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You searched for subject:(Jet engine). Showing records 1 – 30 of 106 total matches.

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Georgia Tech

1. Kundu, Reema. Impact of engine icing on jet engine compressor flow dynamics.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This previously unrecognized form of icing occurs in flights… (more)

Subjects/Keywords: Engine icing; Compressor; Jet engine; Compressible flow; Compressor stall

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APA (6th Edition):

Kundu, R. (2015). Impact of engine icing on jet engine compressor flow dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54870

Chicago Manual of Style (16th Edition):

Kundu, Reema. “Impact of engine icing on jet engine compressor flow dynamics.” 2015. Doctoral Dissertation, Georgia Tech. Accessed October 22, 2019. http://hdl.handle.net/1853/54870.

MLA Handbook (7th Edition):

Kundu, Reema. “Impact of engine icing on jet engine compressor flow dynamics.” 2015. Web. 22 Oct 2019.

Vancouver:

Kundu R. Impact of engine icing on jet engine compressor flow dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/1853/54870.

Council of Science Editors:

Kundu R. Impact of engine icing on jet engine compressor flow dynamics. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54870


Linköping University

2. Wemming, Hannes. Validation and integration of a rubber engine model into an MDO environment.

Degree: Fluid and Mechanical Engineering Systems, 2010, Linköping University

  Multidisciplinary design optimization (MDO) is a technique that has found use in the field of aerospace engineering for aircraft design. It uses optimization to… (more)

Subjects/Keywords: Aero engine; Gas turbine; Jet engine; MDO; Rubber engine; Performance modeling; GasTurb; Vehicle engineering; Farkostteknik

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APA (6th Edition):

Wemming, H. (2010). Validation and integration of a rubber engine model into an MDO environment. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-61028

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):

Wemming, Hannes. “Validation and integration of a rubber engine model into an MDO environment.” 2010. Thesis, Linköping University. Accessed October 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-61028.

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

MLA Handbook (7th Edition):

Wemming, Hannes. “Validation and integration of a rubber engine model into an MDO environment.” 2010. Web. 22 Oct 2019.

Vancouver:

Wemming H. Validation and integration of a rubber engine model into an MDO environment. [Internet] [Thesis]. Linköping University; 2010. [cited 2019 Oct 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-61028.

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

Council of Science Editors:

Wemming H. Validation and integration of a rubber engine model into an MDO environment. [Thesis]. Linköping University; 2010. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-61028

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


Brno University of Technology

3. Fiala, Luboš. Vývojové trendy leteckých lopatkových motorů .

Degree: 2011, Brno University of Technology

 Hlavním záměrem této bakalářské práce je shrnout aktuální vývoj probíhající v oblasti lopatkových civilních motorů. Tento vývoj je směřován ke snížení spotřeby paliva a zvýšení… (more)

Subjects/Keywords: proudový motor; bezplášťové dmychadlo; zpřevodované dmychadlo; jet engine; propfan engine; geared turbofan engine

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APA (6th Edition):

Fiala, L. (2011). Vývojové trendy leteckých lopatkových motorů . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/2114

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):

Fiala, Luboš. “Vývojové trendy leteckých lopatkových motorů .” 2011. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/2114.

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

MLA Handbook (7th Edition):

Fiala, Luboš. “Vývojové trendy leteckých lopatkových motorů .” 2011. Web. 22 Oct 2019.

Vancouver:

Fiala L. Vývojové trendy leteckých lopatkových motorů . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/2114.

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

Council of Science Editors:

Fiala L. Vývojové trendy leteckých lopatkových motorů . [Thesis]. Brno University of Technology; 2011. Available from: http://hdl.handle.net/11012/2114

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


University of New South Wales

4. Le, Minh Khoi. Understanding the development of a reacting fuel jet inside an automotive-size diesel engine using optical and laser-based diagnostics.

Degree: Mechanical & Manufacturing Engineering, 2015, University of New South Wales

 The fuel penetration and reacting diesel jet development have been studied in a small-bore optical engine to improve the understanding of a swirl-influenced, wall-interacting diesel… (more)

Subjects/Keywords: Laser diagnostics; Optical engine; Engine combustion; OH-PLIF; Soot-PLII; Optical diagnostics; Diesel engine; Diesel jet development

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APA (6th Edition):

Le, M. K. (2015). Understanding the development of a reacting fuel jet inside an automotive-size diesel engine using optical and laser-based diagnostics. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/55272 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:37004/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Le, Minh Khoi. “Understanding the development of a reacting fuel jet inside an automotive-size diesel engine using optical and laser-based diagnostics.” 2015. Doctoral Dissertation, University of New South Wales. Accessed October 22, 2019. http://handle.unsw.edu.au/1959.4/55272 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:37004/SOURCE02?view=true.

MLA Handbook (7th Edition):

Le, Minh Khoi. “Understanding the development of a reacting fuel jet inside an automotive-size diesel engine using optical and laser-based diagnostics.” 2015. Web. 22 Oct 2019.

Vancouver:

Le MK. Understanding the development of a reacting fuel jet inside an automotive-size diesel engine using optical and laser-based diagnostics. [Internet] [Doctoral dissertation]. University of New South Wales; 2015. [cited 2019 Oct 22]. Available from: http://handle.unsw.edu.au/1959.4/55272 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:37004/SOURCE02?view=true.

