Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Hot section gas turbine components). Showing records 1 – 30 of 17883 total matches.

[1] [2] [3] [4] [5] … [597]

Search Limiters

Last 2 Years | English Only

Degrees

Languages

Country

▼ Search Limiters

1. Acharya, Ranadip. Multiphysics modeling and statistical process optimization of the scanning laser epitaxy process applied to additive manufacturing of turbine engine hot-section superalloy components.

Degree: PhD, Mechanical Engineering, 2014, Georgia Tech

 Scanning Laser Epitaxy (SLE) is a new laser-based layer-by-layer generative manufacturing technology being developed in the Direct Digital Manufacturing Laboratory at Georgia Tech. SLE allows… (more)

Subjects/Keywords: Additive manufacturing; Hot-section gas turbine components; Multi-physics modeling; Superalloy; Multivariate statistics

…studies and apply this knowledge for hot section turbine component repair and ultimately extend… …the process capability to enable one-step manufacture of complex gas turbine components… …Prior methods of repair specifically for hot-section Ni-base superalloys have shown limited… …230 xii LIST OF FIGURES Figure 1. (a) Turbine airfoil with worn out blade tip… …and (b) cracking in the platform section...... 5 Figure 2. Schematic of SLE (… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Acharya, R. (2014). Multiphysics modeling and statistical process optimization of the scanning laser epitaxy process applied to additive manufacturing of turbine engine hot-section superalloy components. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54294

Chicago Manual of Style (16th Edition):

Acharya, Ranadip. “Multiphysics modeling and statistical process optimization of the scanning laser epitaxy process applied to additive manufacturing of turbine engine hot-section superalloy components.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/54294.

MLA Handbook (7th Edition):

Acharya, Ranadip. “Multiphysics modeling and statistical process optimization of the scanning laser epitaxy process applied to additive manufacturing of turbine engine hot-section superalloy components.” 2014. Web. 18 Mar 2019.

Vancouver:

Acharya R. Multiphysics modeling and statistical process optimization of the scanning laser epitaxy process applied to additive manufacturing of turbine engine hot-section superalloy components. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/54294.

Council of Science Editors:

Acharya R. Multiphysics modeling and statistical process optimization of the scanning laser epitaxy process applied to additive manufacturing of turbine engine hot-section superalloy components. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/54294


Queens University

2. Crawford, James. Design and Calibration of Seven Hole Probes for Flow Measurement .

Degree: Mechanical and Materials Engineering, 2011, Queens University

 The calibration and use of seven hole pressure probes for hot flow measurement was studied extensively, and guidelines were developed for the calibration and use… (more)

Subjects/Keywords: fluid mechanics; flow measurement; pressure probe; hot flow; gas turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Crawford, J. (2011). Design and Calibration of Seven Hole Probes for Flow Measurement . (Thesis). Queens University. Retrieved from http://hdl.handle.net/1974/6380

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):

Crawford, James. “Design and Calibration of Seven Hole Probes for Flow Measurement .” 2011. Thesis, Queens University. Accessed March 18, 2019. http://hdl.handle.net/1974/6380.

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

MLA Handbook (7th Edition):

Crawford, James. “Design and Calibration of Seven Hole Probes for Flow Measurement .” 2011. Web. 18 Mar 2019.

Vancouver:

Crawford J. Design and Calibration of Seven Hole Probes for Flow Measurement . [Internet] [Thesis]. Queens University; 2011. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1974/6380.

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

Council of Science Editors:

Crawford J. Design and Calibration of Seven Hole Probes for Flow Measurement . [Thesis]. Queens University; 2011. Available from: http://hdl.handle.net/1974/6380

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


Penn State University

3. Clark, Kenneth Phillip. Sealing Effectiveness of a Turbine Rim Seal at Engine-Relevant Conditions.

Degree: PhD, Mechanical Engineering, 2016, Penn State University

Gas turbines are characterized by high efficiencies compared to other power generation systems, but even small efficiency gains can result in huge reductions in fuel… (more)

Subjects/Keywords: turbomachinery; turbine; rim seals; hot gas ingestion; experimental; engine relevant

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Clark, K. P. (2016). Sealing Effectiveness of a Turbine Rim Seal at Engine-Relevant Conditions. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13317kpc139

Chicago Manual of Style (16th Edition):

Clark, Kenneth Phillip. “Sealing Effectiveness of a Turbine Rim Seal at Engine-Relevant Conditions.” 2016. Doctoral Dissertation, Penn State University. Accessed March 18, 2019. https://etda.libraries.psu.edu/catalog/13317kpc139.

