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You searched for subject:( aircraft engine). Showing records 1 – 30 of 111 total matches.

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Texas A&M University

1. Jeung, Sung Hwa. Performance of an Open Ends Squeeze Film Damper Operating with Large Amplitude Orbital Motions: Experimental Analysis and Assessment of the Accuracy of the Linearized Force Coefficients Model.

Degree: 2013, Texas A&M University

 Squeeze Film Dampers (SFDs) aid to suppress rotor vibrations and enhance the stability of high-speed rotor-bearing systems. A SFD is a simple oil lubricated film… (more)

Subjects/Keywords: Squeeze Film Damper; Rotordynamics; Aircraft engine

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

APA (6th Edition):

Jeung, S. H. (2013). Performance of an Open Ends Squeeze Film Damper Operating with Large Amplitude Orbital Motions: Experimental Analysis and Assessment of the Accuracy of the Linearized Force Coefficients Model. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151648

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):

Jeung, Sung Hwa. “Performance of an Open Ends Squeeze Film Damper Operating with Large Amplitude Orbital Motions: Experimental Analysis and Assessment of the Accuracy of the Linearized Force Coefficients Model.” 2013. Thesis, Texas A&M University. Accessed December 15, 2019. http://hdl.handle.net/1969.1/151648.

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

MLA Handbook (7th Edition):

Jeung, Sung Hwa. “Performance of an Open Ends Squeeze Film Damper Operating with Large Amplitude Orbital Motions: Experimental Analysis and Assessment of the Accuracy of the Linearized Force Coefficients Model.” 2013. Web. 15 Dec 2019.

Vancouver:

Jeung SH. Performance of an Open Ends Squeeze Film Damper Operating with Large Amplitude Orbital Motions: Experimental Analysis and Assessment of the Accuracy of the Linearized Force Coefficients Model. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/1969.1/151648.

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

Council of Science Editors:

Jeung SH. Performance of an Open Ends Squeeze Film Damper Operating with Large Amplitude Orbital Motions: Experimental Analysis and Assessment of the Accuracy of the Linearized Force Coefficients Model. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151648

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


Cranfield University

2. Navaratne, Rukshan. Investigation of impact of engine degradation on optimum aircraft trajectories.

Degree: PhD, 2016, Cranfield University

 The continuous growth in flight operations has led to public concern regarding the impact of aviation on the environment with its anthropogenic contribution to global… (more)

Subjects/Keywords: Engine Performance Degradation; Aircraft Emissions; Trajectory Optimisation

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APA (6th Edition):

Navaratne, R. (2016). Investigation of impact of engine degradation on optimum aircraft trajectories. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/12296

Chicago Manual of Style (16th Edition):

Navaratne, Rukshan. “Investigation of impact of engine degradation on optimum aircraft trajectories.” 2016. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/12296.

MLA Handbook (7th Edition):

Navaratne, Rukshan. “Investigation of impact of engine degradation on optimum aircraft trajectories.” 2016. Web. 15 Dec 2019.

Vancouver:

Navaratne R. Investigation of impact of engine degradation on optimum aircraft trajectories. [Internet] [Doctoral dissertation]. Cranfield University; 2016. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12296.

Council of Science Editors:

Navaratne R. Investigation of impact of engine degradation on optimum aircraft trajectories. [Doctoral Dissertation]. Cranfield University; 2016. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12296


Brno University of Technology

3. Růžička, Martin. Invertní letadlové motory .

Degree: 2016, Brno University of Technology

 Tato práce pojednává o invertních letadlových motorech. V úvodu je zařazen přehled obecných požadavků kladených na letadlové motory, jejich rozdělení a základní informace o invertní… (more)

Subjects/Keywords: Letadlový motor; invertní motor; konstrukce; Aircraft engine; inverted engine; construction

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APA (6th Edition):

Růžička, M. (2016). Invertní letadlové motory . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/60123

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):

Růžička, Martin. “Invertní letadlové motory .” 2016. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/60123.

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

MLA Handbook (7th Edition):

Růžička, Martin. “Invertní letadlové motory .” 2016. Web. 15 Dec 2019.

Vancouver:

Růžička M. Invertní letadlové motory . [Internet] [Thesis]. Brno University of Technology; 2016. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/60123.

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

Council of Science Editors:

Růžička M. Invertní letadlové motory . [Thesis]. Brno University of Technology; 2016. Available from: http://hdl.handle.net/11012/60123

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


Brno University of Technology

4. Süttő, Daniel. Vývoj motorů BMW .

Degree: 2011, Brno University of Technology

 Táto bakalárska práca s názvom „Vývoj motorů BMW“, pojednáva o histórií vzniku lietadlových motorov a motorov pre jednostopové vozidlá závodu BMW. Poskytuje prehľad konštrukčných riešení… (more)

Subjects/Keywords: Motor; BMW; lietadlový motor; motocykel; výkon; zdvihový objem motora; valec.; Engine; BMW; aircraft engine; motorcycle; power; engine cylinder capacity; cylinder.

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APA (6th Edition):

Süttő, D. (2011). Vývoj motorů BMW . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/6230

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):

Süttő, Daniel. “Vývoj motorů BMW .” 2011. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/6230.

