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You searched for subject:(gas turbine). Showing records 1 – 30 of 577 total matches.

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Baylor University

1. Elston, Cassius A., III. Numerical prediction and correlation of leading edge jet impingement with varying jet shapes and flow conditions for gas turbine cooling.

Degree: M.S.M.E., Mechanical Engineering., 2013, Baylor University

 To increase the core power of gas turbine engines, the combustion temperature is elevated above the metallurgical limits of the internal components. As a consequence,… (more)

Subjects/Keywords: Gas turbine cooling.

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APA (6th Edition):

Elston, Cassius A., I. (2013). Numerical prediction and correlation of leading edge jet impingement with varying jet shapes and flow conditions for gas turbine cooling. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/8827

Chicago Manual of Style (16th Edition):

Elston, Cassius A., III. “Numerical prediction and correlation of leading edge jet impingement with varying jet shapes and flow conditions for gas turbine cooling.” 2013. Masters Thesis, Baylor University. Accessed January 23, 2021. http://hdl.handle.net/2104/8827.

MLA Handbook (7th Edition):

Elston, Cassius A., III. “Numerical prediction and correlation of leading edge jet impingement with varying jet shapes and flow conditions for gas turbine cooling.” 2013. Web. 23 Jan 2021.

Vancouver:

Elston, Cassius A. I. Numerical prediction and correlation of leading edge jet impingement with varying jet shapes and flow conditions for gas turbine cooling. [Internet] [Masters thesis]. Baylor University; 2013. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/2104/8827.

Council of Science Editors:

Elston, Cassius A. I. Numerical prediction and correlation of leading edge jet impingement with varying jet shapes and flow conditions for gas turbine cooling. [Masters Thesis]. Baylor University; 2013. Available from: http://hdl.handle.net/2104/8827


Penn State University

2. Borsuk, Alex James. An Experimental Study of Flame Response in a Technically-premixed Multi-nozzle Gas Turbine Combustor.

Degree: 2014, Penn State University

 The response of flames to velocity perturbations is studied experimentally in a multi-nozzle lean-premixed (LPM) gas turbine combustor experiment, representative of a realistic gas turbine(more)

Subjects/Keywords: combustion; dynamics; instability; gas; turbine

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APA (6th Edition):

Borsuk, A. J. (2014). An Experimental Study of Flame Response in a Technically-premixed Multi-nozzle Gas Turbine Combustor. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/22775

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):

Borsuk, Alex James. “An Experimental Study of Flame Response in a Technically-premixed Multi-nozzle Gas Turbine Combustor.” 2014. Thesis, Penn State University. Accessed January 23, 2021. https://submit-etda.libraries.psu.edu/catalog/22775.

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

MLA Handbook (7th Edition):

Borsuk, Alex James. “An Experimental Study of Flame Response in a Technically-premixed Multi-nozzle Gas Turbine Combustor.” 2014. Web. 23 Jan 2021.

Vancouver:

Borsuk AJ. An Experimental Study of Flame Response in a Technically-premixed Multi-nozzle Gas Turbine Combustor. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Jan 23]. Available from: https://submit-etda.libraries.psu.edu/catalog/22775.

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

Council of Science Editors:

Borsuk AJ. An Experimental Study of Flame Response in a Technically-premixed Multi-nozzle Gas Turbine Combustor. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/22775

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


University of Bath

3. Wang, Le. Study of gas turbine ingress using computational fluid dynamics.

Degree: PhD, 2013, University of Bath

 The ingestion of hot mainstream gas into the wheel-space between the rotor and staler discs is one of the most important internal cooling problems for… (more)

Subjects/Keywords: 621.433; CFD; gas turbine; ingress

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APA (6th Edition):

Wang, L. (2013). Study of gas turbine ingress using computational fluid dynamics. (Doctoral Dissertation). University of Bath. Retrieved from https://researchportal.bath.ac.uk/en/studentthesis/study-of-gas-turbine-ingress-using-computational-fluid-dynamics(5d7e84ad-377d-478a-8f44-096e3dd912cf).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604894

Chicago Manual of Style (16th Edition):

Wang, Le. “Study of gas turbine ingress using computational fluid dynamics.” 2013. Doctoral Dissertation, University of Bath. Accessed January 23, 2021. https://researchportal.bath.ac.uk/en/studentthesis/study-of-gas-turbine-ingress-using-computational-fluid-dynamics(5d7e84ad-377d-478a-8f44-096e3dd912cf).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604894.

MLA Handbook (7th Edition):

Wang, Le. “Study of gas turbine ingress using computational fluid dynamics.” 2013. Web. 23 Jan 2021.

Vancouver:

Wang L. Study of gas turbine ingress using computational fluid dynamics. [Internet] [Doctoral dissertation]. University of Bath; 2013. [cited 2021 Jan 23]. Available from: https://researchportal.bath.ac.uk/en/studentthesis/study-of-gas-turbine-ingress-using-computational-fluid-dynamics(5d7e84ad-377d-478a-8f44-096e3dd912cf).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604894.

