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You searched for subject:(Gas Turbine). Showing records 1 – 30 of 528 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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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


The Ohio State University

2. Smith, Christopher Stephen. Experimental Validation of a Hot Gas Turbine Particle Deposition Facility.

Degree: MS, Aeronautical and Astronautical Engineering, 2010, The Ohio State University

 A new turbine research facility at The Ohio State University Aeronautical and Astronautical Research Lab has been constructed. The purpose of this facility is to… (more)

Subjects/Keywords: Mechanical Engineering; turbine; deposition; gas turbine; turbine deposition; turbine aerodynamics

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APA (6th Edition):

Smith, C. S. (2010). Experimental Validation of a Hot Gas Turbine Particle Deposition Facility. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1269547595

Chicago Manual of Style (16th Edition):

Smith, Christopher Stephen. “Experimental Validation of a Hot Gas Turbine Particle Deposition Facility.” 2010. Masters Thesis, The Ohio State University. Accessed March 29, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1269547595.

MLA Handbook (7th Edition):

Smith, Christopher Stephen. “Experimental Validation of a Hot Gas Turbine Particle Deposition Facility.” 2010. Web. 29 Mar 2020.

Vancouver:

Smith CS. Experimental Validation of a Hot Gas Turbine Particle Deposition Facility. [Internet] [Masters thesis]. The Ohio State University; 2010. [cited 2020 Mar 29]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1269547595.

Council of Science Editors:

Smith CS. Experimental Validation of a Hot Gas Turbine Particle Deposition Facility. [Masters Thesis]. The Ohio State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1269547595


Penn State University

3. Kane, Mangesh Ashok. STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES.

Degree: MS, Mechanical Engineering, 2009, Penn State University

 Conjugate heat transfer for turbulent flow over flat plates and turbine blades have been simulated and studied using a commercial computational fluid dynamics code FLUENT.… (more)

Subjects/Keywords: conjugate heat transfer; gas turbine

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APA (6th Edition):

Kane, M. A. (2009). STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/9333

Chicago Manual of Style (16th Edition):

Kane, Mangesh Ashok. “STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES.” 2009. Masters Thesis, Penn State University. Accessed March 29, 2020. https://etda.libraries.psu.edu/catalog/9333.

MLA Handbook (7th Edition):

Kane, Mangesh Ashok. “STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES.” 2009. Web. 29 Mar 2020.

Vancouver:

Kane MA. STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2020 Mar 29]. Available from: https://etda.libraries.psu.edu/catalog/9333.

Council of Science Editors:

Kane MA. STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES. [Masters Thesis]. Penn State University; 2009. Available from: https://etda.libraries.psu.edu/catalog/9333


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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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


University of Bath

5. 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 March 29, 2020. 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. 29 Mar 2020.

Vancouver:

Wang L. Study of gas turbine ingress using computational fluid dynamics. [Internet] [Doctoral dissertation]. University of Bath; 2013. [cited 2020 Mar 29]. 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

6. Farina, Jordan Thomas. Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization.

Degree: MS, Mechanical Engineering, 2010, Virginia Tech

 The continued use of fossil fuels along with a rise in energy demand has led to increasing levels of carbon emissions over the past years.… (more)

Subjects/Keywords: Hydrogen; Lean-Premixed; Gas Turbine

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APA (6th Edition):

Farina, J. T. (2010). Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31067

Chicago Manual of Style (16th Edition):

Farina, Jordan Thomas. “Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization.” 2010. Masters Thesis, Virginia Tech. Accessed March 29, 2020. http://hdl.handle.net/10919/31067.

MLA Handbook (7th Edition):

Farina, Jordan Thomas. “Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization.” 2010. Web. 29 Mar 2020.

Vancouver:

Farina JT. Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/10919/31067.

Council of Science Editors:

Farina JT. Conversion of a Gas Turbine Engine to Operate on Lean-Premixed Hydrogen-Air: Design and Characterization. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/31067


University of Notre Dame

7. John Thomas Schmitz. Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2010, University of Notre Dame

  The performance and detailed flow physics of a transonic, low-pressure turbine (LPT) stage with design Zw=1.35, ∆hT /U2 = 2.8, ϕ = 0.78, and… (more)

Subjects/Keywords: low pressure turbine; turbine; high load; turbomachinery; gas turbine; high lift

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APA (6th Edition):

Schmitz, J. T. (2010). Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/j098z89301d

Chicago Manual of Style (16th Edition):

Schmitz, John Thomas. “Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>.” 2010. Doctoral Dissertation, University of Notre Dame. Accessed March 29, 2020. https://curate.nd.edu/show/j098z89301d.