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

MLA Handbook (7th Edition):

Süttő, Daniel. “Vývoj motorů BMW .” 2011. Web. 15 Dec 2019.

Vancouver:

Süttő D. Vývoj motorů BMW . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/6230.

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

Council of Science Editors:

Süttő D. Vývoj motorů BMW . [Thesis]. Brno University of Technology; 2011. Available from: http://hdl.handle.net/11012/6230

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


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 December 15, 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. 15 Dec 2019.

Vancouver:

Heczko N. Letecké proudové motory s proměnným cyklem . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Dec 15]. 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


Brno University of Technology

6. Puller, Tomáš. Remotorizace letounu EV-55 Outback .

Degree: 2011, Brno University of Technology

 Práce Remotorizace letounu EV-55 se zabývá možností náhrady tubrovrtulového motoru PT6A-21 pístovým vznětovým motorem. Je proveden výběr vhodného motoru a vrtule a vytvořen 3D model… (more)

Subjects/Keywords: Remotorizace; Vznětový motor; Dvoumotorový letoun; Motorové lože; Letové výkony; Remotorization; Diesel engine; Twin engine aircraft; Engine bed; Flight performances

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APA (6th Edition):

Puller, T. (2011). Remotorizace letounu EV-55 Outback . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/4010

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):

Puller, Tomáš. “Remotorizace letounu EV-55 Outback .” 2011. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/4010.

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

MLA Handbook (7th Edition):

Puller, Tomáš. “Remotorizace letounu EV-55 Outback .” 2011. Web. 15 Dec 2019.

Vancouver:

Puller T. Remotorizace letounu EV-55 Outback . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/4010.

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

Council of Science Editors:

Puller T. Remotorizace letounu EV-55 Outback . [Thesis]. Brno University of Technology; 2011. Available from: http://hdl.handle.net/11012/4010

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


The Ohio State University

7. Li, Wenfei. Fault Diagnostics Study for Linear Uncertain Systems Using Dynamic Threshold with Application to Propulsion System.

Degree: PhD, Aero/Astro Engineering, 2010, The Ohio State University

 Fault detection and isolation plays a critical role in aircraft engines and the performance of their control systems. A great amount of research on model-based… (more)

Subjects/Keywords: Engineering; aircraft engine; dynamic threshold; fault diagnostics; FDI; linear uncertain system

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APA (6th Edition):

Li, W. (2010). Fault Diagnostics Study for Linear Uncertain Systems Using Dynamic Threshold with Application to Propulsion System. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1284971383

Chicago Manual of Style (16th Edition):

Li, Wenfei. “Fault Diagnostics Study for Linear Uncertain Systems Using Dynamic Threshold with Application to Propulsion System.” 2010. Doctoral Dissertation, The Ohio State University. Accessed December 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1284971383.

MLA Handbook (7th Edition):

Li, Wenfei. “Fault Diagnostics Study for Linear Uncertain Systems Using Dynamic Threshold with Application to Propulsion System.” 2010. Web. 15 Dec 2019.

Vancouver:

Li W. Fault Diagnostics Study for Linear Uncertain Systems Using Dynamic Threshold with Application to Propulsion System. [Internet] [Doctoral dissertation]. The Ohio State University; 2010. [cited 2019 Dec 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1284971383.

Council of Science Editors:

Li W. Fault Diagnostics Study for Linear Uncertain Systems Using Dynamic Threshold with Application to Propulsion System. [Doctoral Dissertation]. The Ohio State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1284971383


Universidade Nova

8. Batalha, Euclides da Conceição Pereira. Aircraft Engines Maintenance Costs and Reliability: An Appraisal of the Decision Process to Remove an Engine for a Shop Visit Aiming at Minimum Maintenance Unit Cost.

Degree: 2012, Universidade Nova

Dissertação apresentada como requisito parcial para obtenção do grau de Mestre em Estatística e Gestão de Informação.

The decision to remove an aircraft engine for… (more)

Subjects/Keywords: Aircraft engine; Reliability; Maintenance cost; Optimizing time on-wing

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APA (6th Edition):

Batalha, E. d. C. P. (2012). Aircraft Engines Maintenance Costs and Reliability: An Appraisal of the Decision Process to Remove an Engine for a Shop Visit Aiming at Minimum Maintenance Unit Cost. (Thesis). Universidade Nova. Retrieved from http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/8792

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):

Batalha, Euclides da Conceição Pereira. “Aircraft Engines Maintenance Costs and Reliability: An Appraisal of the Decision Process to Remove an Engine for a Shop Visit Aiming at Minimum Maintenance Unit Cost.” 2012. Thesis, Universidade Nova. Accessed December 15, 2019. http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/8792.

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

MLA Handbook (7th Edition):

Batalha, Euclides da Conceição Pereira. “Aircraft Engines Maintenance Costs and Reliability: An Appraisal of the Decision Process to Remove an Engine for a Shop Visit Aiming at Minimum Maintenance Unit Cost.” 2012. Web. 15 Dec 2019.

Vancouver:

Batalha EdCP. Aircraft Engines Maintenance Costs and Reliability: An Appraisal of the Decision Process to Remove an Engine for a Shop Visit Aiming at Minimum Maintenance Unit Cost. [Internet] [Thesis]. Universidade Nova; 2012. [cited 2019 Dec 15]. Available from: http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/8792.