Council of Science Editors:

Wang L. Study of gas turbine ingress using computational fluid dynamics. [Doctoral Dissertation]. University of Bath; 2013. Available from: https://researchportal.bath.ac.uk/en/studentthesis/study-of-gas-turbine-ingress-using-computational-fluid-dynamics(5d7e84ad-377d-478a-8f44-096e3dd912cf).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604894


Virginia Tech

4. Singh, Prashant. Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions.

Degree: PhD, Mechanical Engineering, 2017, Virginia Tech

 Higher turbine inlet temperatures (TIT) are required for higher overall efficiency of gas turbine engines. Due to the constant push towards achieving high TIT, the… (more)

Subjects/Keywords: Gas turbine; heat transfer; rotation

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APA (6th Edition):

Singh, P. (2017). Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78358

Chicago Manual of Style (16th Edition):

Singh, Prashant. “Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions.” 2017. Doctoral Dissertation, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/78358.

MLA Handbook (7th Edition):

Singh, Prashant. “Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions.” 2017. Web. 23 Jan 2021.

Vancouver:

Singh P. Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions. [Internet] [Doctoral dissertation]. Virginia Tech; 2017. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/78358.

Council of Science Editors:

Singh P. Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under  Stationary and Rotating Conditions. [Doctoral Dissertation]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/78358


Delft University of Technology

5. Bauwens, P.L. (author). Gas path analysis for the MTT micro turbine.

Degree: 2015, Delft University of Technology

Gas turbine diagnostics is as old as the gas turbine itself. Over the years, performance based diagnostics allowed for a shift from time-based maintenance to… (more)

Subjects/Keywords: micro gas turbine; gas turbine simulation; performance modelling; trending; diagnostics

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APA (6th Edition):

Bauwens, P. L. (. (2015). Gas path analysis for the MTT micro turbine. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:a3f7808a-554e-4522-972d-a076012426ee

Chicago Manual of Style (16th Edition):

Bauwens, P L (author). “Gas path analysis for the MTT micro turbine.” 2015. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:a3f7808a-554e-4522-972d-a076012426ee.

MLA Handbook (7th Edition):

Bauwens, P L (author). “Gas path analysis for the MTT micro turbine.” 2015. Web. 23 Jan 2021.

Vancouver:

Bauwens PL(. Gas path analysis for the MTT micro turbine. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:a3f7808a-554e-4522-972d-a076012426ee.

Council of Science Editors:

Bauwens PL(. Gas path analysis for the MTT micro turbine. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:a3f7808a-554e-4522-972d-a076012426ee


Georgia Tech

6. Fu, Haoyun. An architecture-based growth approach for industrial gas turbine product development.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 In this research, an architecture-based methodology has been developed to understand and interpret the ascending performance trajectory of industrial gas turbines from a growth perspective.… (more)

Subjects/Keywords: Industrial gas turbine; Product growth; Gas turbine architecture; Product development

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APA (6th Edition):

Fu, H. (2019). An architecture-based growth approach for industrial gas turbine product development. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/63558

Chicago Manual of Style (16th Edition):

Fu, Haoyun. “An architecture-based growth approach for industrial gas turbine product development.” 2019. Doctoral Dissertation, Georgia Tech. Accessed January 23, 2021. http://hdl.handle.net/1853/63558.

MLA Handbook (7th Edition):

Fu, Haoyun. “An architecture-based growth approach for industrial gas turbine product development.” 2019. Web. 23 Jan 2021.

Vancouver:

Fu H. An architecture-based growth approach for industrial gas turbine product development. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1853/63558.

Council of Science Editors:

Fu H. An architecture-based growth approach for industrial gas turbine product development. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/63558


Stellenbosch University

7. Zhang, Yueqian. Pre-study for conversion of a gas turbine from liquid to gaseous fuel.

Degree: MEng, Mechanical and Mechatronic Engineering, 2016, Stellenbosch University

ENGLISH ABSTRACT: Gaseous fuel has shown its benefits as a promising alternative energy source. In an effort to research the effect of gaseous fuel on… (more)

Subjects/Keywords: Gas turbine; Liquefied petroleum gas; Gas injection; UCTD

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APA (6th Edition):

Zhang, Y. (2016). Pre-study for conversion of a gas turbine from liquid to gaseous fuel. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/98663

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):

Zhang, Yueqian. “Pre-study for conversion of a gas turbine from liquid to gaseous fuel.” 2016. Thesis, Stellenbosch University. Accessed January 23, 2021. http://hdl.handle.net/10019.1/98663.

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

MLA Handbook (7th Edition):

Zhang, Yueqian. “Pre-study for conversion of a gas turbine from liquid to gaseous fuel.” 2016. Web. 23 Jan 2021.

Vancouver:

Zhang Y. Pre-study for conversion of a gas turbine from liquid to gaseous fuel. [Internet] [Thesis]. Stellenbosch University; 2016. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10019.1/98663.

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

Council of Science Editors:

Zhang Y. Pre-study for conversion of a gas turbine from liquid to gaseous fuel. [Thesis]. Stellenbosch University; 2016. Available from: http://hdl.handle.net/10019.1/98663

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


University of Tennessee – Knoxville

8. Hartman, Joshua A. Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT).

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

  With gas turbine engine testing becoming very expensive because of the increasing complexity involved with the engine, engine subsystems, and test support systems, a… (more)

Subjects/Keywords: Gas Turbine; Turbine Engine Design; Turbine Engine Testing; Heat Transfer, Combustion; Propulsion and Power

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APA (6th Edition):

Hartman, J. A. (2014). Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT). (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2821

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):

Hartman, Joshua A. “Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT).” 2014. Thesis, University of Tennessee – Knoxville. Accessed January 23, 2021. https://trace.tennessee.edu/utk_gradthes/2821.