Council of Science Editors:

Le MK. Understanding the development of a reacting fuel jet inside an automotive-size diesel engine using optical and laser-based diagnostics. [Doctoral Dissertation]. University of New South Wales; 2015. Available from: http://handle.unsw.edu.au/1959.4/55272 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:37004/SOURCE02?view=true


Brno University of Technology

5. Heczko, Nikodem. Letecké proudové motory s proměnným cyklem .

Degree: 2013, Brno University of Technology

 V této závěrečné bakalářské práci je zpracován základní přehled a rozdělení turbínových motorů, včetně stručného popisu jejich funkce. Práce je zaměřena na problematiku proudových motorů… (more)

Subjects/Keywords: Proudový motor; letecký motor; proměnný cyklus; turbínový motor; Jet engine; aircraft engine; variable cycle; gas turbine engine

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APA (6th Edition):

Heczko, N. (2013). Letecké proudové motory s proměnným cyklem . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27274

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):

Heczko, Nikodem. “Letecké proudové motory s proměnným cyklem .” 2013. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/27274.

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

MLA Handbook (7th Edition):

Heczko, Nikodem. “Letecké proudové motory s proměnným cyklem .” 2013. Web. 22 Oct 2019.

Vancouver:

Heczko N. Letecké proudové motory s proměnným cyklem . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/27274.

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

Council of Science Editors:

Heczko N. Letecké proudové motory s proměnným cyklem . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/27274

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


Loughborough University

6. Bourne, Duncan. A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach.

Degree: PhD, 2011, Loughborough University

 The design of distributed control systems (DCSs) for large, civil gas turbine engines is a complex architectural challenge. To date, the majority of research into… (more)

Subjects/Keywords: 004.36; Distributed systems; Systems engineering; Genetic algorithm; Optimisation; Jet engine

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

APA (6th Edition):

Bourne, D. (2011). A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/10406 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561164

Chicago Manual of Style (16th Edition):

Bourne, Duncan. “A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach.” 2011. Doctoral Dissertation, Loughborough University. Accessed October 22, 2019. https://dspace.lboro.ac.uk/2134/10406 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561164.

MLA Handbook (7th Edition):

Bourne, Duncan. “A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach.” 2011. Web. 22 Oct 2019.

Vancouver:

Bourne D. A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach. [Internet] [Doctoral dissertation]. Loughborough University; 2011. [cited 2019 Oct 22]. Available from: https://dspace.lboro.ac.uk/2134/10406 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561164.

Council of Science Editors:

Bourne D. A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach. [Doctoral Dissertation]. Loughborough University; 2011. Available from: https://dspace.lboro.ac.uk/2134/10406 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.561164


Lehigh University

7. Mi, Yushi. A Jet Engine Retraction System.

Degree: MS, Mechanical Engineering, 2017, Lehigh University

 A high-altitude dynamic soaring unmanned aerial vehicle (UAV) called JetStreamer has been designed and built in the Composites Lab of Lehigh University. A small jet(more)

Subjects/Keywords: dynamic soaring; jet engine; retraction; UAV; Engineering; Mechanical Engineering

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APA (6th Edition):

Mi, Y. (2017). A Jet Engine Retraction System. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2726

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):

Mi, Yushi. “A Jet Engine Retraction System.” 2017. Thesis, Lehigh University. Accessed October 22, 2019. https://preserve.lehigh.edu/etd/2726.

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

MLA Handbook (7th Edition):

Mi, Yushi. “A Jet Engine Retraction System.” 2017. Web. 22 Oct 2019.

Vancouver:

Mi Y. A Jet Engine Retraction System. [Internet] [Thesis]. Lehigh University; 2017. [cited 2019 Oct 22]. Available from: https://preserve.lehigh.edu/etd/2726.

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

Council of Science Editors:

Mi Y. A Jet Engine Retraction System. [Thesis]. Lehigh University; 2017. Available from: https://preserve.lehigh.edu/etd/2726

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


University of Canterbury

8. Gilmore, Jordan David. Computational Fluid Dynamics Analysis of Jet Engine Test Facilities.

Degree: Mechanical Engineering, 2012, University of Canterbury

 This thesis investigates the application of CFD techniques to the aerodynamic analysis of a U-shaped JETC. Investigations were carried out to determine the flow patterns… (more)

Subjects/Keywords: CFD; Computational Fluid Dynamics; Jet Engine; Test Cell; JETC

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APA (6th Edition):

Gilmore, J. D. (2012). Computational Fluid Dynamics Analysis of Jet Engine Test Facilities. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/7238

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):

Gilmore, Jordan David. “Computational Fluid Dynamics Analysis of Jet Engine Test Facilities.” 2012. Thesis, University of Canterbury. Accessed October 22, 2019. http://hdl.handle.net/10092/7238.

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

MLA Handbook (7th Edition):

Gilmore, Jordan David. “Computational Fluid Dynamics Analysis of Jet Engine Test Facilities.” 2012. Web. 22 Oct 2019.

Vancouver:

Gilmore JD. Computational Fluid Dynamics Analysis of Jet Engine Test Facilities. [Internet] [Thesis]. University of Canterbury; 2012. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/10092/7238.

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

Council of Science Editors:

Gilmore JD. Computational Fluid Dynamics Analysis of Jet Engine Test Facilities. [Thesis]. University of Canterbury; 2012. Available from: http://hdl.handle.net/10092/7238

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


Luleå University of Technology

9. Åhman, Joakim. CFD Validation of Tip Clearance Flows in an Axial Compressor.