MLA Handbook (7th Edition):

Clark, Kenneth Phillip. “Sealing Effectiveness of a Turbine Rim Seal at Engine-Relevant Conditions.” 2016. Web. 18 Mar 2019.

Vancouver:

Clark KP. Sealing Effectiveness of a Turbine Rim Seal at Engine-Relevant Conditions. [Internet] [Doctoral dissertation]. Penn State University; 2016. [cited 2019 Mar 18]. Available from: https://etda.libraries.psu.edu/catalog/13317kpc139.

Council of Science Editors:

Clark KP. Sealing Effectiveness of a Turbine Rim Seal at Engine-Relevant Conditions. [Doctoral Dissertation]. Penn State University; 2016. Available from: https://etda.libraries.psu.edu/catalog/13317kpc139


Louisiana State University

4. Habibi, Mohammad Hamed. Hot corrosion behaviour of new candidates for thermal barrier coatings application in turbine simulated environments.

Degree: PhD, Mechanical Engineering, 2014, Louisiana State University

 Thermal barrier coatings (TBCs) are used gas turbine engines. The current material of choice (YSZ) degrades when it contacts with impurities arise from low quality… (more)

Subjects/Keywords: SEM; XRD; Hot Corrosion; Thermal Barrier Coating; Gas Turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Habibi, M. H. (2014). Hot corrosion behaviour of new candidates for thermal barrier coatings application in turbine simulated environments. (Doctoral Dissertation). Louisiana State University. Retrieved from etd-02202014-135120 ; https://digitalcommons.lsu.edu/gradschool_dissertations/301

Chicago Manual of Style (16th Edition):

Habibi, Mohammad Hamed. “Hot corrosion behaviour of new candidates for thermal barrier coatings application in turbine simulated environments.” 2014. Doctoral Dissertation, Louisiana State University. Accessed March 18, 2019. etd-02202014-135120 ; https://digitalcommons.lsu.edu/gradschool_dissertations/301.

MLA Handbook (7th Edition):

Habibi, Mohammad Hamed. “Hot corrosion behaviour of new candidates for thermal barrier coatings application in turbine simulated environments.” 2014. Web. 18 Mar 2019.

Vancouver:

Habibi MH. Hot corrosion behaviour of new candidates for thermal barrier coatings application in turbine simulated environments. [Internet] [Doctoral dissertation]. Louisiana State University; 2014. [cited 2019 Mar 18]. Available from: etd-02202014-135120 ; https://digitalcommons.lsu.edu/gradschool_dissertations/301.

Council of Science Editors:

Habibi MH. Hot corrosion behaviour of new candidates for thermal barrier coatings application in turbine simulated environments. [Doctoral Dissertation]. Louisiana State University; 2014. Available from: etd-02202014-135120 ; https://digitalcommons.lsu.edu/gradschool_dissertations/301


University of Ottawa

5. Smith, Craig I. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance .

Degree: 2010, University of Ottawa

 The temperature of the flow entering a high-pressure turbine stage is inherently non-uniform, as it is produced by several discrete, azimuthally-distributed combustors. In general, however,… (more)

Subjects/Keywords: hot streak; turbomachinery; turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Smith, C. I. (2010). Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . (Thesis). University of Ottawa. Retrieved from http://hdl.handle.net/10393/19660

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):

Smith, Craig I. “Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance .” 2010. Thesis, University of Ottawa. Accessed March 18, 2019. http://hdl.handle.net/10393/19660.

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

MLA Handbook (7th Edition):

Smith, Craig I. “Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance .” 2010. Web. 18 Mar 2019.

Vancouver:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Internet] [Thesis]. University of Ottawa; 2010. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/10393/19660.

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

Council of Science Editors:

Smith CI. Effect of Inlet Temperature Non-Uniformity on High-Pressure Turbine Performance . [Thesis]. University of Ottawa; 2010. Available from: http://hdl.handle.net/10393/19660

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


Baylor University

6. 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: 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.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/8827

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):

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. Thesis, Baylor University. Accessed March 18, 2019. http://hdl.handle.net/2104/8827.