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

MLA Handbook (7th Edition):

Hartman, Joshua A. “Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT).” 2014. Web. 23 Jan 2021.

Vancouver:

Hartman JA. Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT). [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2021 Jan 23]. Available from: https://trace.tennessee.edu/utk_gradthes/2821.

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

Council of Science Editors:

Hartman JA. Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT). [Thesis]. University of Tennessee – Knoxville; 2014. Available from: https://trace.tennessee.edu/utk_gradthes/2821

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


Penn State University

9. Bunce, Nicholas Allen. Flame transfer function measurements and mechanisms in a single-nozzle combustor.

Degree: 2013, Penn State University

 The response of a fully-premixed flame to velocity fluctuations was experimentally measured in a single-nozzle, swirl-stabilized, model gas turbine combustor. Flame response was quantified in… (more)

Subjects/Keywords: combustion; gas turbine; flame response; swirling

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APA (6th Edition):

Bunce, N. A. (2013). Flame transfer function measurements and mechanisms in a single-nozzle combustor. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/18989

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):

Bunce, Nicholas Allen. “Flame transfer function measurements and mechanisms in a single-nozzle combustor.” 2013. Thesis, Penn State University. Accessed January 23, 2021. https://submit-etda.libraries.psu.edu/catalog/18989.

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

MLA Handbook (7th Edition):

Bunce, Nicholas Allen. “Flame transfer function measurements and mechanisms in a single-nozzle combustor.” 2013. Web. 23 Jan 2021.

Vancouver:

Bunce NA. Flame transfer function measurements and mechanisms in a single-nozzle combustor. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 23]. Available from: https://submit-etda.libraries.psu.edu/catalog/18989.

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

Council of Science Editors:

Bunce NA. Flame transfer function measurements and mechanisms in a single-nozzle combustor. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/18989

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


Penn State University

10. Kirsch, Kathryn Louise. Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins.

Degree: 2013, Penn State University

Gas turbines are a vital component in meeting modern society’s energy conversion needs and are found in a variety of applications, most generally in the… (more)

Subjects/Keywords: heat transfer; gas turbine; internal cooling

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APA (6th Edition):

Kirsch, K. L. (2013). Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/20005

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):

Kirsch, Kathryn Louise. “Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins.” 2013. Thesis, Penn State University. Accessed January 23, 2021. https://submit-etda.libraries.psu.edu/catalog/20005.

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

MLA Handbook (7th Edition):

Kirsch, Kathryn Louise. “Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins.” 2013. Web. 23 Jan 2021.

Vancouver:

Kirsch KL. Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 23]. Available from: https://submit-etda.libraries.psu.edu/catalog/20005.

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

Council of Science Editors:

Kirsch KL. Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/20005

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


Penn State University

11. Jones, Brian Keith. Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor .

Degree: 2011, Penn State University

 To satisfy increasingly stringent environmental regulations, gas turbine engines are run in a lean premixed mode. Unfortunately, operating in this mode greatly increases the flame’s… (more)

Subjects/Keywords: premixed; flame; instabilities; lean; combustion; gas turbine

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APA (6th Edition):

Jones, B. K. (2011). Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/10638

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):

Jones, Brian Keith. “Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor .” 2011. Thesis, Penn State University. Accessed January 23, 2021. https://submit-etda.libraries.psu.edu/catalog/10638.

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

MLA Handbook (7th Edition):

Jones, Brian Keith. “Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor .” 2011. Web. 23 Jan 2021.

Vancouver:

Jones BK. Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Jan 23]. Available from: https://submit-etda.libraries.psu.edu/catalog/10638.

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

Council of Science Editors:

Jones BK. Flame Response Mechanisms and their Interaction in a Lean Premixed Swirl-Stabilized Gas Turbine Combustor . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/10638

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


Penn State University

12. Jennings, Timothy John. FILM-COOLED GAS TURBINE VANE TEMPERATURE CALCULATIONS WITH AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH USING EMPIRICAL FILM CORRELATIONS .

Degree: 2011, Penn State University

 The design of gas turbine blades and vanes is a challenging task. The nature of the problem calls for high speed, high temperature, turbulent flows… (more)

Subjects/Keywords: conjugate; gas turbine; film-cooling; heat transfer

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APA (6th Edition):

Jennings, T. J. (2011). FILM-COOLED GAS TURBINE VANE TEMPERATURE CALCULATIONS WITH AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH USING EMPIRICAL FILM CORRELATIONS . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11935

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):

Jennings, Timothy John. “FILM-COOLED GAS TURBINE VANE TEMPERATURE CALCULATIONS WITH AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH USING EMPIRICAL FILM CORRELATIONS .” 2011. Thesis, Penn State University. Accessed January 23, 2021. https://submit-etda.libraries.psu.edu/catalog/11935.

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

MLA Handbook (7th Edition):

Jennings, Timothy John. “FILM-COOLED GAS TURBINE VANE TEMPERATURE CALCULATIONS WITH AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH USING EMPIRICAL FILM CORRELATIONS .” 2011. Web. 23 Jan 2021.