MLA Handbook (7th Edition):

Schmitz, John Thomas. “Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>.” 2010. Web. 29 Mar 2020.

Vancouver:

Schmitz JT. Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2020 Mar 29]. Available from: https://curate.nd.edu/show/j098z89301d.

Council of Science Editors:

Schmitz JT. Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>. [Doctoral Dissertation]. University of Notre Dame; 2010. Available from: https://curate.nd.edu/show/j098z89301d


Delft University of Technology

8. Bauwens, P.L. 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. “Gas path analysis for the MTT micro turbine:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 29, 2020. http://resolver.tudelft.nl/uuid:a3f7808a-554e-4522-972d-a076012426ee.

MLA Handbook (7th Edition):

Bauwens, P L. “Gas path analysis for the MTT micro turbine:.” 2015. Web. 29 Mar 2020.

Vancouver:

Bauwens PL. Gas path analysis for the MTT micro turbine:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Mar 29]. 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


University of Tennessee – Knoxville

9. 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 March 29, 2020. 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. 29 Mar 2020.

Vancouver:

Hartman JA. Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT). [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2020 Mar 29]. 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


Indian Institute of Science

10. Ashirvadam, Kampa. Combustion Instability Screech In Gas Turbine Afterburner.

Degree: 2007, Indian Institute of Science

Gas turbine reheat thrust augmenters known as afterburners are used to provide additional thrust during emergencies, take off, combat, and in supersonic flight of high-performance… (more)

Subjects/Keywords: Gas Turbine; Combustion; Gas Turbines - Combustion; Gas Turbine Afterburners; Aircraft Gas Turbines - Combustion; Gas Turbines - Combustion Chambers; Gas Turbine Afterburners - Combustion Instabiltiy; Heat Engineering

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APA (6th Edition):

Ashirvadam, K. (2007). Combustion Instability Screech In Gas Turbine Afterburner. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/581

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):

Ashirvadam, Kampa. “Combustion Instability Screech In Gas Turbine Afterburner.” 2007. Thesis, Indian Institute of Science. Accessed March 29, 2020. http://hdl.handle.net/2005/581.

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

MLA Handbook (7th Edition):

Ashirvadam, Kampa. “Combustion Instability Screech In Gas Turbine Afterburner.” 2007. Web. 29 Mar 2020.

Vancouver:

Ashirvadam K. Combustion Instability Screech In Gas Turbine Afterburner. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/2005/581.

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

Council of Science Editors:

Ashirvadam K. Combustion Instability Screech In Gas Turbine Afterburner. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/581

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


Penn State University

11. Vadvadgi, Aneesh Sridhar. CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR.

Degree: MS, Mechanical Engineering, 2010, Penn State University

 The present study deals with the numerical modeling of the turbulent flow in a rotor-stator cavity with or without imposed through flow with heat transfer.… (more)

Subjects/Keywords: CFD; Conjugate heat transfer; gas turbine

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APA (6th Edition):

Vadvadgi, A. S. (2010). CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10740

Chicago Manual of Style (16th Edition):

Vadvadgi, Aneesh Sridhar. “CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR.” 2010. Masters Thesis, Penn State University. Accessed March 29, 2020. https://etda.libraries.psu.edu/catalog/10740.

MLA Handbook (7th Edition):

Vadvadgi, Aneesh Sridhar. “CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR.” 2010. Web. 29 Mar 2020.

Vancouver:

Vadvadgi AS. CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2020 Mar 29]. Available from: https://etda.libraries.psu.edu/catalog/10740.

Council of Science Editors:

Vadvadgi AS. CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR. [Masters Thesis]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/10740


Penn State University

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

Degree: MS, Mechanical Engineering, 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. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/20005

Chicago Manual of Style (16th Edition):

Kirsch, Kathryn Louise. “Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins.” 2013. Masters Thesis, Penn State University. Accessed March 29, 2020. https://etda.libraries.psu.edu/catalog/20005.

MLA Handbook (7th Edition):

Kirsch, Kathryn Louise. “Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins.” 2013. Web. 29 Mar 2020.