Degree: 2016, Luleå University of Technology

When designing a compressor it is desirable to keep the development cost low while ensuring that the compressor meets the required performance. The typical… (more)

Subjects/Keywords: Technology; Teknik; CFD; validation; tip clearance; compressor; jet engine

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APA (6th Edition):

Åhman, J. (2016). CFD Validation of Tip Clearance Flows in an Axial Compressor. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-43216

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):

Åhman, Joakim. “CFD Validation of Tip Clearance Flows in an Axial Compressor.” 2016. Thesis, Luleå University of Technology. Accessed October 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-43216.

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

MLA Handbook (7th Edition):

Åhman, Joakim. “CFD Validation of Tip Clearance Flows in an Axial Compressor.” 2016. Web. 22 Oct 2019.

Vancouver:

Åhman J. CFD Validation of Tip Clearance Flows in an Axial Compressor. [Internet] [Thesis]. Luleå University of Technology; 2016. [cited 2019 Oct 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-43216.

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

Council of Science Editors:

Åhman J. CFD Validation of Tip Clearance Flows in an Axial Compressor. [Thesis]. Luleå University of Technology; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-43216

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


Baylor University

10. [No author]. Evaluating approaches to detecting ice accretion in and around turbofan jet engines.

Degree: 2018, Baylor University

 The accumulation of ice crystals in the compressor stages of a jet engine causes power loss events during flight that could potentially become catastrophic. The… (more)

Subjects/Keywords: Ice cloud. Ice accretion. Turbofan jet engine. Radiometry. Interferometry.

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APA (6th Edition):

author], [. (2018). Evaluating approaches to detecting ice accretion in and around turbofan jet engines. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/10432

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):

author], [No. “Evaluating approaches to detecting ice accretion in and around turbofan jet engines. ” 2018. Thesis, Baylor University. Accessed October 22, 2019. http://hdl.handle.net/2104/10432.

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

MLA Handbook (7th Edition):

author], [No. “Evaluating approaches to detecting ice accretion in and around turbofan jet engines. ” 2018. Web. 22 Oct 2019.

Vancouver:

author] [. Evaluating approaches to detecting ice accretion in and around turbofan jet engines. [Internet] [Thesis]. Baylor University; 2018. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/2104/10432.

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

Council of Science Editors:

author] [. Evaluating approaches to detecting ice accretion in and around turbofan jet engines. [Thesis]. Baylor University; 2018. Available from: http://hdl.handle.net/2104/10432

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


Utah State University

11. Schaefermeyer, M. Ryan. Aerodynamic Thrust Vectoring For Attitude Control Of A Vertically Thrusting Jet Engine.

Degree: MS, Mechanical and Aerospace Engineering, 2011, Utah State University

  NASA’s long range vision for space exploration includes human and robotic missions to extraterrestrial bodies including the moon, asteroids and the martian surface. All… (more)

Subjects/Keywords: Aerodynamic; Thrust; Attitude; Verticallly Thrusting; Jet Engine; Engineering; Mechanical Engineering

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

APA (6th Edition):

Schaefermeyer, M. R. (2011). Aerodynamic Thrust Vectoring For Attitude Control Of A Vertically Thrusting Jet Engine. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/1237

Chicago Manual of Style (16th Edition):

Schaefermeyer, M Ryan. “Aerodynamic Thrust Vectoring For Attitude Control Of A Vertically Thrusting Jet Engine.” 2011. Masters Thesis, Utah State University. Accessed October 22, 2019. https://digitalcommons.usu.edu/etd/1237.

MLA Handbook (7th Edition):

Schaefermeyer, M Ryan. “Aerodynamic Thrust Vectoring For Attitude Control Of A Vertically Thrusting Jet Engine.” 2011. Web. 22 Oct 2019.

Vancouver:

Schaefermeyer MR. Aerodynamic Thrust Vectoring For Attitude Control Of A Vertically Thrusting Jet Engine. [Internet] [Masters thesis]. Utah State University; 2011. [cited 2019 Oct 22]. Available from: https://digitalcommons.usu.edu/etd/1237.

Council of Science Editors:

Schaefermeyer MR. Aerodynamic Thrust Vectoring For Attitude Control Of A Vertically Thrusting Jet Engine. [Masters Thesis]. Utah State University; 2011. Available from: https://digitalcommons.usu.edu/etd/1237


Loughborough University

12. Bourne, Duncan. A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach.

Degree: PhD, 2011, Loughborough University

 The design of distributed control systems (DCSs) for large, civil gas turbine engines is a complex architectural challenge. To date, the majority of research into… (more)

Subjects/Keywords: 004.36; Distributed systems; Systems engineering; Genetic algorithm; Optimisation; Jet engine

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

APA (6th Edition):

Bourne, D. (2011). A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/10406

Chicago Manual of Style (16th Edition):

Bourne, Duncan. “A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach.” 2011. Doctoral Dissertation, Loughborough University. Accessed October 22, 2019. http://hdl.handle.net/2134/10406.

MLA Handbook (7th Edition):

Bourne, Duncan. “A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach.” 2011. Web. 22 Oct 2019.

Vancouver:

Bourne D. A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach. [Internet] [Doctoral dissertation]. Loughborough University; 2011. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/2134/10406.