Vancouver:

Jennings TJ. FILM-COOLED GAS TURBINE VANE TEMPERATURE CALCULATIONS WITH AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH USING EMPIRICAL FILM CORRELATIONS . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Jan 23]. Available from: https://submit-etda.libraries.psu.edu/catalog/11935.

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

Council of Science Editors:

Jennings TJ. FILM-COOLED GAS TURBINE VANE TEMPERATURE CALCULATIONS WITH AN ITERATIVE CONJUGATE HEAT TRANSFER APPROACH USING EMPIRICAL FILM CORRELATIONS . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/11935

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


University of Canterbury

13. Asgari, Hamid. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks.

Degree: Mechanical Engineering, 2014, University of Canterbury

 This thesis investigates novel methodologies for modelling, simulation and control of gas turbines using ANNs. In the field of modelling and simulation, two different types… (more)

Subjects/Keywords: gas turbine; neural network; modelling; simulation; control

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APA (6th Edition):

Asgari, H. (2014). Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/9355

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):

Asgari, Hamid. “Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks.” 2014. Thesis, University of Canterbury. Accessed January 23, 2021. http://hdl.handle.net/10092/9355.

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

MLA Handbook (7th Edition):

Asgari, Hamid. “Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks.” 2014. Web. 23 Jan 2021.

Vancouver:

Asgari H. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. [Internet] [Thesis]. University of Canterbury; 2014. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10092/9355.

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

Council of Science Editors:

Asgari H. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. [Thesis]. University of Canterbury; 2014. Available from: http://hdl.handle.net/10092/9355

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


Baylor University

14. Harmon, Weston V. An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades.

Degree: M.S.M.E., Mechanical Engineering., 2014, Baylor University

 Jet impingement is often utilized in the leading edge of actively cooled turbine airfoils to protect the blades from the extreme heat loads encountered within… (more)

Subjects/Keywords: Impingement cooling.; Gas turbine cooling.; Rotating impingement.

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APA (6th Edition):

Harmon, W. V. (2014). An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9158

Chicago Manual of Style (16th Edition):

Harmon, Weston V. “An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades.” 2014. Masters Thesis, Baylor University. Accessed January 23, 2021. http://hdl.handle.net/2104/9158.

MLA Handbook (7th Edition):

Harmon, Weston V. “An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades.” 2014. Web. 23 Jan 2021.

Vancouver:

Harmon WV. An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades. [Internet] [Masters thesis]. Baylor University; 2014. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/2104/9158.

Council of Science Editors:

Harmon WV. An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades. [Masters Thesis]. Baylor University; 2014. Available from: http://hdl.handle.net/2104/9158

15. Kingery, Joseph. An Experimental Investigation Into The Effects Of High Free-Stream Turbulence On Full Coverage Shaped Hole Film Cooling In An Accelerating Boundary Layer.

Degree: MS, Mechanical Engineering, 2015, University of North Dakota

  The purpose of this study is to experimentally investigate the effects of high free stream turbulence on shaped hole film cooling and heat transfer… (more)

Subjects/Keywords: film cooling; gas turbine; shaped holes; turbulence

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APA (6th Edition):

Kingery, J. (2015). An Experimental Investigation Into The Effects Of High Free-Stream Turbulence On Full Coverage Shaped Hole Film Cooling In An Accelerating Boundary Layer. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/1789

Chicago Manual of Style (16th Edition):

Kingery, Joseph. “An Experimental Investigation Into The Effects Of High Free-Stream Turbulence On Full Coverage Shaped Hole Film Cooling In An Accelerating Boundary Layer.” 2015. Masters Thesis, University of North Dakota. Accessed January 23, 2021. https://commons.und.edu/theses/1789.

MLA Handbook (7th Edition):

Kingery, Joseph. “An Experimental Investigation Into The Effects Of High Free-Stream Turbulence On Full Coverage Shaped Hole Film Cooling In An Accelerating Boundary Layer.” 2015. Web. 23 Jan 2021.

Vancouver:

Kingery J. An Experimental Investigation Into The Effects Of High Free-Stream Turbulence On Full Coverage Shaped Hole Film Cooling In An Accelerating Boundary Layer. [Internet] [Masters thesis]. University of North Dakota; 2015. [cited 2021 Jan 23]. Available from: https://commons.und.edu/theses/1789.

Council of Science Editors:

Kingery J. An Experimental Investigation Into The Effects Of High Free-Stream Turbulence On Full Coverage Shaped Hole Film Cooling In An Accelerating Boundary Layer. [Masters Thesis]. University of North Dakota; 2015. Available from: https://commons.und.edu/theses/1789


Northeastern University

16. Fang, Zilong. Casting Imperfection Effects On Heat Transfer Around A 180-degree Turn In A Gas Turbine Airfoil Rib-roughened Cooling Cavity.