Vancouver:

Kirsch KL. Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2020 Mar 29]. Available from: https://etda.libraries.psu.edu/catalog/20005.

Council of Science Editors:

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


Penn State University

13. Marzelli, Steven Benjamin. Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines.

Degree: MS, Mechanical Engineering, 2010, Penn State University

 Due to the ever-increasing demand for energy, it is likely that stationary gas turbine engines will require the use of fuels with a diverse range… (more)

Subjects/Keywords: gas turbine engines; lean premixed; flameholding

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APA (6th Edition):

Marzelli, S. B. (2010). Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/10838

Chicago Manual of Style (16th Edition):

Marzelli, Steven Benjamin. “Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines.” 2010. Masters Thesis, Penn State University. Accessed March 29, 2020. https://etda.libraries.psu.edu/catalog/10838.

MLA Handbook (7th Edition):

Marzelli, Steven Benjamin. “Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines.” 2010. Web. 29 Mar 2020.

Vancouver:

Marzelli SB. Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2020 Mar 29]. Available from: https://etda.libraries.psu.edu/catalog/10838.

Council of Science Editors:

Marzelli SB. Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines. [Masters Thesis]. Penn State University; 2010. Available from: https://etda.libraries.psu.edu/catalog/10838


University of Sydney

14. 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 March 29, 2020. 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. 29 Mar 2020.

Vancouver:

Armstrong JL. Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines . [Internet] [Thesis]. University of Sydney; 2017. [cited 2020 Mar 29]. 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


Virginia Tech

15. 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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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


Delft University of Technology

16. Singh, V. Transient modelling and analysis of the OP16 gas turbine in GSP:.

Degree: 2015, Delft University of Technology

 With the current trend towards flexible engine operation with high efficiency and low emissions, dynamic modelling of gas turbines has become critical to ensure safe… (more)

Subjects/Keywords: gas turbine; transient performance analysis; GSP

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APA (6th Edition):

Singh, V. (2015). Transient modelling and analysis of the OP16 gas turbine in GSP:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e134587d-da8c-4f47-b4a6-bcec254a1ef5

Chicago Manual of Style (16th Edition):

Singh, V. “Transient modelling and analysis of the OP16 gas turbine in GSP:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 29, 2020. http://resolver.tudelft.nl/uuid:e134587d-da8c-4f47-b4a6-bcec254a1ef5.

MLA Handbook (7th Edition):

Singh, V. “Transient modelling and analysis of the OP16 gas turbine in GSP:.” 2015. Web. 29 Mar 2020.

Vancouver:

Singh V. Transient modelling and analysis of the OP16 gas turbine in GSP:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2020 Mar 29]. Available from: http://resolver.tudelft.nl/uuid:e134587d-da8c-4f47-b4a6-bcec254a1ef5.

Council of Science Editors:

Singh V. Transient modelling and analysis of the OP16 gas turbine in GSP:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:e134587d-da8c-4f47-b4a6-bcec254a1ef5


University of Canterbury

17. 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 March 29, 2020. 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. 29 Mar 2020.

Vancouver:

Asgari H. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. [Internet] [Thesis]. University of Canterbury; 2014. [cited 2020 Mar 29]. 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


MIT

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

Degree: PhD, 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 . (Doctoral Dissertation). MIT. Retrieved from http://hdl.handle.net/1721.1/13815

Chicago Manual of Style (16th Edition):

Giles, M (Michael). “Newton solution of steady two-dimensional transonic flow .” 1985. Doctoral Dissertation, MIT. Accessed March 29, 2020. http://hdl.handle.net/1721.1/13815.

MLA Handbook (7th Edition):

Giles, M (Michael). “Newton solution of steady two-dimensional transonic flow .” 1985. Web. 29 Mar 2020.

Vancouver:

Giles M(. Newton solution of steady two-dimensional transonic flow . [Internet] [Doctoral dissertation]. MIT; 1985. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/1721.1/13815.

Council of Science Editors:

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

19. 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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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

20. 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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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


Baylor University

21. 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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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


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 March 29, 2020. 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. 29 Mar 2020.

Vancouver:

Chen G. Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas. [Internet] [Masters thesis]. Georgia Tech; 2013. [cited 2020 Mar 29]. 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


INP Toulouse

23. 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 March 29, 2020. 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. 29 Mar 2020.

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 2020 Mar 29]. 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

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

Degree: 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 (6th Edition):

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

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):

Brower, Marissa. “Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures.” 2012. Thesis, Texas A&M University. Accessed March 29, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11597.