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

Council of Science Editors:

Batalha EdCP. Aircraft Engines Maintenance Costs and Reliability: An Appraisal of the Decision Process to Remove an Engine for a Shop Visit Aiming at Minimum Maintenance Unit Cost. [Thesis]. Universidade Nova; 2012. Available from: http://www.rcaap.pt/detail.jsp?id=oai:run.unl.pt:10362/8792

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


Cranfield University

9. Venediger, Benjamin. Civil aircraft trajectory analyses - impact of engine degradation on fuel burn and emissions.

Degree: MSc by Research, 2013, Cranfield University

 Commercial aviation and air traffic is still expected to grow by 4-5% annually in the future and thus the effect of aircraft operation on the… (more)

Subjects/Keywords: Aircraft Trajectory; Engine Degradation; Fuel Burn; Emissions; Optimisation

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APA (6th Edition):

Venediger, B. (2013). Civil aircraft trajectory analyses - impact of engine degradation on fuel burn and emissions. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/9156

Chicago Manual of Style (16th Edition):

Venediger, Benjamin. “Civil aircraft trajectory analyses - impact of engine degradation on fuel burn and emissions.” 2013. Masters Thesis, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/9156.

MLA Handbook (7th Edition):

Venediger, Benjamin. “Civil aircraft trajectory analyses - impact of engine degradation on fuel burn and emissions.” 2013. Web. 15 Dec 2019.

Vancouver:

Venediger B. Civil aircraft trajectory analyses - impact of engine degradation on fuel burn and emissions. [Internet] [Masters thesis]. Cranfield University; 2013. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9156.

Council of Science Editors:

Venediger B. Civil aircraft trajectory analyses - impact of engine degradation on fuel burn and emissions. [Masters Thesis]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9156


University of Akron

10. Kline, Sara E. An Investigation of the Performance of Compliant Finger Seals for use in Gas Turbine Engines using Navier-Stokes and Reynolds Equation Based Numerical Models and Experimental Evaluation.

Degree: PhD, Mechanical Engineering, 2016, University of Akron

 This work analyzed the performance of two foot pad designs for the compliant finger seal. The double wedge and Rayleigh step pad designs were tested… (more)

Subjects/Keywords: Mechanical Engineering; gas turbines; finger seals; turbomachinery; aircraft engine seals

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APA (6th Edition):

Kline, S. E. (2016). An Investigation of the Performance of Compliant Finger Seals for use in Gas Turbine Engines using Navier-Stokes and Reynolds Equation Based Numerical Models and Experimental Evaluation. (Doctoral Dissertation). University of Akron. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=akron1478984223281402

Chicago Manual of Style (16th Edition):

Kline, Sara E. “An Investigation of the Performance of Compliant Finger Seals for use in Gas Turbine Engines using Navier-Stokes and Reynolds Equation Based Numerical Models and Experimental Evaluation.” 2016. Doctoral Dissertation, University of Akron. Accessed December 15, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=akron1478984223281402.

MLA Handbook (7th Edition):

Kline, Sara E. “An Investigation of the Performance of Compliant Finger Seals for use in Gas Turbine Engines using Navier-Stokes and Reynolds Equation Based Numerical Models and Experimental Evaluation.” 2016. Web. 15 Dec 2019.

Vancouver:

Kline SE. An Investigation of the Performance of Compliant Finger Seals for use in Gas Turbine Engines using Navier-Stokes and Reynolds Equation Based Numerical Models and Experimental Evaluation. [Internet] [Doctoral dissertation]. University of Akron; 2016. [cited 2019 Dec 15]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=akron1478984223281402.

Council of Science Editors:

Kline SE. An Investigation of the Performance of Compliant Finger Seals for use in Gas Turbine Engines using Navier-Stokes and Reynolds Equation Based Numerical Models and Experimental Evaluation. [Doctoral Dissertation]. University of Akron; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=akron1478984223281402


Cranfield University

11. Navaratne, Rukshan. Investigation of impact of engine degradation on optimum aircraft trajectories.

Degree: PhD, 2016, Cranfield University

 The continuous growth in flight operations has led to public concern regarding the impact of aviation on the environment with its anthropogenic contribution to global… (more)

Subjects/Keywords: 629.134; Engine Performance Degradation; Aircraft Emissions; Trajectory Optimisation

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

APA (6th Edition):

Navaratne, R. (2016). Investigation of impact of engine degradation on optimum aircraft trajectories. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/12296 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720967

Chicago Manual of Style (16th Edition):

Navaratne, Rukshan. “Investigation of impact of engine degradation on optimum aircraft trajectories.” 2016. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/12296 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720967.

MLA Handbook (7th Edition):

Navaratne, Rukshan. “Investigation of impact of engine degradation on optimum aircraft trajectories.” 2016. Web. 15 Dec 2019.

Vancouver:

Navaratne R. Investigation of impact of engine degradation on optimum aircraft trajectories. [Internet] [Doctoral dissertation]. Cranfield University; 2016. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12296 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720967.