Degree: MS, Department of Mechanical and Industrial Engineering, 2018, Northeastern University

 For modern gas turbine engines, the inlet temperature is increased to obtain higher efficiency. To prevent the failure of the turbine blade caused by this… (more)

Subjects/Keywords: gas turbine; rib-roughened; Mechanical engineering

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APA (6th Edition):

Fang, Z. (2018). Casting Imperfection Effects On Heat Transfer Around A 180-degree Turn In A Gas Turbine Airfoil Rib-roughened Cooling Cavity. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20327431

Chicago Manual of Style (16th Edition):

Fang, Zilong. “Casting Imperfection Effects On Heat Transfer Around A 180-degree Turn In A Gas Turbine Airfoil Rib-roughened Cooling Cavity.” 2018. Masters Thesis, Northeastern University. Accessed January 23, 2021. http://hdl.handle.net/2047/D20327431.

MLA Handbook (7th Edition):

Fang, Zilong. “Casting Imperfection Effects On Heat Transfer Around A 180-degree Turn In A Gas Turbine Airfoil Rib-roughened Cooling Cavity.” 2018. Web. 23 Jan 2021.

Vancouver:

Fang Z. Casting Imperfection Effects On Heat Transfer Around A 180-degree Turn In A Gas Turbine Airfoil Rib-roughened Cooling Cavity. [Internet] [Masters thesis]. Northeastern University; 2018. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/2047/D20327431.

Council of Science Editors:

Fang Z. Casting Imperfection Effects On Heat Transfer Around A 180-degree Turn In A Gas Turbine Airfoil Rib-roughened Cooling Cavity. [Masters Thesis]. Northeastern University; 2018. Available from: http://hdl.handle.net/2047/D20327431

17. Raddum, Alexander. Transient Performance of Siemens SGT-750 and SGT-800 : Modeling and Simulations of Industrial Gas Turbines on Island Grids.

Degree: Applied Physics and Electronics, 2020, Umeå University

  Distributed energy production in the form of renewable energy sources are expected to increase in the coming years, a consequence of this is instability… (more)

Subjects/Keywords: Gas Turbine; Transients; Simulation; Energy Engineering; Energiteknik

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APA (6th Edition):

Raddum, A. (2020). Transient Performance of Siemens SGT-750 and SGT-800 : Modeling and Simulations of Industrial Gas Turbines on Island Grids. (Thesis). Umeå University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-171648

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):

Raddum, Alexander. “Transient Performance of Siemens SGT-750 and SGT-800 : Modeling and Simulations of Industrial Gas Turbines on Island Grids.” 2020. Thesis, Umeå University. Accessed January 23, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-171648.

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

MLA Handbook (7th Edition):

Raddum, Alexander. “Transient Performance of Siemens SGT-750 and SGT-800 : Modeling and Simulations of Industrial Gas Turbines on Island Grids.” 2020. Web. 23 Jan 2021.

Vancouver:

Raddum A. Transient Performance of Siemens SGT-750 and SGT-800 : Modeling and Simulations of Industrial Gas Turbines on Island Grids. [Internet] [Thesis]. Umeå University; 2020. [cited 2021 Jan 23]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-171648.

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

Council of Science Editors:

Raddum A. Transient Performance of Siemens SGT-750 and SGT-800 : Modeling and Simulations of Industrial Gas Turbines on Island Grids. [Thesis]. Umeå University; 2020. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:umu:diva-171648

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


Delft University of Technology

18. Voets, Roel (author). Combustion instabilities in combined cycle gas turbine: Analysis and modelling of the impact of operating conditions on combustion instability.

Degree: 2020, Delft University of Technology

 <p class="MsoNormal" style="margin-bottom:0cm;margin-bottom:.0001pt;line-height: normal;mso-layout-grid-align:none;text-autospace:none">With increasing discussion and legislation around emissions, gas turbines have evolved to limit their emissions, especially NOx emissions. The way of operating the… (more)

Subjects/Keywords: Combustion Instability; Gas Turbine; Humming; Thermo-acoustics

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APA (6th Edition):

Voets, R. (. (2020). Combustion instabilities in combined cycle gas turbine: Analysis and modelling of the impact of operating conditions on combustion instability. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:55e219cd-ff23-426c-a87b-f506d80d0ce2

Chicago Manual of Style (16th Edition):

Voets, Roel (author). “Combustion instabilities in combined cycle gas turbine: Analysis and modelling of the impact of operating conditions on combustion instability.” 2020. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:55e219cd-ff23-426c-a87b-f506d80d0ce2.

MLA Handbook (7th Edition):

Voets, Roel (author). “Combustion instabilities in combined cycle gas turbine: Analysis and modelling of the impact of operating conditions on combustion instability.” 2020. Web. 23 Jan 2021.

Vancouver:

Voets R(. Combustion instabilities in combined cycle gas turbine: Analysis and modelling of the impact of operating conditions on combustion instability. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:55e219cd-ff23-426c-a87b-f506d80d0ce2.

Council of Science Editors:

Voets R(. Combustion instabilities in combined cycle gas turbine: Analysis and modelling of the impact of operating conditions on combustion instability. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:55e219cd-ff23-426c-a87b-f506d80d0ce2


Delft University of Technology

19. Jagtenberg, Michelle (author). Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine.

Degree: 2018, Delft University of Technology

 In the near future the Royal Netherlands Air Force will replace their fleet of F-16’s with the F-35. In the past the NLR has aided… (more)

Subjects/Keywords: lifing analysis; gas turbine; heat transfer

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APA (6th Edition):

Jagtenberg, M. (. (2018). Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9cde0103-7518-469b-ba11-feeae40a7b64

Chicago Manual of Style (16th Edition):

Jagtenberg, Michelle (author). “Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine.” 2018. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:9cde0103-7518-469b-ba11-feeae40a7b64.

