2016. Available from: https://trace.tennessee.edu/utk_graddiss/3979


Embry-Riddle Aeronautical University

22. Kitchen-McKinley, Samuel J. Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems.

Degree: PhD, Physical Sciences, 2017, Embry-Riddle Aeronautical University

  Small spacecrafts requiring small propulsion systems are becoming more popular for low Earth orbit. It is important for these research satellites to have accurate… (more)

Subjects/Keywords: Aerospace Engineering; Engineering Physics; Propulsion and Power; Space Vehicles; Statistical, Nonlinear, and Soft Matter Physics

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APA (6th Edition):

Kitchen-McKinley, S. J. (2017). Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/357

Chicago Manual of Style (16th Edition):

Kitchen-McKinley, Samuel J. “Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems.” 2017. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed January 18, 2020. https://commons.erau.edu/edt/357.

MLA Handbook (7th Edition):

Kitchen-McKinley, Samuel J. “Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems.” 2017. Web. 18 Jan 2020.

Vancouver:

Kitchen-McKinley SJ. Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2017. [cited 2020 Jan 18]. Available from: https://commons.erau.edu/edt/357.

Council of Science Editors:

Kitchen-McKinley SJ. Variable Structure Feedback Control with Application to Spacecraft with Small Thrust Propulsion Systems. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2017. Available from: https://commons.erau.edu/edt/357


University of Colorado

23. Guerrant, Daniel Vernon. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  Solar sails enable or enhance exploration of a variety of destinations both within and without the solar system. The heliogyro solar sail architecture divides… (more)

Subjects/Keywords: attitude control; dynamics; heliogyro; solar sail; structural dynamics; Astrodynamics; Propulsion and Power; Space Vehicles

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APA (6th Edition):

Guerrant, D. V. (2015). Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/101

Chicago Manual of Style (16th Edition):

Guerrant, Daniel Vernon. “Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.” 2015. Doctoral Dissertation, University of Colorado. Accessed January 18, 2020. https://scholar.colorado.edu/asen_gradetds/101.

MLA Handbook (7th Edition):

Guerrant, Daniel Vernon. “Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis.” 2015. Web. 18 Jan 2020.

Vancouver:

Guerrant DV. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2020 Jan 18]. Available from: https://scholar.colorado.edu/asen_gradetds/101.

Council of Science Editors:

Guerrant DV. Performance Quantification of Heliogyro Solar Sails Using Structural, Attitude, and Orbital Dynamics and Control Analysis. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/101


University of Tennessee – Knoxville

24. Lemieux, Jonathan. DJI S-1000 SPREADING WINGS OCTOCOPTER: DETERMINATION OF ROTOR DOWNWASH SLIPSTREAM SIZE.

Degree: MS, Engineering Science, 2016, University of Tennessee – Knoxville

  The DJI S-1000 Spreading Wings octocopter rotor downwash slipstream area of influence was measured in axial climb conditions and in straight level flight. These… (more)

Subjects/Keywords: Dr Trevor Moeller; Aerodynamics and Fluid Mechanics; Aeronautical Vehicles; Propulsion and Power

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APA (6th Edition):

Lemieux, J. (2016). DJI S-1000 SPREADING WINGS OCTOCOPTER: DETERMINATION OF ROTOR DOWNWASH SLIPSTREAM SIZE. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/4295

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):

Lemieux, Jonathan. “DJI S-1000 SPREADING WINGS OCTOCOPTER: DETERMINATION OF ROTOR DOWNWASH SLIPSTREAM SIZE.” 2016. Thesis, University of Tennessee – Knoxville. Accessed January 18, 2020. https://trace.tennessee.edu/utk_gradthes/4295.

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

MLA Handbook (7th Edition):

Lemieux, Jonathan. “DJI S-1000 SPREADING WINGS OCTOCOPTER: DETERMINATION OF ROTOR DOWNWASH SLIPSTREAM SIZE.” 2016. Web. 18 Jan 2020.

Vancouver:

Lemieux J. DJI S-1000 SPREADING WINGS OCTOCOPTER: DETERMINATION OF ROTOR DOWNWASH SLIPSTREAM SIZE. [Internet] [Thesis]. University of Tennessee – Knoxville; 2016. [cited 2020 Jan 18]. Available from: https://trace.tennessee.edu/utk_gradthes/4295.

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

Council of Science Editors:

Lemieux J. DJI S-1000 SPREADING WINGS OCTOCOPTER: DETERMINATION OF ROTOR DOWNWASH SLIPSTREAM SIZE. [Thesis]. University of Tennessee – Knoxville; 2016. Available from: https://trace.tennessee.edu/utk_gradthes/4295

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


University of Kentucky

25. Grib, Stephen William. LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS.

Degree: 2018, University of Kentucky

 Practical gas turbine engine combustors create extremely non-uniform flowfields, which are highly stratified making it imperative that similar environments are well understood. Laser diagnostics were… (more)

Subjects/Keywords: Laser Diagnostics; Edge Flames; Autoignition; Flame Stabilization; Extinction; Heat Transfer, Combustion; Propulsion and Power

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APA (6th Edition):

Grib, S. W. (2018). LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS. (Doctoral Dissertation). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/117

Chicago Manual of Style (16th Edition):

Grib, Stephen William. “LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS.” 2018. Doctoral Dissertation, University of Kentucky. Accessed January 18, 2020. https://uknowledge.uky.edu/me_etds/117.