Council of Science Editors:

Navaratne R. Investigation of impact of engine degradation on optimum aircraft trajectories. [Doctoral Dissertation]. Cranfield University; 2016. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/12296 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.720967


University of Connecticut

12. Hacker, Jennifer. L1 Adaptive Control of Uncertain Nonlinear Systems with Dynamic Constraints: As Applied to Commercial Aircraft Engines.

Degree: MS, Mechanical Engineering, 2011, University of Connecticut

  L1 adaptive control for a turbofan commercial aircraft engine is developed and applied in the presences of constraint limits. Turbofan engines are a highly… (more)

Subjects/Keywords: Adaptive Control; Aircraft Engine; nonlinear; robust; adaptation; limits

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APA (6th Edition):

Hacker, J. (2011). L1 Adaptive Control of Uncertain Nonlinear Systems with Dynamic Constraints: As Applied to Commercial Aircraft Engines. (Masters Thesis). University of Connecticut. Retrieved from https://opencommons.uconn.edu/gs_theses/128

Chicago Manual of Style (16th Edition):

Hacker, Jennifer. “L1 Adaptive Control of Uncertain Nonlinear Systems with Dynamic Constraints: As Applied to Commercial Aircraft Engines.” 2011. Masters Thesis, University of Connecticut. Accessed December 15, 2019. https://opencommons.uconn.edu/gs_theses/128.

MLA Handbook (7th Edition):

Hacker, Jennifer. “L1 Adaptive Control of Uncertain Nonlinear Systems with Dynamic Constraints: As Applied to Commercial Aircraft Engines.” 2011. Web. 15 Dec 2019.

Vancouver:

Hacker J. L1 Adaptive Control of Uncertain Nonlinear Systems with Dynamic Constraints: As Applied to Commercial Aircraft Engines. [Internet] [Masters thesis]. University of Connecticut; 2011. [cited 2019 Dec 15]. Available from: https://opencommons.uconn.edu/gs_theses/128.

Council of Science Editors:

Hacker J. L1 Adaptive Control of Uncertain Nonlinear Systems with Dynamic Constraints: As Applied to Commercial Aircraft Engines. [Masters Thesis]. University of Connecticut; 2011. Available from: https://opencommons.uconn.edu/gs_theses/128


Cranfield University

13. Al-Akam, Aws Akram Mahmood. Modelling the aerodynamics of an aero-engine exhaust system.

Degree: 2018, Cranfield University

 Aero-engine design is one of the most demanding tasks when the aircraft is constructed. The selection of the engine component’s size and geometrical features depends… (more)

Subjects/Keywords: Propelling-nozzle; nozzle performance metrics; nozzle parameterisation; engine-aircraft aerodynamic interference

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APA (6th Edition):

Al-Akam, A. A. M. (2018). Modelling the aerodynamics of an aero-engine exhaust system. (Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/14356

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):

Al-Akam, Aws Akram Mahmood. “Modelling the aerodynamics of an aero-engine exhaust system.” 2018. Thesis, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/14356.

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

MLA Handbook (7th Edition):

Al-Akam, Aws Akram Mahmood. “Modelling the aerodynamics of an aero-engine exhaust system.” 2018. Web. 15 Dec 2019.

Vancouver:

Al-Akam AAM. Modelling the aerodynamics of an aero-engine exhaust system. [Internet] [Thesis]. Cranfield University; 2018. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14356.

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

Council of Science Editors:

Al-Akam AAM. Modelling the aerodynamics of an aero-engine exhaust system. [Thesis]. Cranfield University; 2018. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14356

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


Cranfield University

14. Al-Akam, Aws Akram Mahmood. Modelling the aerodynamics of an aero-engine exhaust system.

Degree: PhD, 2018, Cranfield University

 Aero-engine design is one of the most demanding tasks when the aircraft is constructed. The selection of the engine component's size and geometrical features depends… (more)

Subjects/Keywords: Propelling-nozzle; nozzle performance metrics; nozzle parameterisation; engine-aircraft aerodynamic interference

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

APA (6th Edition):

Al-Akam, A. A. M. (2018). Modelling the aerodynamics of an aero-engine exhaust system. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/14356 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783284

Chicago Manual of Style (16th Edition):

Al-Akam, Aws Akram Mahmood. “Modelling the aerodynamics of an aero-engine exhaust system.” 2018. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/14356 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783284.

MLA Handbook (7th Edition):

Al-Akam, Aws Akram Mahmood. “Modelling the aerodynamics of an aero-engine exhaust system.” 2018. Web. 15 Dec 2019.

Vancouver:

Al-Akam AAM. Modelling the aerodynamics of an aero-engine exhaust system. [Internet] [Doctoral dissertation]. Cranfield University; 2018. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14356 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783284.

Council of Science Editors:

Al-Akam AAM. Modelling the aerodynamics of an aero-engine exhaust system. [Doctoral Dissertation]. Cranfield University; 2018. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/14356 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.783284


Brno University of Technology

15. Bauer, Martin. Koncepce uspořádání pohonné jednotky na letounu .

Degree: 2012, Brno University of Technology

 Tato bakalářská práce se zabývá koncepcemi umístění pohonných jednotek na letounech. Je zde vytvořen přehled uspořádání pohonných jednotek v jednotlivých kategoriích letounů. V práci jsou… (more)

Subjects/Keywords: Koncepce uspořádání pohonné jednotky na letounu; umístění motoru na letounu; letadlový motor; letecký motor.; Location of the engine on aircraft; placing of the engine on aircraft; power unit arrangement on aircraft; aircraft engine; aircraft power unit.