MLA Handbook (7th Edition):

Jagtenberg, Michelle (author). “Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine.” 2018. Web. 23 Jan 2021.

Vancouver:

Jagtenberg M(. Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:9cde0103-7518-469b-ba11-feeae40a7b64.

Council of Science Editors:

Jagtenberg M(. Development Of A Preliminary Lifing Analysis Tool For The F135-PW-100 Engine. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:9cde0103-7518-469b-ba11-feeae40a7b64


Michigan State University

20. Tarkleson, Eric. Wave-disk engine control, system design and implementation.

Degree: 2013, Michigan State University

Thesis M.S. Michigan State University. Electrical Engineeri 2013.

The wave disk engine is a type of internal combustion gas turbine engine invented by Dr. Norbert… (more)

Subjects/Keywords: Gas-turbine disks; Internal combustion engines; Engineering

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APA (6th Edition):

Tarkleson, E. (2013). Wave-disk engine control, system design and implementation. (Thesis). Michigan State University. Retrieved from http://etd.lib.msu.edu/islandora/object/etd:1591

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):

Tarkleson, Eric. “Wave-disk engine control, system design and implementation.” 2013. Thesis, Michigan State University. Accessed January 23, 2021. http://etd.lib.msu.edu/islandora/object/etd:1591.

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

MLA Handbook (7th Edition):

Tarkleson, Eric. “Wave-disk engine control, system design and implementation.” 2013. Web. 23 Jan 2021.

Vancouver:

Tarkleson E. Wave-disk engine control, system design and implementation. [Internet] [Thesis]. Michigan State University; 2013. [cited 2021 Jan 23]. Available from: http://etd.lib.msu.edu/islandora/object/etd:1591.

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

Council of Science Editors:

Tarkleson E. Wave-disk engine control, system design and implementation. [Thesis]. Michigan State University; 2013. Available from: http://etd.lib.msu.edu/islandora/object/etd:1591

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


MIT

21. Giles, M. (Michael). Newton solution of steady two-dimensional transonic flow .

Degree: Massachusetts Institute of Technology. Gas Turbine Laboratory, 1985, MIT

Subjects/Keywords: Gas Turbine Laboratory.

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APA (6th Edition):

Giles, M. (. (1985). Newton solution of steady two-dimensional transonic flow . (Thesis). MIT. Retrieved from http://hdl.handle.net/1721.1/13815

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):

Giles, M (Michael). “Newton solution of steady two-dimensional transonic flow .” 1985. Thesis, MIT. Accessed January 23, 2021. http://hdl.handle.net/1721.1/13815.

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

MLA Handbook (7th Edition):

Giles, M (Michael). “Newton solution of steady two-dimensional transonic flow .” 1985. Web. 23 Jan 2021.

Vancouver:

Giles M(. Newton solution of steady two-dimensional transonic flow . [Internet] [Thesis]. MIT; 1985. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1721.1/13815.

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

Council of Science Editors:

Giles M(. Newton solution of steady two-dimensional transonic flow . [Thesis]. MIT; 1985. Available from: http://hdl.handle.net/1721.1/13815

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


Georgia Tech

22. Chen, Grace. Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas.

Degree: MS, Chemical and Biomolecular Engineering, 2013, Georgia Tech

 The purpose of this thesis study is to assess the feasibility of using a fiber sorbent module system to remove t-butyl mercaptan (TBM), a common… (more)

Subjects/Keywords: Fiber adsorbents; Mercaptan; Gas turbine corrosion

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APA (6th Edition):

Chen, G. (2013). Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52912

Chicago Manual of Style (16th Edition):

Chen, Grace. “Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas.” 2013. Masters Thesis, Georgia Tech. Accessed January 23, 2021. http://hdl.handle.net/1853/52912.

MLA Handbook (7th Edition):

Chen, Grace. “Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas.” 2013. Web. 23 Jan 2021.

Vancouver:

Chen G. Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas. [Internet] [Masters thesis]. Georgia Tech; 2013. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1853/52912.

Council of Science Editors:

Chen G. Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas. [Masters Thesis]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/52912


Linköping University

23. Hansson, Edvin. Creating a Dynamic Model of a Gas Turbine in the MVEM Framework Using an Ellipse Compressor Model.

Degree: Vehicular Systems, 2020, Linköping University

The legislations on greenhouse gas emissions are getting tougher and tougher every year. This drives the demand for energy efficient gas turbines with as… (more)

Subjects/Keywords: Gas turbine; Modeling; control; Control Engineering; Reglerteknik

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APA (6th Edition):

Hansson, E. (2020). Creating a Dynamic Model of a Gas Turbine in the MVEM Framework Using an Ellipse Compressor Model. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-165062

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, Edvin. “Creating a Dynamic Model of a Gas Turbine in the MVEM Framework Using an Ellipse Compressor Model.” 2020. Thesis, Linköping University. Accessed January 23, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-165062.

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

MLA Handbook (7th Edition):

Hansson, Edvin. “Creating a Dynamic Model of a Gas Turbine in the MVEM Framework Using an Ellipse Compressor Model.” 2020. Web. 23 Jan 2021.