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

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. 18 Mar 2019.

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] [Thesis]. Baylor University; 2013. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/2104/8827.

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

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. [Thesis]. Baylor University; 2013. Available from: http://hdl.handle.net/2104/8827

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


The Ohio State University

7. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Smith CS. Experimental Validation of a Hot Gas Turbine Particle Deposition Facility. [Internet] [Masters thesis]. The Ohio State University; 2010. [cited 2019 Mar 18]. 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


University of Texas – Austin

8. -3980-1932. Development of novel tapered pin fin geometries for additive manufacturing of compact heat exchangers.

Degree: Mechanical Engineering, 2016, University of Texas – Austin

 Pin fin arrays are widely used to enhance forced convection heat transfer across various industries, finding application in turbine blade trailing edges, electronics cooling, and… (more)

Subjects/Keywords: Additive manufacturing; Heat exchanger; Heat transfer; Pin fin; Teardrop pin fin; Tapered pin fin; Elliptical pin fin; Specific friction loss; Variable section; Blade cooling; Gas turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

-3980-1932. (2016). Development of novel tapered pin fin geometries for additive manufacturing of compact heat exchangers. (Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/41624

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

Chicago Manual of Style (16th Edition):

-3980-1932. “Development of novel tapered pin fin geometries for additive manufacturing of compact heat exchangers.” 2016. Thesis, University of Texas – Austin. Accessed March 18, 2019. http://hdl.handle.net/2152/41624.

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

MLA Handbook (7th Edition):

-3980-1932. “Development of novel tapered pin fin geometries for additive manufacturing of compact heat exchangers.” 2016. Web. 18 Mar 2019.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

-3980-1932. Development of novel tapered pin fin geometries for additive manufacturing of compact heat exchangers. [Internet] [Thesis]. University of Texas – Austin; 2016. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/2152/41624.

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

Council of Science Editors:

-3980-1932. Development of novel tapered pin fin geometries for additive manufacturing of compact heat exchangers. [Thesis]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/41624

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


University of Notre Dame

9. Nicholas Andrew Jaffa. Unsteady Measurement Techniques for Turbomachinery Flows</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2015, University of Notre Dame

  Accurate unsteady measurements are required for studying the flows in high speed turbomachines, which rely on the interaction between rotating and stationary components. Using… (more)

Subjects/Keywords: stagnation temperature; axial velocity; error analysis; high speed; compressible; unsteady; gas turbine; measurement techniques; slanted hot-wire; constant temperature anemometry; kiel probe; turbine; stagnation pressure; turbomachinery; hot-wire; hot-wire calibration; frequency response; compressor; swirl velocity; laser pulse; unsteady total pressure probe; multiple overheat; validation; uncertainty quantification; phase locked average; swirl angle; phase peak yaw; radial velocity

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Jaffa, N. A. (2015). Unsteady Measurement Techniques for Turbomachinery Flows</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/w9504x54160

Chicago Manual of Style (16th Edition):

Jaffa, Nicholas Andrew. “Unsteady Measurement Techniques for Turbomachinery Flows</h1>.” 2015. Doctoral Dissertation, University of Notre Dame. Accessed March 18, 2019. https://curate.nd.edu/show/w9504x54160.

MLA Handbook (7th Edition):

Jaffa, Nicholas Andrew. “Unsteady Measurement Techniques for Turbomachinery Flows</h1>.” 2015. Web. 18 Mar 2019.

Vancouver:

Jaffa NA. Unsteady Measurement Techniques for Turbomachinery Flows</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2015. [cited 2019 Mar 18]. Available from: https://curate.nd.edu/show/w9504x54160.

Council of Science Editors:

Jaffa NA. Unsteady Measurement Techniques for Turbomachinery Flows</h1>. [Doctoral Dissertation]. University of Notre Dame; 2015. Available from: https://curate.nd.edu/show/w9504x54160


Penn State University

10. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Kane MA. STUDY OF GAS TURBINE BLADE CONJUGATE HEAT TRANSFER TO DETERMINE BLADE TEMPERATURES. [Internet] [Masters thesis]. Penn State University; 2009. [cited 2019 Mar 18]. 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

11. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

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 2019 Mar 18]. 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

12. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wang, L. (2013). Study of gas turbine ingress using computational fluid dynamics. (Doctoral Dissertation). University of Bath. Retrieved from 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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Wang L. Study of gas turbine ingress using computational fluid dynamics. [Internet] [Doctoral dissertation]. University of Bath; 2013. [cited 2019 Mar 18]. Available from: 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://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604894


Virginia Tech

13. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

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 2019 Mar 18]. 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

14. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Schmitz JT. Experimental Measurements in a Highly Loaded Low Pressure Turbine</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2010. [cited 2019 Mar 18]. 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

15. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Bauwens PL. Gas path analysis for the MTT micro turbine:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Mar 18]. 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


Brno University of Technology

16. Drábek, Ivo. Energetický zdroj se spalovací turbinou .

Degree: 2012, Brno University of Technology

 Cílem diplomové práce je vytvoření projektu energetického zdroje se spalovací turbínou o výkonu 50 MWe, pro danou lokalitu. Jedná se tedy o vhodný výběr spalovací… (more)

Subjects/Keywords: Energetický zdroj; spalovací turbína; paroplynový blok; kogenerace; vzduchový kondenzátor; ohřívák topné vody; dispoziční návrh; tepelné schéma.; Power plant; gas turbine; combined gas and steam (COGAS); cogeneration; air condenser; hot water heater; layout design; thermal diagram.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Drábek, I. (2012). Energetický zdroj se spalovací turbinou . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/5385

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):

Drábek, Ivo. “Energetický zdroj se spalovací turbinou .” 2012. Thesis, Brno University of Technology. Accessed March 18, 2019. http://hdl.handle.net/11012/5385.

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

MLA Handbook (7th Edition):

Drábek, Ivo. “Energetický zdroj se spalovací turbinou .” 2012. Web. 18 Mar 2019.

Vancouver:

Drábek I. Energetický zdroj se spalovací turbinou . [Internet] [Thesis]. Brno University of Technology; 2012. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/11012/5385.

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

Council of Science Editors:

Drábek I. Energetický zdroj se spalovací turbinou . [Thesis]. Brno University of Technology; 2012. Available from: http://hdl.handle.net/11012/5385

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


University of Tennessee – Knoxville

17. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Hartman JA. Design and Fabrication of a Low-Cost Turbine Engine Component Testbed (TECT). [Internet] [Thesis]. University of Tennessee – Knoxville; 2014. [cited 2019 Mar 18]. 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

18. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Ashirvadam K. Combustion Instability Screech In Gas Turbine Afterburner. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 Mar 18]. 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


University of Canterbury

19. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Asgari H. Modelling, Simulation and Control of Gas Turbines Using Artificial Neural Networks. [Internet] [Thesis]. University of Canterbury; 2014. [cited 2019 Mar 18]. 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


Georgia Tech

20. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Chen G. Fiber adsorbents for tert-butyl mercaptan removal from pipeline grade natural gas. [Internet] [Masters thesis]. Georgia Tech; 2013. [cited 2019 Mar 18]. 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


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: 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.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9158

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):

Harmon, Weston V. “An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades. ” 2014. Thesis, Baylor University. Accessed March 18, 2019. http://hdl.handle.net/2104/9158.

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

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. 18 Mar 2019.

Vancouver:

Harmon WV. An experimental investigation of round and racetrack shaped jets for leading edge region cooling of gas turbine blades. [Internet] [Thesis]. Baylor University; 2014. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/2104/9158.

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

Council of Science Editors:

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

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


University of California – Merced

22. Johnson, Duval. CHARACTERIZING CHEMICAL CLEANERS USED IN REMOVING VARNISH IN GAS TURBINE ENGINES.

Degree: Mechanical Engineering, 2018, University of California – Merced

 Varnish is an undesirable by-product of using hydrocarbons as lubricants and hydraulic fluids. Oxidation of hydrocarbons is a natural process accelerated by heat, pressure, light… (more)

Subjects/Keywords: Mechanical engineering; Gas Turbine; Triboloby; Varnish

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Johnson, D. (2018). CHARACTERIZING CHEMICAL CLEANERS USED IN REMOVING VARNISH IN GAS TURBINE ENGINES. (Thesis). University of California – Merced. Retrieved from http://www.escholarship.org/uc/item/1m81s8qt

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):

Johnson, Duval. “CHARACTERIZING CHEMICAL CLEANERS USED IN REMOVING VARNISH IN GAS TURBINE ENGINES.” 2018. Thesis, University of California – Merced. Accessed March 18, 2019. http://www.escholarship.org/uc/item/1m81s8qt.