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

MLA Handbook (7th Edition):

Brower, Marissa. “Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures.” 2012. Web. 29 Mar 2020.

Vancouver:

Brower M. Ignition Delay Times of Natural Gas/Hydrogen Blends at Elevated Pressures. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2012-08-11597.

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

Council of Science Editors:

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

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


Virginia Tech

25. Stitzel, Sarah M. Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine.

Degree: MS, Mechanical Engineering, 2001, Virginia Tech

 The current demands for higher performance in gas turbine engines can be reached by raising combustion temperatures to increase thermal efficiency. Hot combustion temperatures create… (more)

Subjects/Keywords: Turbine Vane; Gas Turbine; Combustor; CFD

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APA (6th Edition):

Stitzel, S. M. (2001). Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30992

Chicago Manual of Style (16th Edition):

Stitzel, Sarah M. “Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine.” 2001. Masters Thesis, Virginia Tech. Accessed March 29, 2020. http://hdl.handle.net/10919/30992.

MLA Handbook (7th Edition):

Stitzel, Sarah M. “Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine.” 2001. Web. 29 Mar 2020.

Vancouver:

Stitzel SM. Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine. [Internet] [Masters thesis]. Virginia Tech; 2001. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/10919/30992.

Council of Science Editors:

Stitzel SM. Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine. [Masters Thesis]. Virginia Tech; 2001. Available from: http://hdl.handle.net/10919/30992

26. Bufi, Elio Antonio. Optimisation robuste de turbines pour les cycles organiques de Rankine (ORC) : Robust optimization of ORC turbine expanders.

Degree: Docteur es, Mécanique des fluides, 2016, Paris, ENSAM; Politecnico di Bari. Dipartimento di Ingegneria Meccanica e Gestionale (Italia)

 Au cours des dernières années, le cycles organique de Rankine (ORC) ont reçu un grand intérêt de la communauté scientifique et technique en raison de… (more)

Subjects/Keywords: Gaz dense; Orc; Turbine; Optimisation; Incertitudes; Dense gas; Orc; Turbine; Optimization; Uncertainty

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APA (6th Edition):

Bufi, E. A. (2016). Optimisation robuste de turbines pour les cycles organiques de Rankine (ORC) : Robust optimization of ORC turbine expanders. (Doctoral Dissertation). Paris, ENSAM; Politecnico di Bari. Dipartimento di Ingegneria Meccanica e Gestionale (Italia). Retrieved from http://www.theses.fr/2016ENAM0070

Chicago Manual of Style (16th Edition):

Bufi, Elio Antonio. “Optimisation robuste de turbines pour les cycles organiques de Rankine (ORC) : Robust optimization of ORC turbine expanders.” 2016. Doctoral Dissertation, Paris, ENSAM; Politecnico di Bari. Dipartimento di Ingegneria Meccanica e Gestionale (Italia). Accessed March 29, 2020. http://www.theses.fr/2016ENAM0070.

MLA Handbook (7th Edition):

Bufi, Elio Antonio. “Optimisation robuste de turbines pour les cycles organiques de Rankine (ORC) : Robust optimization of ORC turbine expanders.” 2016. Web. 29 Mar 2020.

Vancouver:

Bufi EA. Optimisation robuste de turbines pour les cycles organiques de Rankine (ORC) : Robust optimization of ORC turbine expanders. [Internet] [Doctoral dissertation]. Paris, ENSAM; Politecnico di Bari. Dipartimento di Ingegneria Meccanica e Gestionale (Italia); 2016. [cited 2020 Mar 29]. Available from: http://www.theses.fr/2016ENAM0070.

Council of Science Editors:

Bufi EA. Optimisation robuste de turbines pour les cycles organiques de Rankine (ORC) : Robust optimization of ORC turbine expanders. [Doctoral Dissertation]. Paris, ENSAM; Politecnico di Bari. Dipartimento di Ingegneria Meccanica e Gestionale (Italia); 2016. Available from: http://www.theses.fr/2016ENAM0070

27. Underwood, Sean Christopher. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.

Degree: PhD, Aerospace Engineering, 2018, University of Kansas

 The service life of gas turbine engine turbine blades depends on the blade’s material, service temperature and total stress. In high-performance gas turbines, film cooling… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Aerothermodynamics; Film Cooling; Gas Turbine; Impingement Cooling; Propulsion; Turbine Blade Cooling

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APA (6th Edition):

Underwood, S. C. (2018). Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27605

Chicago Manual of Style (16th Edition):

Underwood, Sean Christopher. “Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.” 2018. Doctoral Dissertation, University of Kansas. Accessed March 29, 2020. http://hdl.handle.net/1808/27605.