Council of Science Editors:

Bourne D. A method for the architectural design of distributed control systems for large, civil jet engines : a systems engineering approach. [Doctoral Dissertation]. Loughborough University; 2011. Available from: http://hdl.handle.net/2134/10406


Brno University of Technology

13. Trusík, Vojtěch. Zkoušení leteckých proudových motorů .

Degree: 2011, Brno University of Technology

 Tato bakalářská práce se skládá ze dvou základních části. První část práce se zabývá popisem leteckých úřadů a agentur, činností proudového motoru, zkušebním zařízením a… (more)

Subjects/Keywords: Letecký motor; proudový motor; lopatkový motor; zkušební zařízení; zkouška; soustavy lopatkových motorů; tah; charakteristika; Aircraft engine; jet engine; blade engine; testing bed; test; systems of jet engines; thrust; characteristic

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APA (6th Edition):

Trusík, V. (2011). Zkoušení leteckých proudových motorů . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1506

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):

Trusík, Vojtěch. “Zkoušení leteckých proudových motorů .” 2011. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/1506.

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

MLA Handbook (7th Edition):

Trusík, Vojtěch. “Zkoušení leteckých proudových motorů .” 2011. Web. 22 Oct 2019.

Vancouver:

Trusík V. Zkoušení leteckých proudových motorů . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/1506.

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

Council of Science Editors:

Trusík V. Zkoušení leteckých proudových motorů . [Thesis]. Brno University of Technology; 2011. Available from: http://hdl.handle.net/11012/1506

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


University of Oxford

14. Forsyth, Peter. High temperature particle deposition with gas turbine applications.

Degree: PhD, 2017, University of Oxford

 This thesis describes validated improvements in the modelling of micron-sized particle deposition within gas turbine engine secondary air systems. The initial aim of the research… (more)

Subjects/Keywords: Aerospace; Fluid dynamics; Multi-phase flow; Engineering; Two-phase flow; Gas turbine engine; Particle motion; High temperature; Particle deposition; Jet engine

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APA (6th Edition):

Forsyth, P. (2017). High temperature particle deposition with gas turbine applications. (Doctoral Dissertation). University of Oxford. Retrieved from http://ora.ox.ac.uk/objects/uuid:61556237-feed-43cb-9f4a-d0aed00ca3f8 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748784

Chicago Manual of Style (16th Edition):

Forsyth, Peter. “High temperature particle deposition with gas turbine applications.” 2017. Doctoral Dissertation, University of Oxford. Accessed October 22, 2019. http://ora.ox.ac.uk/objects/uuid:61556237-feed-43cb-9f4a-d0aed00ca3f8 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748784.

MLA Handbook (7th Edition):

Forsyth, Peter. “High temperature particle deposition with gas turbine applications.” 2017. Web. 22 Oct 2019.

Vancouver:

Forsyth P. High temperature particle deposition with gas turbine applications. [Internet] [Doctoral dissertation]. University of Oxford; 2017. [cited 2019 Oct 22]. Available from: http://ora.ox.ac.uk/objects/uuid:61556237-feed-43cb-9f4a-d0aed00ca3f8 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748784.

Council of Science Editors:

Forsyth P. High temperature particle deposition with gas turbine applications. [Doctoral Dissertation]. University of Oxford; 2017. Available from: http://ora.ox.ac.uk/objects/uuid:61556237-feed-43cb-9f4a-d0aed00ca3f8 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.748784


Brno University of Technology

15. Štefanovič, Peter. Vývoj a současně vyráběné jednoproudové motory .

Degree: 2016, Brno University of Technology

 Hlavným cieľom tejto bakalárskej práce je akýsi ucelený prehľad v oblasti jednoprúdových motorov. Stručne vysvetľuje širokú problematiku plynových turbín z hľadiska samotného fungovania, princípu činnosti… (more)

Subjects/Keywords: Jednoprúdový motor; tepelný stroj; ťah; spaľovacia komora; turbína.; Pure jet engine; heat engine; thrust; combustion chamber; turbine.

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APA (6th Edition):

Štefanovič, P. (2016). Vývoj a současně vyráběné jednoproudové motory . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/60294

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):

Štefanovič, Peter. “Vývoj a současně vyráběné jednoproudové motory .” 2016. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/60294.

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

MLA Handbook (7th Edition):

Štefanovič, Peter. “Vývoj a současně vyráběné jednoproudové motory .” 2016. Web. 22 Oct 2019.

Vancouver:

Štefanovič P. Vývoj a současně vyráběné jednoproudové motory . [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/60294.

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

Council of Science Editors:

Štefanovič P. Vývoj a současně vyráběné jednoproudové motory . [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/60294

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


Loughborough University

16. Carrotte, Jonathan F. The mixing characteristics of dilution jets issuing into a confined cross-flow.

Degree: PhD, 1990, Loughborough University

 An experimental investigation has been carried out into the mixing of a row of jets injected into a confined cross-flow. Measurements were made on a… (more)

Subjects/Keywords: 621.4352; Jet mixing/gas turbine engine

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APA (6th Edition):

Carrotte, J. F. (1990). The mixing characteristics of dilution jets issuing into a confined cross-flow. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/32627 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276211

Chicago Manual of Style (16th Edition):

Carrotte, Jonathan F. “The mixing characteristics of dilution jets issuing into a confined cross-flow.” 1990. Doctoral Dissertation, Loughborough University. Accessed October 22, 2019. https://dspace.lboro.ac.uk/2134/32627 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276211.