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

APA (6th Edition):

Bauer, M. (2012). Koncepce uspořádání pohonné jednotky na letounu . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/5712

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):

Bauer, Martin. “Koncepce uspořádání pohonné jednotky na letounu .” 2012. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/5712.

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

MLA Handbook (7th Edition):

Bauer, Martin. “Koncepce uspořádání pohonné jednotky na letounu .” 2012. Web. 15 Dec 2019.

Vancouver:

Bauer M. Koncepce uspořádání pohonné jednotky na letounu . [Internet] [Thesis]. Brno University of Technology; 2012. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/5712.

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

Council of Science Editors:

Bauer M. Koncepce uspořádání pohonné jednotky na letounu . [Thesis]. Brno University of Technology; 2012. Available from: http://hdl.handle.net/11012/5712

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


Brno University of Technology

16. Pochop, Ladislav. Dvoudobé vznětové letecké motory .

Degree: 2010, Brno University of Technology

 Tato bakalářská práce je pojednáním o dvoudobých vznětových leteckých motorech. Popisuje princip funkce dvoudobého vznětového motoru, jeho odlišnosti od motoru čtyřdobého a motoru zážehového. Dále… (more)

Subjects/Keywords: Letecký motor; pístový motor; dvoudobý motor; vznětový motor; dieselový motor.; Aircraft engine; piston engine; two-stroke engine; compression-ignition engine; diesel engine.

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APA (6th Edition):

Pochop, L. (2010). Dvoudobé vznětové letecké motory . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/15525

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):

Pochop, Ladislav. “Dvoudobé vznětové letecké motory .” 2010. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/15525.

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

MLA Handbook (7th Edition):

Pochop, Ladislav. “Dvoudobé vznětové letecké motory .” 2010. Web. 15 Dec 2019.

Vancouver:

Pochop L. Dvoudobé vznětové letecké motory . [Internet] [Thesis]. Brno University of Technology; 2010. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/15525.

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

Council of Science Editors:

Pochop L. Dvoudobé vznětové letecké motory . [Thesis]. Brno University of Technology; 2010. Available from: http://hdl.handle.net/11012/15525

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


RMIT University

17. Anele, O. Atmospheric lead monitoring at Moorabbin Airport, Melbourne, Australia.

Degree: 2016, RMIT University

 There is ample evidence to show that any lead in the atmosphere affects human beings to some degree. Consequently, the use of leaded fuel was… (more)

Subjects/Keywords: Fields of Research; Lead; Piston engine; Aircraft; Modelling; High volume sampling; Air pollution

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APA (6th Edition):

Anele, O. (2016). Atmospheric lead monitoring at Moorabbin Airport, Melbourne, Australia. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:161625

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):

Anele, O. “Atmospheric lead monitoring at Moorabbin Airport, Melbourne, Australia.” 2016. Thesis, RMIT University. Accessed December 15, 2019. http://researchbank.rmit.edu.au/view/rmit:161625.

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

MLA Handbook (7th Edition):

Anele, O. “Atmospheric lead monitoring at Moorabbin Airport, Melbourne, Australia.” 2016. Web. 15 Dec 2019.

Vancouver:

Anele O. Atmospheric lead monitoring at Moorabbin Airport, Melbourne, Australia. [Internet] [Thesis]. RMIT University; 2016. [cited 2019 Dec 15]. Available from: http://researchbank.rmit.edu.au/view/rmit:161625.

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

Council of Science Editors:

Anele O. Atmospheric lead monitoring at Moorabbin Airport, Melbourne, Australia. [Thesis]. RMIT University; 2016. Available from: http://researchbank.rmit.edu.au/view/rmit:161625

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

18. Lokesh, Kadambari. Techno-economic environmental risk analysis of advanced biofuels for civil aviation.

Degree: PhD, 2015, Cranfield University

 Commercial aviation has demonstrated its ability to be a key driver of global socio-economic growth to this date. This growth, resulting from an ever increasing… (more)

Subjects/Keywords: 629.134; Bio-Synthetic Paraffinic Kerosene; Life Cycle Assessment; Thermodynamics; Engine/Aircraft analysis; DOC

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

APA (6th Edition):

Lokesh, K. (2015). Techno-economic environmental risk analysis of advanced biofuels for civil aviation. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/9243 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.650164

Chicago Manual of Style (16th Edition):

Lokesh, Kadambari. “Techno-economic environmental risk analysis of advanced biofuels for civil aviation.” 2015. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/9243 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.650164.

MLA Handbook (7th Edition):

Lokesh, Kadambari. “Techno-economic environmental risk analysis of advanced biofuels for civil aviation.” 2015. Web. 15 Dec 2019.

Vancouver:

Lokesh K. Techno-economic environmental risk analysis of advanced biofuels for civil aviation. [Internet] [Doctoral dissertation]. Cranfield University; 2015. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9243 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.650164.