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

MLA Handbook (7th Edition):

Johnson, Duval. “CHARACTERIZING CHEMICAL CLEANERS USED IN REMOVING VARNISH IN GAS TURBINE ENGINES.” 2018. Web. 18 Mar 2019.

Vancouver:

Johnson D. CHARACTERIZING CHEMICAL CLEANERS USED IN REMOVING VARNISH IN GAS TURBINE ENGINES. [Internet] [Thesis]. University of California – Merced; 2018. [cited 2019 Mar 18]. Available from: http://www.escholarship.org/uc/item/1m81s8qt.

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

Council of Science Editors:

Johnson D. CHARACTERIZING CHEMICAL CLEANERS USED IN REMOVING VARNISH IN GAS TURBINE ENGINES. [Thesis]. University of California – Merced; 2018. Available from: http://www.escholarship.org/uc/item/1m81s8qt

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


Penn State University

23. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. https://etda.libraries.psu.edu/catalog/10740.

MLA Handbook (7th Edition):

Vadvadgi, Aneesh Sridhar. “CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR.” 2010. Web. 18 Mar 2019.

Vancouver:

Vadvadgi AS. CALCULATION OF TEMPERATURES IN GAS TURBINE ROTOR-STATOR. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2019 Mar 18]. 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

24. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Kirsch KL. Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 Mar 18]. 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

25. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Marzelli SB. Flameholding Studies for Lean Premixed Fuel Injectors for Application in Gas Turbine Engines. [Internet] [Masters thesis]. Penn State University; 2010. [cited 2019 Mar 18]. 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

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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Armstrong JL. Investigation of Semi‐Constant Volume Combustion for Micro Gas Turbines . [Internet] [Thesis]. University of Sydney; 2017. [cited 2019 Mar 18]. 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


Delft University of Technology

27. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

Vancouver:

Singh V. Transient modelling and analysis of the OP16 gas turbine in GSP:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Mar 18]. 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


MIT

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

Degree: PhD, Gas Turbine Laboratory, 1985, MIT

Subjects/Keywords: Gas Turbine Laboratory.

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. http://hdl.handle.net/1721.1/13815.

MLA Handbook (7th Edition):

Giles, M (Michael). “Newton solution of steady two-dimensional transonic flow .” 1985. Web. 18 Mar 2019.

Vancouver:

Giles M(. Newton solution of steady two-dimensional transonic flow . [Internet] [Doctoral dissertation]. MIT; 1985. [cited 2019 Mar 18]. 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


Virginia Tech

29. 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

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

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 18, 2019. 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. 18 Mar 2019.

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 2019 Mar 18]. 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 Pretoria

30. Miglietti, Warren Martin Andre. High strength, ductile wide gap braze joints for stationary turbine component repairs.

Degree: Materials Science and Metallurgical Engineering, 2008, University of Pretoria

 Wide cracks in land-based Ni- or Co-base superalloy turbine components are difficult to repair successfully using conventional welding or brazing techniques. This project examined the… (more)

Subjects/Keywords: Turbine components; Liquid phase diffusion brazing; Braze joints; UCTD

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Miglietti, W. M. (2008). High strength, ductile wide gap braze joints for stationary turbine component repairs. (Doctoral Dissertation). University of Pretoria. Retrieved from http://hdl.handle.net/2263/29403

Chicago Manual of Style (16th Edition):

Miglietti, Warren Martin. “High strength, ductile wide gap braze joints for stationary turbine component repairs.” 2008. Doctoral Dissertation, University of Pretoria. Accessed March 18, 2019. http://hdl.handle.net/2263/29403.

MLA Handbook (7th Edition):

Miglietti, Warren Martin. “High strength, ductile wide gap braze joints for stationary turbine component repairs.” 2008. Web. 18 Mar 2019.

Vancouver:

Miglietti WM. High strength, ductile wide gap braze joints for stationary turbine component repairs. [Internet] [Doctoral dissertation]. University of Pretoria; 2008. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/2263/29403.

Council of Science Editors:

Miglietti WM. High strength, ductile wide gap braze joints for stationary turbine component repairs. [Doctoral Dissertation]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/29403

[1] [2] [3] [4] [5] … [597]

.