MLA Handbook (7th Edition):

Carrotte, Jonathan F. “The mixing characteristics of dilution jets issuing into a confined cross-flow.” 1990. Web. 22 Oct 2019.

Vancouver:

Carrotte JF. The mixing characteristics of dilution jets issuing into a confined cross-flow. [Internet] [Doctoral dissertation]. Loughborough University; 1990. [cited 2019 Oct 22]. Available from: https://dspace.lboro.ac.uk/2134/32627 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276211.

Council of Science Editors:

Carrotte JF. The mixing characteristics of dilution jets issuing into a confined cross-flow. [Doctoral Dissertation]. Loughborough University; 1990. Available from: https://dspace.lboro.ac.uk/2134/32627 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276211


University of Canterbury

17. Ho, Wei Hua. Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell.

Degree: Department of Mechanical Engineering, 2009, University of Canterbury

 This thesis details an in investigation of two problems arising during the testing of a jet engine in a test cell, namely the formation and… (more)

Subjects/Keywords: Infrasound; low frequency noise; vortices; vortex; CFD; Fluent; jet engine test cell; JETC

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APA (6th Edition):

Ho, W. H. (2009). Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/4457

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):

Ho, Wei Hua. “Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell.” 2009. Thesis, University of Canterbury. Accessed October 22, 2019. http://hdl.handle.net/10092/4457.

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

MLA Handbook (7th Edition):

Ho, Wei Hua. “Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell.” 2009. Web. 22 Oct 2019.

Vancouver:

Ho WH. Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell. [Internet] [Thesis]. University of Canterbury; 2009. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/10092/4457.

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

Council of Science Editors:

Ho WH. Investigation into the Vortex Formation Threshold and Infrasound Generation in a Jet Engine Test Cell. [Thesis]. University of Canterbury; 2009. Available from: http://hdl.handle.net/10092/4457

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


University of Cincinnati

18. DRENSKY, GEORGE K. EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES.

Degree: PhD, Engineering : Aerospace Engineering, 2007, University of Cincinnati

 The design and development of high performance turbomachinery operating in both ambient and high temperature environment in the presence of solid particles requires a thorough… (more)

Subjects/Keywords: Engineering, Aerospace; Composite materials; Erosion Tunnel; Erosion; Models and Correlations; Jet Engine Performance

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APA (6th Edition):

DRENSKY, G. K. (2007). EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1178118863

Chicago Manual of Style (16th Edition):

DRENSKY, GEORGE K. “EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES.” 2007. Doctoral Dissertation, University of Cincinnati. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1178118863.

MLA Handbook (7th Edition):

DRENSKY, GEORGE K. “EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES.” 2007. Web. 22 Oct 2019.

Vancouver:

DRENSKY GK. EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES. [Internet] [Doctoral dissertation]. University of Cincinnati; 2007. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1178118863.

Council of Science Editors:

DRENSKY GK. EXPERIMENTAL INVESTIGATION OF COMPOSITE MATERIAL EROSION CHARACTERISTICS UNDER CONDITIONS ENCOUNTERED IN TURBOFAN ENGINES. [Doctoral Dissertation]. University of Cincinnati; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1178118863


RMIT University

19. Jiang, S. Numerical analysis of two-stroke engine with direct injection and jet ignition.

Degree: 2015, RMIT University

 This thesis is carried out to evaluate the combustion evolution and the engine performance parameters of a two-stroke engine with direct injection and jet ignition.… (more)

Subjects/Keywords: Fields of Research; Direct injection; Jet ignition; Two-stroke engine; Computational fluid dynamics; Numerical analysis

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APA (6th Edition):

Jiang, S. (2015). Numerical analysis of two-stroke engine with direct injection and jet ignition. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161450

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):

Jiang, S. “Numerical analysis of two-stroke engine with direct injection and jet ignition.” 2015. Thesis, RMIT University. Accessed October 22, 2019. http://researchbank.rmit.edu.au/view/rmit:161450.

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

MLA Handbook (7th Edition):

Jiang, S. “Numerical analysis of two-stroke engine with direct injection and jet ignition.” 2015. Web. 22 Oct 2019.

Vancouver:

Jiang S. Numerical analysis of two-stroke engine with direct injection and jet ignition. [Internet] [Thesis]. RMIT University; 2015. [cited 2019 Oct 22]. Available from: http://researchbank.rmit.edu.au/view/rmit:161450.

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

Council of Science Editors:

Jiang S. Numerical analysis of two-stroke engine with direct injection and jet ignition. [Thesis]. RMIT University; 2015. Available from: http://researchbank.rmit.edu.au/view/rmit:161450

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

20. Marhaba, Iman. Structure et propriétés physico-chimiques à l'échelle nanométrique d'aérosols carbonés d'origine aéronautique : Structure and physico-chemical properties of aircraft carbonaceous aerosols at the nanometer scale.