MLA Handbook (7th Edition):

Grib, Stephen William. “LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS.” 2018. Web. 18 Jan 2020.

Vancouver:

Grib SW. LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS. [Internet] [Doctoral dissertation]. University of Kentucky; 2018. [cited 2020 Jan 18]. Available from: https://uknowledge.uky.edu/me_etds/117.

Council of Science Editors:

Grib SW. LAMINAR AND TURBULENT STUDY OF COMBUSTION IN STRATIFIED ENVIRONMENTS USING LASER BASED MEASUREMENTS. [Doctoral Dissertation]. University of Kentucky; 2018. Available from: https://uknowledge.uky.edu/me_etds/117


University of Kentucky

26. Flath, Allen, III. Mathematical Programming Approach for the Design of Satellite Power Systems.

Degree: 2019, University of Kentucky

 Satellite power systems can be understood as islanded dc microgrids supplied by specialized and coordinated solar cell arrays augmented by electrochemical battery systems to handle… (more)

Subjects/Keywords: satellite power systems; mathematical model; distributed power generation; modular architectures; multi-period models; Controls and Control Theory; Electrical and Electronics; Power and Energy; Propulsion and Power

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APA (6th Edition):

Flath, Allen, I. (2019). Mathematical Programming Approach for the Design of Satellite Power Systems. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/ece_etds/136

Chicago Manual of Style (16th Edition):

Flath, Allen, III. “Mathematical Programming Approach for the Design of Satellite Power Systems.” 2019. Masters Thesis, University of Kentucky. Accessed January 18, 2020. https://uknowledge.uky.edu/ece_etds/136.

MLA Handbook (7th Edition):

Flath, Allen, III. “Mathematical Programming Approach for the Design of Satellite Power Systems.” 2019. Web. 18 Jan 2020.

Vancouver:

Flath, Allen I. Mathematical Programming Approach for the Design of Satellite Power Systems. [Internet] [Masters thesis]. University of Kentucky; 2019. [cited 2020 Jan 18]. Available from: https://uknowledge.uky.edu/ece_etds/136.

Council of Science Editors:

Flath, Allen I. Mathematical Programming Approach for the Design of Satellite Power Systems. [Masters Thesis]. University of Kentucky; 2019. Available from: https://uknowledge.uky.edu/ece_etds/136


Michigan Technological University

27. Terhune, Kurt Joseph. Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source.

Degree: PhD, Department of Mechanical Engineering-Engineering Mechanics, 2017, Michigan Technological University

  Two electrospray sources were developed to operate on an ionic liquid ferrofluid; one source was a pressure‑fed capillary electrospray source and the other was… (more)

Subjects/Keywords: Electrospray; ferrofluid; ionic liquid; mass spectrometry; ionic liquid ferrofluid; Analytical Chemistry; Other Engineering; Other Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Terhune, K. J. (2017). Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source. (Doctoral Dissertation). Michigan Technological University. Retrieved from http://digitalcommons.mtu.edu/etdr/547

Chicago Manual of Style (16th Edition):

Terhune, Kurt Joseph. “Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source.” 2017. Doctoral Dissertation, Michigan Technological University. Accessed January 18, 2020. http://digitalcommons.mtu.edu/etdr/547.

MLA Handbook (7th Edition):

Terhune, Kurt Joseph. “Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source.” 2017. Web. 18 Jan 2020.

Vancouver:

Terhune KJ. Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source. [Internet] [Doctoral dissertation]. Michigan Technological University; 2017. [cited 2020 Jan 18]. Available from: http://digitalcommons.mtu.edu/etdr/547.

Council of Science Editors:

Terhune KJ. Influence of Magnetic Nanoparticles and Magnetic Stress on an Ionic Liquid Electrospray Source. [Doctoral Dissertation]. Michigan Technological University; 2017. Available from: http://digitalcommons.mtu.edu/etdr/547


University of Tennessee – Knoxville

28. Cox, Jon Rylan. Turbine Engine Rotor Blade Damage Detection through the Analysis of Vibration of Stationary Components.

Degree: 2016, University of Tennessee – Knoxville

 Rotor blade fault detection and health monitoring systems are crucial for gas turbine engine testing and evaluation. The most commonly used techniques involve monitoring blades… (more)

Subjects/Keywords: Structural Analysis; Modal Analysis; Statistical Analysis; NSMS; ViPA; ViPS; Aerospace Engineering; Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Cox, J. R. (2016). Turbine Engine Rotor Blade Damage Detection through the Analysis of Vibration of Stationary Components. (Doctoral Dissertation). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_graddiss/4091

Chicago Manual of Style (16th Edition):

Cox, Jon Rylan. “Turbine Engine Rotor Blade Damage Detection through the Analysis of Vibration of Stationary Components.” 2016. Doctoral Dissertation, University of Tennessee – Knoxville. Accessed January 18, 2020. https://trace.tennessee.edu/utk_graddiss/4091.