Vancouver:

Hansson E. Creating a Dynamic Model of a Gas Turbine in the MVEM Framework Using an Ellipse Compressor Model. [Internet] [Thesis]. Linköping University; 2020. [cited 2021 Jan 23]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-165062.

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

Council of Science Editors:

Hansson E. Creating a Dynamic Model of a Gas Turbine in the MVEM Framework Using an Ellipse Compressor Model. [Thesis]. Linköping University; 2020. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-165062

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


Virginia Tech

24. Leblanc, Christopher N. Design, Analysis, and Development of a Tripod Film Cooling Hole Design for Reduced Coolant Usage.

Degree: PhD, Mechanical Engineering, 2012, Virginia Tech

 This research has a small portion focused on interior serpentine channels, with the primary focus on improving the effectiveness of the film cooling technique through… (more)

Subjects/Keywords: Heat Transfer; Gas Turbine Cooling; Film Cooling

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APA (6th Edition):

Leblanc, C. N. (2012). Design, Analysis, and Development of a Tripod Film Cooling Hole Design for Reduced Coolant Usage. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/19206

Chicago Manual of Style (16th Edition):

Leblanc, Christopher N. “Design, Analysis, and Development of a Tripod Film Cooling Hole Design for Reduced Coolant Usage.” 2012. Doctoral Dissertation, Virginia Tech. Accessed January 23, 2021. http://hdl.handle.net/10919/19206.

MLA Handbook (7th Edition):

Leblanc, Christopher N. “Design, Analysis, and Development of a Tripod Film Cooling Hole Design for Reduced Coolant Usage.” 2012. Web. 23 Jan 2021.

Vancouver:

Leblanc CN. Design, Analysis, and Development of a Tripod Film Cooling Hole Design for Reduced Coolant Usage. [Internet] [Doctoral dissertation]. Virginia Tech; 2012. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/10919/19206.

Council of Science Editors:

Leblanc CN. Design, Analysis, and Development of a Tripod Film Cooling Hole Design for Reduced Coolant Usage. [Doctoral Dissertation]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/19206


University of Canterbury

25. Asgari, Hamid. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks.

Degree: PhD, Mechanical Engineering, 2014, University of Canterbury

 This thesis investigates novel methodologies for modelling, simulation and control of gas turbines using ANNs. In the field of modelling and simulation, two different types… (more)

Subjects/Keywords: gas turbine; neural network; modelling; simulation; control

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APA (6th Edition):

Asgari, H. (2014). Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. (Doctoral Dissertation). University of Canterbury. Retrieved from http://dx.doi.org/10.26021/3555

Chicago Manual of Style (16th Edition):

Asgari, Hamid. “Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks.” 2014. Doctoral Dissertation, University of Canterbury. Accessed January 23, 2021. http://dx.doi.org/10.26021/3555.

MLA Handbook (7th Edition):

Asgari, Hamid. “Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks.” 2014. Web. 23 Jan 2021.

Vancouver:

Asgari H. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. [Internet] [Doctoral dissertation]. University of Canterbury; 2014. [cited 2021 Jan 23]. Available from: http://dx.doi.org/10.26021/3555.

Council of Science Editors:

Asgari H. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. [Doctoral Dissertation]. University of Canterbury; 2014. Available from: http://dx.doi.org/10.26021/3555


University of Sydney

26. Armstrong, James Leonard. Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines .

Degree: 2017, University of Sydney

 An efficient micro gas turbine could be used to power long range high altitude unmanned aerial vehicles or alternatively as a small portable electrical power… (more)

Subjects/Keywords: micro; gas; turbine; constant; volume; combustion

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APA (6th Edition):

Armstrong, J. L. (2017). Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/17115

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):

Armstrong, James Leonard. “Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines .” 2017. Thesis, University of Sydney. Accessed January 23, 2021. http://hdl.handle.net/2123/17115.

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

MLA Handbook (7th Edition):

Armstrong, James Leonard. “Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines .” 2017. Web. 23 Jan 2021.

Vancouver:

Armstrong JL. Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines . [Internet] [Thesis]. University of Sydney; 2017. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/2123/17115.

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

Council of Science Editors:

Armstrong JL. Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines . [Thesis]. University of Sydney; 2017. Available from: http://hdl.handle.net/2123/17115

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


INP Toulouse

27. Koupper, Charlie. Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines : Simulations instationnaires multi-composants dédiées à l'impact de la chambre de combustion sur la turbine des turbines à gaz aéronautiques.

Degree: Docteur es, Dynamique des fluides, 2015, INP Toulouse

De nos jours, seules les turbines à gaz sont à même de propulser les larges aéronefs (avions ou hélicoptères). Depuis les premiers prototypes construits dans… (more)

Subjects/Keywords: Turbine à gaz; Chambre de combustion; Turbine; Turbulence; Temperature; Cfd; Les; Gas turbine; Combustor; Turbine; Temperature; Turbulence; Cfd; Les

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APA (6th Edition):

Koupper, C. (2015). Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines : Simulations instationnaires multi-composants dédiées à l'impact de la chambre de combustion sur la turbine des turbines à gaz aéronautiques. (Doctoral Dissertation). INP Toulouse. Retrieved from http://www.theses.fr/2015INPT0035

Chicago Manual of Style (16th Edition):

Koupper, Charlie. “Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines : Simulations instationnaires multi-composants dédiées à l'impact de la chambre de combustion sur la turbine des turbines à gaz aéronautiques.” 2015. Doctoral Dissertation, INP Toulouse. Accessed January 23, 2021. http://www.theses.fr/2015INPT0035.