Council of Science Editors:

Lokesh K. Techno-economic environmental risk analysis of advanced biofuels for civil aviation. [Doctoral Dissertation]. Cranfield University; 2015. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9243 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.650164


Linköping University

19. Sandvik, Gustav. Estimation of Engine Inlet Air Temperature in Fighter Aircraft.

Degree: Automatic Control, 2018, Linköping University

An accurate estimate of the gasturbine inlet air temperature is essential to the stability of the engine since its control depends on it. Most… (more)

Subjects/Keywords: system identification; grey box modeling; engine inlet temperature; heat transfer; fighter aircraft; Control Engineering; Reglerteknik

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APA (6th Edition):

Sandvik, G. (2018). Estimation of Engine Inlet Air Temperature in Fighter Aircraft. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149557

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):

Sandvik, Gustav. “Estimation of Engine Inlet Air Temperature in Fighter Aircraft.” 2018. Thesis, Linköping University. Accessed December 15, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149557.

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

MLA Handbook (7th Edition):

Sandvik, Gustav. “Estimation of Engine Inlet Air Temperature in Fighter Aircraft.” 2018. Web. 15 Dec 2019.

Vancouver:

Sandvik G. Estimation of Engine Inlet Air Temperature in Fighter Aircraft. [Internet] [Thesis]. Linköping University; 2018. [cited 2019 Dec 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149557.

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

Council of Science Editors:

Sandvik G. Estimation of Engine Inlet Air Temperature in Fighter Aircraft. [Thesis]. Linköping University; 2018. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-149557

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

20. Lokesh, Kadambari. Techno-economic environmental risk analysis of advanced biofuels for civil aviation.

Degree: PhD, 2015, Cranfield University

 Commercial aviation has demonstrated its ability to be a key driver of global socio-economic growth to this date. This growth, resulting from an ever increasing… (more)

Subjects/Keywords: Bio-Synthetic Paraffinic Kerosene; Life Cycle Assessment; Thermodynamics; Engine/Aircraft analysis; DOC

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

APA (6th Edition):

Lokesh, K. (2015). Techno-economic environmental risk analysis of advanced biofuels for civil aviation. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/9243

Chicago Manual of Style (16th Edition):

Lokesh, Kadambari. “Techno-economic environmental risk analysis of advanced biofuels for civil aviation.” 2015. Doctoral Dissertation, Cranfield University. Accessed December 15, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/9243.

MLA Handbook (7th Edition):

Lokesh, Kadambari. “Techno-economic environmental risk analysis of advanced biofuels for civil aviation.” 2015. Web. 15 Dec 2019.

Vancouver:

Lokesh K. Techno-economic environmental risk analysis of advanced biofuels for civil aviation. [Internet] [Doctoral dissertation]. Cranfield University; 2015. [cited 2019 Dec 15]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9243.

Council of Science Editors:

Lokesh K. Techno-economic environmental risk analysis of advanced biofuels for civil aviation. [Doctoral Dissertation]. Cranfield University; 2015. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/9243


Luleå University of Technology

21. Hozic, Dzenan. Mechanical loads on a turbofan engine structure at blade-off.

Degree: 2009, Luleå University of Technology

Aircraft engine development is an expensive and time consuming business. The engines have to be designed to withstand loads well above those encountered during… (more)

Subjects/Keywords: Technology; rotor dynamics; turbofan model; FBO; fan blade-off; mechanical; loads; aircraft engine; Teknik

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APA (6th Edition):

Hozic, D. (2009). Mechanical loads on a turbofan engine structure at blade-off. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56753

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):

Hozic, Dzenan. “Mechanical loads on a turbofan engine structure at blade-off.” 2009. Thesis, Luleå University of Technology. Accessed December 15, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56753.

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

MLA Handbook (7th Edition):

Hozic, Dzenan. “Mechanical loads on a turbofan engine structure at blade-off.” 2009. Web. 15 Dec 2019.

Vancouver:

Hozic D. Mechanical loads on a turbofan engine structure at blade-off. [Internet] [Thesis]. Luleå University of Technology; 2009. [cited 2019 Dec 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56753.

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

Council of Science Editors:

Hozic D. Mechanical loads on a turbofan engine structure at blade-off. [Thesis]. Luleå University of Technology; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-56753

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


Brno University of Technology

22. Novák, Lukáš. Návrh reduktoru zážehového šestiválcového leteckého motoru .

Degree: 2013, Brno University of Technology

 Práce se zabývá návrhem reduktoru pro šestiválcový letecký motor. Jsou zde zpracovány jednotlivé součásti reduktoru a následně jako sestava s klikovým hřídelem je řešeno torzní… (more)

Subjects/Keywords: Reduktor; ozubené; soukolí; kolo; hřídel; letecký; motor; Reducer; gearbox; gear; shaft; aircraft; engine

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APA (6th Edition):

Novák, L. (2013). Návrh reduktoru zážehového šestiválcového leteckého motoru . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/20359

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):

Novák, Lukáš. “Návrh reduktoru zážehového šestiválcového leteckého motoru .” 2013. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/20359.