Degree: Docteur es, Physique et sciences de la matière. Matière condensée et nanosciences, 2017, Aix Marseille Université

Les particules de suie émises par les moteurs d'avion influencent le climat en absorbant/diffusant la lumière solaire. Elles agissent aussi comme noyaux glaciogènes dans l’atmosphère… (more)

Subjects/Keywords: Suies; Turboréacteur; Met; Ftir; Nexafs; Xps; Soot; Jet engine; Tem; Ftir; Nexafs; Xps; 530

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APA (6th Edition):

Marhaba, I. (2017). Structure et propriétés physico-chimiques à l'échelle nanométrique d'aérosols carbonés d'origine aéronautique : Structure and physico-chemical properties of aircraft carbonaceous aerosols at the nanometer scale. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2017AIXM0308

Chicago Manual of Style (16th Edition):

Marhaba, Iman. “Structure et propriétés physico-chimiques à l'échelle nanométrique d'aérosols carbonés d'origine aéronautique : Structure and physico-chemical properties of aircraft carbonaceous aerosols at the nanometer scale.” 2017. Doctoral Dissertation, Aix Marseille Université. Accessed October 22, 2019. http://www.theses.fr/2017AIXM0308.

MLA Handbook (7th Edition):

Marhaba, Iman. “Structure et propriétés physico-chimiques à l'échelle nanométrique d'aérosols carbonés d'origine aéronautique : Structure and physico-chemical properties of aircraft carbonaceous aerosols at the nanometer scale.” 2017. Web. 22 Oct 2019.

Vancouver:

Marhaba I. Structure et propriétés physico-chimiques à l'échelle nanométrique d'aérosols carbonés d'origine aéronautique : Structure and physico-chemical properties of aircraft carbonaceous aerosols at the nanometer scale. [Internet] [Doctoral dissertation]. Aix Marseille Université 2017. [cited 2019 Oct 22]. Available from: http://www.theses.fr/2017AIXM0308.

Council of Science Editors:

Marhaba I. Structure et propriétés physico-chimiques à l'échelle nanométrique d'aérosols carbonés d'origine aéronautique : Structure and physico-chemical properties of aircraft carbonaceous aerosols at the nanometer scale. [Doctoral Dissertation]. Aix Marseille Université 2017. Available from: http://www.theses.fr/2017AIXM0308


Ohio University

21. Dowler, John D. Using Neural Networks with Limited Data to Estimate Manufacturing Cost.

Degree: MS, Industrial and Systems Engineering (Engineering and Technology), 2008, Ohio University

  This paper investigates the ability of a neural network to estimate the cost of jet engine components, specifically shafts and cases. Even with limited… (more)

Subjects/Keywords: Economics; Engineering; Industrial Engineering; Neural network; cost estimation; limited data; jet engine

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APA (6th Edition):

Dowler, J. D. (2008). Using Neural Networks with Limited Data to Estimate Manufacturing Cost. (Masters Thesis). Ohio University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1211293606

Chicago Manual of Style (16th Edition):

Dowler, John D. “Using Neural Networks with Limited Data to Estimate Manufacturing Cost.” 2008. Masters Thesis, Ohio University. Accessed October 22, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1211293606.

MLA Handbook (7th Edition):

Dowler, John D. “Using Neural Networks with Limited Data to Estimate Manufacturing Cost.” 2008. Web. 22 Oct 2019.

Vancouver:

Dowler JD. Using Neural Networks with Limited Data to Estimate Manufacturing Cost. [Internet] [Masters thesis]. Ohio University; 2008. [cited 2019 Oct 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1211293606.

Council of Science Editors:

Dowler JD. Using Neural Networks with Limited Data to Estimate Manufacturing Cost. [Masters Thesis]. Ohio University; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1211293606


Cranfield University

22. Tourlidakis, A. Numerical modelling of viscous turbomachinery flows with a pressure correction method.

Degree: PhD, 1992, Cranfield University

 A fully elliptic computational method for the analysis of steady viscous flow in high speed subsonic centrifugal compressor impellers with tip leakage, is presented. A… (more)

Subjects/Keywords: 532; Jet engine gas flow modelling

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APA (6th Edition):

Tourlidakis, A. (1992). Numerical modelling of viscous turbomachinery flows with a pressure correction method. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/3997 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305246

Chicago Manual of Style (16th Edition):

Tourlidakis, A. “Numerical modelling of viscous turbomachinery flows with a pressure correction method.” 1992. Doctoral Dissertation, Cranfield University. Accessed October 22, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/3997 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305246.

MLA Handbook (7th Edition):

Tourlidakis, A. “Numerical modelling of viscous turbomachinery flows with a pressure correction method.” 1992. Web. 22 Oct 2019.

Vancouver:

Tourlidakis A. Numerical modelling of viscous turbomachinery flows with a pressure correction method. [Internet] [Doctoral dissertation]. Cranfield University; 1992. [cited 2019 Oct 22]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/3997 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305246.

Council of Science Editors:

Tourlidakis A. Numerical modelling of viscous turbomachinery flows with a pressure correction method. [Doctoral Dissertation]. Cranfield University; 1992. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/3997 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305246


University of Arkansas

23. Mason, Rex. Pacer Comet 4: Automated Jet Engine Testing of a TF33-P100 Pratt & Whitney Engine.

Degree: MSEE, 2015, University of Arkansas

  Pacer Comet 4 found its life out of necessity to replace an obsolescent Pacer Comet 3 engine test system at Tinker AFB in Oklahoma… (more)

Subjects/Keywords: Automated; Jet engine; Pacer comet; Testing; Tf33; Aerospace Engineering; Electrical and Computer Engineering

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APA (6th Edition):

Mason, R. (2015). Pacer Comet 4: Automated Jet Engine Testing of a TF33-P100 Pratt & Whitney Engine. (Masters Thesis). University of Arkansas. Retrieved from https://scholarworks.uark.edu/etd/32

Chicago Manual of Style (16th Edition):

Mason, Rex. “Pacer Comet 4: Automated Jet Engine Testing of a TF33-P100 Pratt & Whitney Engine.” 2015. Masters Thesis, University of Arkansas. Accessed October 22, 2019. https://scholarworks.uark.edu/etd/32.