MLA Handbook (7th Edition):

Koupper, Charlie. “Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines : Simulations instationnaires multi-composants dédiées à l'impact de la chambre de combustion sur la turbine des turbines à gaz aéronautiques.” 2015. Web. 23 Jan 2021.

Vancouver:

Koupper C. Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines : Simulations instationnaires multi-composants dédiées à l'impact de la chambre de combustion sur la turbine des turbines à gaz aéronautiques. [Internet] [Doctoral dissertation]. INP Toulouse; 2015. [cited 2021 Jan 23]. Available from: http://www.theses.fr/2015INPT0035.

Council of Science Editors:

Koupper C. Unsteady multi-component simulations dedicated to the impact of the combustion chamber on the turbine of aeronautical gas turbines : Simulations instationnaires multi-composants dédiées à l'impact de la chambre de combustion sur la turbine des turbines à gaz aéronautiques. [Doctoral Dissertation]. INP Toulouse; 2015. Available from: http://www.theses.fr/2015INPT0035


Texas A&M University

28. Kim, Donghak. Process Integration of a Gas to Liquid Plant and a Power Plant.

Degree: MS, Energy, 2018, Texas A&M University

 The gas-to-liquid (GTL) industry is vulnerable to the variation of the oil and gas market price. This shortcoming has forced future GTL projects to be… (more)

Subjects/Keywords: gas to liquid; process integration; power plant; gas turbine

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APA (6th Edition):

Kim, D. (2018). Process Integration of a Gas to Liquid Plant and a Power Plant. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/188945

Chicago Manual of Style (16th Edition):

Kim, Donghak. “Process Integration of a Gas to Liquid Plant and a Power Plant.” 2018. Masters Thesis, Texas A&M University. Accessed January 23, 2021. http://hdl.handle.net/1969.1/188945.

MLA Handbook (7th Edition):

Kim, Donghak. “Process Integration of a Gas to Liquid Plant and a Power Plant.” 2018. Web. 23 Jan 2021.

Vancouver:

Kim D. Process Integration of a Gas to Liquid Plant and a Power Plant. [Internet] [Masters thesis]. Texas A&M University; 2018. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1969.1/188945.

Council of Science Editors:

Kim D. Process Integration of a Gas to Liquid Plant and a Power Plant. [Masters Thesis]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/188945


Texas A&M University

29. Brower, Marissa. Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures.

Degree: MS, Mechanical Engineering, 2012, Texas A&M University

 Applications of natural gases that contain high levels of hydrogen have become a primary interest in the gas turbine market. For reheat gas turbines, understanding… (more)

Subjects/Keywords: natural gas; hydrogen; reactivity; ignition delay time; gas turbine; gas turbine conditions; elevated pressures; shock tube; L9 matrix

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

APA (6th Edition):

Brower, M. (2012). Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11597

Chicago Manual of Style (16th Edition):

Brower, Marissa. “Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures.” 2012. Masters Thesis, Texas A&M University. Accessed January 23, 2021. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11597.

MLA Handbook (7th Edition):

Brower, Marissa. “Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures.” 2012. Web. 23 Jan 2021.

Vancouver:

Brower M. Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11597.

Council of Science Editors:

Brower M. Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11597

30. Matthew, Osagie. Modeling and Simulation of Natural Gas fired Quadruple Cycle for Power Generation.

Degree: 2019, The Catholic University of America

The United States consumed 38% of its primary energy of 97.7 quadrillion Btu on the electric power sector in 2017. The electric utility power plants… (more)

Subjects/Keywords: Gas Turbine; Organic Rankine Cycle; Solid oxide fuel cell; Steam Turbine; Working Fluids

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

APA (6th Edition):

Matthew, O. (2019). Modeling and Simulation of Natural Gas fired Quadruple Cycle for Power Generation. (Thesis). The Catholic University of America. Retrieved from http://hdl.handle.net/1961/cuislandora:213692

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):

Matthew, Osagie. “Modeling and Simulation of Natural Gas fired Quadruple Cycle for Power Generation.” 2019. Thesis, The Catholic University of America. Accessed January 23, 2021. http://hdl.handle.net/1961/cuislandora:213692.

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

MLA Handbook (7th Edition):

Matthew, Osagie. “Modeling and Simulation of Natural Gas fired Quadruple Cycle for Power Generation.” 2019. Web. 23 Jan 2021.

Vancouver:

Matthew O. Modeling and Simulation of Natural Gas fired Quadruple Cycle for Power Generation. [Internet] [Thesis]. The Catholic University of America; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1961/cuislandora:213692.

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

Council of Science Editors:

Matthew O. Modeling and Simulation of Natural Gas fired Quadruple Cycle for Power Generation. [Thesis]. The Catholic University of America; 2019. Available from: http://hdl.handle.net/1961/cuislandora:213692

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

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