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

MLA Handbook (7th Edition):

Novák, Lukáš. “Návrh reduktoru zážehového šestiválcového leteckého motoru .” 2013. Web. 15 Dec 2019.

Vancouver:

Novák L. Návrh reduktoru zážehového šestiválcového leteckého motoru . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/20359.

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

Council of Science Editors:

Novák L. Návrh reduktoru zážehového šestiválcového leteckého motoru . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/20359

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


Brno University of Technology

23. Vaněk, Václav. Ojnice leteckého motoru .

Degree: 2012, Brno University of Technology

 Tato bakalářská práce se zabývá návrhem uspořádání ojnic plochého leteckého motoru. Součástí práce je návrh základních rozměrů vnitřní a rozvidlené ojnice společně se stanovením průběhu… (more)

Subjects/Keywords: Ojnice; plochý letecký motor; pevnostní kontrola; Piston rod; flat aircraft engine; strength test

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APA (6th Edition):

Vaněk, V. (2012). Ojnice leteckého motoru . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/7847

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):

Vaněk, Václav. “Ojnice leteckého motoru .” 2012. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/7847.

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

MLA Handbook (7th Edition):

Vaněk, Václav. “Ojnice leteckého motoru .” 2012. Web. 15 Dec 2019.

Vancouver:

Vaněk V. Ojnice leteckého motoru . [Internet] [Thesis]. Brno University of Technology; 2012. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/7847.

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

Council of Science Editors:

Vaněk V. Ojnice leteckého motoru . [Thesis]. Brno University of Technology; 2012. Available from: http://hdl.handle.net/11012/7847

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


Brno University of Technology

24. Durchan, Vladimír. Současné trendy ve vývoji leteckých pohonných jednotek .

Degree: 2014, Brno University of Technology

 Tato bakalářská práce popisuje současné trendy a novinky ve vývoji leteckých pohonných jednotek, jejich aplikaci v současnosti vyráběných leteckých pohonných jednotkách. Jednotlivá konstrukční řešení vyplývajících… (more)

Subjects/Keywords: Letecká pohonná jednotka; letecký motor; trend; vývoj; Aicraft powerplant; aircraft engine; trend; development

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APA (6th Edition):

Durchan, V. (2014). Současné trendy ve vývoji leteckých pohonných jednotek . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33495

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):

Durchan, Vladimír. “Současné trendy ve vývoji leteckých pohonných jednotek .” 2014. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/33495.

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

MLA Handbook (7th Edition):

Durchan, Vladimír. “Současné trendy ve vývoji leteckých pohonných jednotek .” 2014. Web. 15 Dec 2019.

Vancouver:

Durchan V. Současné trendy ve vývoji leteckých pohonných jednotek . [Internet] [Thesis]. Brno University of Technology; 2014. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/33495.

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

Council of Science Editors:

Durchan V. Současné trendy ve vývoji leteckých pohonných jednotek . [Thesis]. Brno University of Technology; 2014. Available from: http://hdl.handle.net/11012/33495

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


Brno University of Technology

25. Josefíková, Kateřina. Návrh klikového mechanismu leteckého vznětového motoru .

Degree: 2010, Brno University of Technology

 Cílem této diplomové práce je návrh klikového mechanismu pro vznětový letecký motor. Dále pak vhodné vyvážení klikového mechanismu, pevnostní kontrola klikového hřídele a výpočet torzních… (more)

Subjects/Keywords: letecký motor; klikový hřídel; vyvažování; torzní kmitání; aircraft engine; crankshaft; balancing; torsion vabration

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APA (6th Edition):

Josefíková, K. (2010). Návrh klikového mechanismu leteckého vznětového motoru . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/16926

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):

Josefíková, Kateřina. “Návrh klikového mechanismu leteckého vznětového motoru .” 2010. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/16926.

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

MLA Handbook (7th Edition):

Josefíková, Kateřina. “Návrh klikového mechanismu leteckého vznětového motoru .” 2010. Web. 15 Dec 2019.

Vancouver:

Josefíková K. Návrh klikového mechanismu leteckého vznětového motoru . [Internet] [Thesis]. Brno University of Technology; 2010. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/16926.

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

Council of Science Editors:

Josefíková K. Návrh klikového mechanismu leteckého vznětového motoru . [Thesis]. Brno University of Technology; 2010. Available from: http://hdl.handle.net/11012/16926

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

26. Magoha, Paul W. Incident-response monitoring technologies for aircraft-cabin air quality.

Degree: PhD, Department of Mechanical Engineering, 2012, Kansas State University

 Poor air quality in commercial aircraft cabins can be caused by volatile organophosphorus (OP) compounds emitted from the jet engine bleed air system during smoke/fume… (more)

Subjects/Keywords: Smoke/fume incidents; Jet engine oils; Aircraft-cabin air quality; Tri-cresyl phosphate isomers; Aircraft-bleed air simulator; Aircraft-cabin air recirculation filters; Engineering (0537)

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

APA (6th Edition):

Magoha, P. W. (2012). Incident-response monitoring technologies for aircraft-cabin air quality. (Doctoral Dissertation). Kansas State University. Retrieved from http://hdl.handle.net/2097/14187

Chicago Manual of Style (16th Edition):

Magoha, Paul W. “Incident-response monitoring technologies for aircraft-cabin air quality.” 2012. Doctoral Dissertation, Kansas State University. Accessed December 15, 2019. http://hdl.handle.net/2097/14187.