MLA Handbook (7th Edition):

Mason, Rex. “Pacer Comet 4: Automated Jet Engine Testing of a TF33-P100 Pratt & Whitney Engine.” 2015. Web. 22 Oct 2019.

Vancouver:

Mason R. Pacer Comet 4: Automated Jet Engine Testing of a TF33-P100 Pratt & Whitney Engine. [Internet] [Masters thesis]. University of Arkansas; 2015. [cited 2019 Oct 22]. Available from: https://scholarworks.uark.edu/etd/32.

Council of Science Editors:

Mason R. Pacer Comet 4: Automated Jet Engine Testing of a TF33-P100 Pratt & Whitney Engine. [Masters Thesis]. University of Arkansas; 2015. Available from: https://scholarworks.uark.edu/etd/32

24. Srikrishnanivas, Deepak. Rotor Dynamic Analysis of RM12 Jet Engine Rotor using ANSYS.

Degree: 2012, , School of Engineering

  Rotordynamics is a field under mechanics, mainly deals with the vibration of rotating structures. In recent days, the study about rotordynamics has gained more… (more)

Subjects/Keywords: Rotordynamics; RM12; Jet engine; Gas turbines; Ansys; Dyrobes; Vibration; Rotor; Twin spool

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APA (6th Edition):

Srikrishnanivas, D. (2012). Rotor Dynamic Analysis of RM12 Jet Engine Rotor using ANSYS. (Thesis). , School of Engineering. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:bth-2904

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):

Srikrishnanivas, Deepak. “Rotor Dynamic Analysis of RM12 Jet Engine Rotor using ANSYS.” 2012. Thesis, , School of Engineering. Accessed October 22, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:bth-2904.

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

MLA Handbook (7th Edition):

Srikrishnanivas, Deepak. “Rotor Dynamic Analysis of RM12 Jet Engine Rotor using ANSYS.” 2012. Web. 22 Oct 2019.

Vancouver:

Srikrishnanivas D. Rotor Dynamic Analysis of RM12 Jet Engine Rotor using ANSYS. [Internet] [Thesis]. , School of Engineering; 2012. [cited 2019 Oct 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:bth-2904.

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

Council of Science Editors:

Srikrishnanivas D. Rotor Dynamic Analysis of RM12 Jet Engine Rotor using ANSYS. [Thesis]. , School of Engineering; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:bth-2904

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


University of Tennessee – Knoxville

25. Holst, Kevin Raymond. A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors.

Degree: MS, Aerospace Engineering, 2012, University of Tennessee – Knoxville

  Ramjet and scramjet engines are being developed to provide a more fuel efficient means of propulsion at high Mach numbers. Part of the development… (more)

Subjects/Keywords: Ramjet; Engine Performance; Uncertainty; Free-jet; Ground Test; Other Mechanical Engineering; Propulsion and Power

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APA (6th Edition):

Holst, K. R. (2012). A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/1163

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):

Holst, Kevin Raymond. “A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors.” 2012. Thesis, University of Tennessee – Knoxville. Accessed October 22, 2019. https://trace.tennessee.edu/utk_gradthes/1163.

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

MLA Handbook (7th Edition):

Holst, Kevin Raymond. “A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors.” 2012. Web. 22 Oct 2019.

Vancouver:

Holst KR. A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors. [Internet] [Thesis]. University of Tennessee – Knoxville; 2012. [cited 2019 Oct 22]. Available from: https://trace.tennessee.edu/utk_gradthes/1163.

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

Council of Science Editors:

Holst KR. A Method for Performance Analysis of a Ramjet Engine in a Free-jet Test Facility and Analysis of Performance Uncertainty Contributors. [Thesis]. University of Tennessee – Knoxville; 2012. Available from: https://trace.tennessee.edu/utk_gradthes/1163

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


Brno University of Technology

26. Voda, Tomáš. Modelování a řízení leteckých proudových motorů .

Degree: 2017, Brno University of Technology

 Tato práce se zabývá popisem leteckých motorů, jejich požadavky na řízení a možnostmi řízení těchto motorů. V praktické části byl vytvořen model motoru Jetcat P80-SE.… (more)

Subjects/Keywords: Letecké motory; řízení; model motoru; PID; Jetcat; Jet engines; control; engine model; PID; Jetcat

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APA (6th Edition):

Voda, T. (2017). Modelování a řízení leteckých proudových motorů . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/65240

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):

Voda, Tomáš. “Modelování a řízení leteckých proudových motorů .” 2017. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/65240.

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

MLA Handbook (7th Edition):

Voda, Tomáš. “Modelování a řízení leteckých proudových motorů .” 2017. Web. 22 Oct 2019.

Vancouver:

Voda T. Modelování a řízení leteckých proudových motorů . [Internet] [Thesis]. Brno University of Technology; 2017. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/65240.

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

Council of Science Editors:

Voda T. Modelování a řízení leteckých proudových motorů . [Thesis]. Brno University of Technology; 2017. Available from: http://hdl.handle.net/11012/65240

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


University of Toronto

27. Liang, Jason Jian. Design and Development of an Experimental Apparatus to Study Jet Fuel Coking in Small Gas Turbine Fuel Nozzles.