MLA Handbook (7th Edition):

Cox, Jon Rylan. “Turbine Engine Rotor Blade Damage Detection through the Analysis of Vibration of Stationary Components.” 2016. Web. 18 Jan 2020.

Vancouver:

Cox JR. Turbine Engine Rotor Blade Damage Detection through the Analysis of Vibration of Stationary Components. [Internet] [Doctoral dissertation]. University of Tennessee – Knoxville; 2016. [cited 2020 Jan 18]. Available from: https://trace.tennessee.edu/utk_graddiss/4091.

Council of Science Editors:

Cox JR. Turbine Engine Rotor Blade Damage Detection through the Analysis of Vibration of Stationary Components. [Doctoral Dissertation]. University of Tennessee – Knoxville; 2016. Available from: https://trace.tennessee.edu/utk_graddiss/4091


University of Tennessee – Knoxville

29. Mo, Jingke. Fundamental Studies of Electrochemical Reactions and Microfluidics in Proton Exchange Membrane Electrolyzer Cells.

Degree: 2016, University of Tennessee – Knoxville

 In electrochemical energy devices, including fuel cells, electrolyzers and batteries, the electrochemical reactions occur only on triple phase boundaries (TPBs). The boundaries provide the conductors… (more)

Subjects/Keywords: electrochemical reaction; microfluidics; visualization; liquid gas diffusion layer; modeling; proton exchange membrane electrolyzer cell; Energy Systems; Propulsion and Power

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APA (6th Edition):

Mo, J. (2016). Fundamental Studies of Electrochemical Reactions and Microfluidics in Proton Exchange Membrane Electrolyzer Cells. (Doctoral Dissertation). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_graddiss/4151

Chicago Manual of Style (16th Edition):

Mo, Jingke. “Fundamental Studies of Electrochemical Reactions and Microfluidics in Proton Exchange Membrane Electrolyzer Cells.” 2016. Doctoral Dissertation, University of Tennessee – Knoxville. Accessed January 18, 2020. https://trace.tennessee.edu/utk_graddiss/4151.

MLA Handbook (7th Edition):

Mo, Jingke. “Fundamental Studies of Electrochemical Reactions and Microfluidics in Proton Exchange Membrane Electrolyzer Cells.” 2016. Web. 18 Jan 2020.

Vancouver:

Mo J. Fundamental Studies of Electrochemical Reactions and Microfluidics in Proton Exchange Membrane Electrolyzer Cells. [Internet] [Doctoral dissertation]. University of Tennessee – Knoxville; 2016. [cited 2020 Jan 18]. Available from: https://trace.tennessee.edu/utk_graddiss/4151.

Council of Science Editors:

Mo J. Fundamental Studies of Electrochemical Reactions and Microfluidics in Proton Exchange Membrane Electrolyzer Cells. [Doctoral Dissertation]. University of Tennessee – Knoxville; 2016. Available from: https://trace.tennessee.edu/utk_graddiss/4151


Cal Poly

30. Bodnar, Maxwell J. The Creation, Analysis, and Verification of a Comprehensive Model of a Micro Ion Thruster.

Degree: MS, Aerospace Engineering, 2015, Cal Poly

  A computational model of the micro-ion thruster MiXI has been developed, analyzed, and partially verified. This model includes submodels that govern the physical, magnetic,… (more)

Subjects/Keywords: thesis; masters; cal poly; model; MiXI; ion thruster; Aerospace Engineering; Propulsion and Power; Systems Engineering and Multidisciplinary Design Optimization

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

APA (6th Edition):

Bodnar, M. J. (2015). The Creation, Analysis, and Verification of a Comprehensive Model of a Micro Ion Thruster. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1565 ; 10.15368/theses.2015.174

Chicago Manual of Style (16th Edition):

Bodnar, Maxwell J. “The Creation, Analysis, and Verification of a Comprehensive Model of a Micro Ion Thruster.” 2015. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/1565 ; 10.15368/theses.2015.174.

MLA Handbook (7th Edition):

Bodnar, Maxwell J. “The Creation, Analysis, and Verification of a Comprehensive Model of a Micro Ion Thruster.” 2015. Web. 18 Jan 2020.

Vancouver:

Bodnar MJ. The Creation, Analysis, and Verification of a Comprehensive Model of a Micro Ion Thruster. [Internet] [Masters thesis]. Cal Poly; 2015. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/1565 ; 10.15368/theses.2015.174.

Council of Science Editors:

Bodnar MJ. The Creation, Analysis, and Verification of a Comprehensive Model of a Micro Ion Thruster. [Masters Thesis]. Cal Poly; 2015. Available from: https://digitalcommons.calpoly.edu/theses/1565 ; 10.15368/theses.2015.174

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