MLA Handbook (7th Edition):

Underwood, Sean Christopher. “Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.” 2018. Web. 29 Mar 2020.

Vancouver:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/1808/27605.

Council of Science Editors:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Doctoral Dissertation]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27605


Brno University of Technology

28. Tota, Lukáš. Tepelné tubiny .

Degree: 2011, Brno University of Technology

 Bakalářská práce pojednává o tepelných turbínách. První kapitola se věnuje historii, s ohledem na stroje, které turbínám předcházely a charakteristickým problémům provázejícím výrobu turbín. Dále je… (more)

Subjects/Keywords: Parní turbína; plynová turbína; tepelný cyklus; energie; Steam turbine; gas turbine; heat cycle; energy

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APA (6th Edition):

Tota, L. (2011). Tepelné tubiny . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/5532

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):

Tota, Lukáš. “Tepelné tubiny .” 2011. Thesis, Brno University of Technology. Accessed March 29, 2020. http://hdl.handle.net/11012/5532.

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

MLA Handbook (7th Edition):

Tota, Lukáš. “Tepelné tubiny .” 2011. Web. 29 Mar 2020.

Vancouver:

Tota L. Tepelné tubiny . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/11012/5532.

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

Council of Science Editors:

Tota L. Tepelné tubiny . [Thesis]. Brno University of Technology; 2011. Available from: http://hdl.handle.net/11012/5532

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


Linköping University

29. Farhanieh, Arman. Investigation on methods to improve heat loadprediction of the SGT-600 gas turbine.

Degree: Applied Thermodynamics and Fluid Mechanics, 2016, Linköping University

  In modern gas turbines, with the increase of inlet gas temperature to raise thework output, the importance of accurate aero-thermal analysis has become of… (more)

Subjects/Keywords: Gas Turbine; CFD; Turbomachinery; High Pressure Turbine; Heat Load; Time Transformation; Profile Transformation; Mixing Plane

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APA (6th Edition):

Farhanieh, A. (2016). Investigation on methods to improve heat loadprediction of the SGT-600 gas turbine. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-124552

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):

Farhanieh, Arman. “Investigation on methods to improve heat loadprediction of the SGT-600 gas turbine.” 2016. Thesis, Linköping University. Accessed March 29, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-124552.

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

MLA Handbook (7th Edition):

Farhanieh, Arman. “Investigation on methods to improve heat loadprediction of the SGT-600 gas turbine.” 2016. Web. 29 Mar 2020.

Vancouver:

Farhanieh A. Investigation on methods to improve heat loadprediction of the SGT-600 gas turbine. [Internet] [Thesis]. Linköping University; 2016. [cited 2020 Mar 29]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-124552.

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

Council of Science Editors:

Farhanieh A. Investigation on methods to improve heat loadprediction of the SGT-600 gas turbine. [Thesis]. Linköping University; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-124552

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


Indian Institute of Science

30. Singhal, Atul. Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations.

Degree: 2009, Indian Institute of Science

 Trapped Vortex Combustor (TVC) is a relatively new concept for potential use in gas turbine engines addressing ever increasing demands of high efficiency, low emissions,… (more)

Subjects/Keywords: Combustion Engineering; Combustion Dynamics - Simulation; Trapped Vortex Combustor (TVC); Computational Fluid Dynamics; Gas Turbine Combustors; Cavity Flow Dynamics; Single Cavity; Gas Turbine; Combustion Efficiency; Gas Turbine Combustors; Heat Engineering

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

APA (6th Edition):

Singhal, A. (2009). Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1123

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):

Singhal, Atul. “Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations.” 2009. Thesis, Indian Institute of Science. Accessed March 29, 2020. http://hdl.handle.net/2005/1123.

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

MLA Handbook (7th Edition):

Singhal, Atul. “Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations.” 2009. Web. 29 Mar 2020.

Vancouver:

Singhal A. Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2020 Mar 29]. Available from: http://hdl.handle.net/2005/1123.

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

Council of Science Editors:

Singhal A. Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1123

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

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