Degree: 2013, University of Toronto

An experimental apparatus was designed and built to study the thermal autoxidative carbon deposition, or coking, in the fuel injection nozzles of small gas turbine… (more)

Subjects/Keywords: jet fuel; fossil fuel; thermal stability; gas turbine; coking; injector nozzle; pressure drop; engine; 0538

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APA (6th Edition):

Liang, J. J. (2013). Design and Development of an Experimental Apparatus to Study Jet Fuel Coking in Small Gas Turbine Fuel Nozzles. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43080

Chicago Manual of Style (16th Edition):

Liang, Jason Jian. “Design and Development of an Experimental Apparatus to Study Jet Fuel Coking in Small Gas Turbine Fuel Nozzles.” 2013. Masters Thesis, University of Toronto. Accessed October 22, 2019. http://hdl.handle.net/1807/43080.

MLA Handbook (7th Edition):

Liang, Jason Jian. “Design and Development of an Experimental Apparatus to Study Jet Fuel Coking in Small Gas Turbine Fuel Nozzles.” 2013. Web. 22 Oct 2019.

Vancouver:

Liang JJ. Design and Development of an Experimental Apparatus to Study Jet Fuel Coking in Small Gas Turbine Fuel Nozzles. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/1807/43080.

Council of Science Editors:

Liang JJ. Design and Development of an Experimental Apparatus to Study Jet Fuel Coking in Small Gas Turbine Fuel Nozzles. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43080


Virginia Tech

28. Siddens, Aaron Jeffrey. A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 This work presents a detailed predictive modeling methodology for comprehensive crashworthiness analysis of advanced jet engine forward sections, containing hybrid and composite structures, when subjected… (more)

Subjects/Keywords: Composite damage; Hybrid structures; Progressive failure; Jet engine forward section; Soft impact

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

APA (6th Edition):

Siddens, A. J. (2012). A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76957

Chicago Manual of Style (16th Edition):

Siddens, Aaron Jeffrey. “A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures.” 2012. Masters Thesis, Virginia Tech. Accessed October 22, 2019. http://hdl.handle.net/10919/76957.

MLA Handbook (7th Edition):

Siddens, Aaron Jeffrey. “A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures.” 2012. Web. 22 Oct 2019.

Vancouver:

Siddens AJ. A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/10919/76957.

Council of Science Editors:

Siddens AJ. A Predictive Methodology for Soft Impact Damage in Jet Engines Incorporating Hybrid Composite Structures. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76957


Loughborough University

29. Carrotte, Jonathan F. The mixing characteristics of dilution jets issuing into a confined cross-flow.

Degree: PhD, 1990, Loughborough University

 An experimental investigation has been carried out into the mixing of a row of jets injected into a confined cross-flow. Measurements were made on a… (more)

Subjects/Keywords: 621.4352; Jet mixing/gas turbine engine

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APA (6th Edition):

Carrotte, J. F. (1990). The mixing characteristics of dilution jets issuing into a confined cross-flow. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/32627

Chicago Manual of Style (16th Edition):

Carrotte, Jonathan F. “The mixing characteristics of dilution jets issuing into a confined cross-flow.” 1990. Doctoral Dissertation, Loughborough University. Accessed October 22, 2019. http://hdl.handle.net/2134/32627.

MLA Handbook (7th Edition):

Carrotte, Jonathan F. “The mixing characteristics of dilution jets issuing into a confined cross-flow.” 1990. Web. 22 Oct 2019.

Vancouver:

Carrotte JF. The mixing characteristics of dilution jets issuing into a confined cross-flow. [Internet] [Doctoral dissertation]. Loughborough University; 1990. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/2134/32627.

Council of Science Editors:

Carrotte JF. The mixing characteristics of dilution jets issuing into a confined cross-flow. [Doctoral Dissertation]. Loughborough University; 1990. Available from: http://hdl.handle.net/2134/32627


Brno University of Technology

30. Mašková, Šárka. Palivo-regulační soustavy leteckých lopatkových motorů .

Degree: 2016, Brno University of Technology

 Tato bakalářská práce se zabývá palivo-regulačními soustavami leteckých lopatkových motorů, konkrétně historickým vývojem těchto soustav včetně přiblížení současných trendů v této oblasti, popisem funkce různých… (more)

Subjects/Keywords: Palivo-regulační jednotka; hydro-mechanický regulátor paliva; elektronický regulátor paliva; FADEC; lopatkový motor; Fuel control unit system; hydro-mechanical engine control unit; electronic engine control unit; FADEC; jet engine

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

APA (6th Edition):

Mašková, . (2016). Palivo-regulační soustavy leteckých lopatkových motorů . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/61027

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):

Mašková, Šárka. “Palivo-regulační soustavy leteckých lopatkových motorů .” 2016. Thesis, Brno University of Technology. Accessed October 22, 2019. http://hdl.handle.net/11012/61027.

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

MLA Handbook (7th Edition):

Mašková, Šárka. “Palivo-regulační soustavy leteckých lopatkových motorů .” 2016. Web. 22 Oct 2019.

Vancouver:

Mašková . Palivo-regulační soustavy leteckých lopatkových motorů . [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2019 Oct 22]. Available from: http://hdl.handle.net/11012/61027.

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

Council of Science Editors:

Mašková . Palivo-regulační soustavy leteckých lopatkových motorů . [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/61027

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

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