MLA Handbook (7th Edition):

Magoha, Paul W. “Incident-response monitoring technologies for aircraft-cabin air quality.” 2012. Web. 15 Dec 2019.

Vancouver:

Magoha PW. Incident-response monitoring technologies for aircraft-cabin air quality. [Internet] [Doctoral dissertation]. Kansas State University; 2012. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/2097/14187.

Council of Science Editors:

Magoha PW. Incident-response monitoring technologies for aircraft-cabin air quality. [Doctoral Dissertation]. Kansas State University; 2012. Available from: http://hdl.handle.net/2097/14187


Brno University of Technology

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

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 December 15, 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. 15 Dec 2019.

Vancouver:

Trusík V. Zkoušení leteckých proudových motorů . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2019 Dec 15]. 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


Brno University of Technology

28. Harasim, Tomáš. Možnosti zmenšení spotřeby paliva dopravných letadel .

Degree: 2013, Brno University of Technology

 V důsledku dlouhodobé ekonomické krize se v posledních letech zavádějí různá úsporná opatření. Vyjímkou není ani letecké odvětví. Z tohoto důvodu se v této práci… (more)

Subjects/Keywords: Spotřeba letadla; historie letectví; letecké palivové soustavy; letový režim; metody snižování spotřeby paliva; letecký motor; proudový motor.; Fuel consumption of aircraft; aircraft history; aisrcraft fuel systems; flight mode; possibilities of reduction of airliners fuel consumption; aircraft engine; turbojet engine.

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

APA (6th Edition):

Harasim, T. (2013). Možnosti zmenšení spotřeby paliva dopravných letadel . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/26699

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):

Harasim, Tomáš. “Možnosti zmenšení spotřeby paliva dopravných letadel .” 2013. Thesis, Brno University of Technology. Accessed December 15, 2019. http://hdl.handle.net/11012/26699.

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

MLA Handbook (7th Edition):

Harasim, Tomáš. “Možnosti zmenšení spotřeby paliva dopravných letadel .” 2013. Web. 15 Dec 2019.

Vancouver:

Harasim T. Možnosti zmenšení spotřeby paliva dopravných letadel . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Dec 15]. Available from: http://hdl.handle.net/11012/26699.

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

Council of Science Editors:

Harasim T. Možnosti zmenšení spotřeby paliva dopravných letadel . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/26699

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

29. Roskvist, Jimmy. Konceptframtagning av inspektionspluggar till flygmotorer.

Degree: Engineering Science, 2009, University West

  This report describes the results of the project "Concept development of jet engine inspection plugs" carried out in the spring of 2008. The work… (more)

Subjects/Keywords: Inspection plug; aircraft engine; QFD; FMEA; Production Engineering, Human Work Science and Ergonomics; Produktionsteknik, arbetsvetenskap och ergonomi

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

APA (6th Edition):

Roskvist, J. (2009). Konceptframtagning av inspektionspluggar till flygmotorer. (Thesis). University West. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1634

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):

Roskvist, Jimmy. “Konceptframtagning av inspektionspluggar till flygmotorer.” 2009. Thesis, University West. Accessed December 15, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1634.

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

MLA Handbook (7th Edition):

Roskvist, Jimmy. “Konceptframtagning av inspektionspluggar till flygmotorer.” 2009. Web. 15 Dec 2019.

Vancouver:

Roskvist J. Konceptframtagning av inspektionspluggar till flygmotorer. [Internet] [Thesis]. University West; 2009. [cited 2019 Dec 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1634.

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

Council of Science Editors:

Roskvist J. Konceptframtagning av inspektionspluggar till flygmotorer. [Thesis]. University West; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1634

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

30. Hansson, Anders. Flygplanstillverkning : Fixturkoncept till robotgradning.

Degree: Engineering Science, 2009, University West

Volvo Aeros flygmotortillverkning i Trollhättan har infört ett antal nya detaljvarianter i produktionen. Detta har medfört att den robotcell som är avsedd att utföra… (more)

Subjects/Keywords: Deburring; robot; concept generation; fixture; volvo aero; aircraft engine; Fixtur; robotcell; gradning; flygmotor; volvo aero; konceptgenerering

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

APA (6th Edition):

Hansson, A. (2009). Flygplanstillverkning : Fixturkoncept till robotgradning. (Thesis). University West. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1610

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):

Hansson, Anders. “Flygplanstillverkning : Fixturkoncept till robotgradning.” 2009. Thesis, University West. Accessed December 15, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1610.

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

MLA Handbook (7th Edition):

Hansson, Anders. “Flygplanstillverkning : Fixturkoncept till robotgradning.” 2009. Web. 15 Dec 2019.

Vancouver:

Hansson A. Flygplanstillverkning : Fixturkoncept till robotgradning. [Internet] [Thesis]. University West; 2009. [cited 2019 Dec 15]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1610.

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

Council of Science Editors:

Hansson A. Flygplanstillverkning : Fixturkoncept till robotgradning. [Thesis]. University West; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-1610

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

[1] [2] [3] [4]

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