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You searched for subject:(Film Cooling). Showing records 1 – 30 of 187 total matches.

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Baylor University

1. [No author]. Experimental investigation of full coverage combustor film cooling and airfoil film cooling for advanced gas turbines engines.

Degree: 2017, Baylor University

Film cooling in modern gas turbine engines uses coolant from the compressor to protect the surface of the combustor lining and turbine airfoils from the… (more)

Subjects/Keywords: Film cooling.

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APA (6th Edition):

author], [. (2017). Experimental investigation of full coverage combustor film cooling and airfoil film cooling for advanced gas turbines engines. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/10081

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

Chicago Manual of Style (16th Edition):

author], [No. “Experimental investigation of full coverage combustor film cooling and airfoil film cooling for advanced gas turbines engines. ” 2017. Thesis, Baylor University. Accessed September 17, 2019. http://hdl.handle.net/2104/10081.

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

MLA Handbook (7th Edition):

author], [No. “Experimental investigation of full coverage combustor film cooling and airfoil film cooling for advanced gas turbines engines. ” 2017. Web. 17 Sep 2019.

Vancouver:

author] [. Experimental investigation of full coverage combustor film cooling and airfoil film cooling for advanced gas turbines engines. [Internet] [Thesis]. Baylor University; 2017. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/2104/10081.

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

Council of Science Editors:

author] [. Experimental investigation of full coverage combustor film cooling and airfoil film cooling for advanced gas turbines engines. [Thesis]. Baylor University; 2017. Available from: http://hdl.handle.net/2104/10081

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


Baylor University

2. [No author]. Effect of inlet hole geometry on surface film cooling effectiveness from compound angle, shaped holes.

Degree: 2018, Baylor University

 The gas turbine engine operates at temperatures that far exceed the melting point of the metals from which they are made. Cooling air from the… (more)

Subjects/Keywords: Film cooling.

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APA (6th Edition):

author], [. (2018). Effect of inlet hole geometry on surface film cooling effectiveness from compound angle, shaped holes. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/10370

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

Chicago Manual of Style (16th Edition):

author], [No. “Effect of inlet hole geometry on surface film cooling effectiveness from compound angle, shaped holes. ” 2018. Thesis, Baylor University. Accessed September 17, 2019. http://hdl.handle.net/2104/10370.

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

MLA Handbook (7th Edition):

author], [No. “Effect of inlet hole geometry on surface film cooling effectiveness from compound angle, shaped holes. ” 2018. Web. 17 Sep 2019.

Vancouver:

author] [. Effect of inlet hole geometry on surface film cooling effectiveness from compound angle, shaped holes. [Internet] [Thesis]. Baylor University; 2018. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/2104/10370.

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

Council of Science Editors:

author] [. Effect of inlet hole geometry on surface film cooling effectiveness from compound angle, shaped holes. [Thesis]. Baylor University; 2018. Available from: http://hdl.handle.net/2104/10370

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


The Ohio State University

3. Kheniser, Issam E. Film Cooling Experiments in a Medium Duration Blowdown Facility.

Degree: MS, Mechanical Engineering, 2010, The Ohio State University

  As gas turbine engines are driven to be more efficient, quiet, and to produce less pollutant the turbine inlet temperature has a tendency to… (more)

Subjects/Keywords: Mechanical Engineering; Blowdown; Film; cooling; film-cooling

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APA (6th Edition):

Kheniser, I. E. (2010). Film Cooling Experiments in a Medium Duration Blowdown Facility. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1276540410

Chicago Manual of Style (16th Edition):

Kheniser, Issam E. “Film Cooling Experiments in a Medium Duration Blowdown Facility.” 2010. Masters Thesis, The Ohio State University. Accessed September 17, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1276540410.

MLA Handbook (7th Edition):

Kheniser, Issam E. “Film Cooling Experiments in a Medium Duration Blowdown Facility.” 2010. Web. 17 Sep 2019.

Vancouver:

Kheniser IE. Film Cooling Experiments in a Medium Duration Blowdown Facility. [Internet] [Masters thesis]. The Ohio State University; 2010. [cited 2019 Sep 17]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1276540410.

Council of Science Editors:

Kheniser IE. Film Cooling Experiments in a Medium Duration Blowdown Facility. [Masters Thesis]. The Ohio State University; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1276540410


Virginia Tech

4. 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 September 17, 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. 17 Sep 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 Sep 17]. 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


Texas A&M University

5. Liu, Kuo-Chun. Blowing Ratio Effects on Film Cooling Effectiveness.

Degree: 2010, Texas A&M University

 The research focuses on testing the film cooling effectiveness on a gas turbine blade suction side surface. The test is performed on a five bladed… (more)

Subjects/Keywords: film cooling; blowing ratio

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APA (6th Edition):

Liu, K. (2010). Blowing Ratio Effects on Film Cooling Effectiveness. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2927

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):

Liu, Kuo-Chun. “Blowing Ratio Effects on Film Cooling Effectiveness.” 2010. Thesis, Texas A&M University. Accessed September 17, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2927.

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

MLA Handbook (7th Edition):

Liu, Kuo-Chun. “Blowing Ratio Effects on Film Cooling Effectiveness.” 2010. Web. 17 Sep 2019.

Vancouver:

Liu K. Blowing Ratio Effects on Film Cooling Effectiveness. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2927.

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

Council of Science Editors:

Liu K. Blowing Ratio Effects on Film Cooling Effectiveness. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-2927

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


Louisiana State University

6. Gonzalez Rodriguez, Carlos Rene. Experimental Study of a Cascade of Low Pressure Turbine Blades with Upstream Periodic Stator Wakes.

Degree: MSME, Mechanical Engineering, 2015, Louisiana State University

 The objective of this study is to experimentally study film cooling flows. A closed-loop wind tunnel with a four passage linear cascade of US Air… (more)

Subjects/Keywords: film cooling; periodic wakes; PIV

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APA (6th Edition):

Gonzalez Rodriguez, C. R. (2015). Experimental Study of a Cascade of Low Pressure Turbine Blades with Upstream Periodic Stator Wakes. (Masters Thesis). Louisiana State University. Retrieved from etd-11122015-210639 ; https://digitalcommons.lsu.edu/gradschool_theses/1971

Chicago Manual of Style (16th Edition):

Gonzalez Rodriguez, Carlos Rene. “Experimental Study of a Cascade of Low Pressure Turbine Blades with Upstream Periodic Stator Wakes.” 2015. Masters Thesis, Louisiana State University. Accessed September 17, 2019. etd-11122015-210639 ; https://digitalcommons.lsu.edu/gradschool_theses/1971.

MLA Handbook (7th Edition):

Gonzalez Rodriguez, Carlos Rene. “Experimental Study of a Cascade of Low Pressure Turbine Blades with Upstream Periodic Stator Wakes.” 2015. Web. 17 Sep 2019.

Vancouver:

Gonzalez Rodriguez CR. Experimental Study of a Cascade of Low Pressure Turbine Blades with Upstream Periodic Stator Wakes. [Internet] [Masters thesis]. Louisiana State University; 2015. [cited 2019 Sep 17]. Available from: etd-11122015-210639 ; https://digitalcommons.lsu.edu/gradschool_theses/1971.

Council of Science Editors:

Gonzalez Rodriguez CR. Experimental Study of a Cascade of Low Pressure Turbine Blades with Upstream Periodic Stator Wakes. [Masters Thesis]. Louisiana State University; 2015. Available from: etd-11122015-210639 ; https://digitalcommons.lsu.edu/gradschool_theses/1971


Louisiana State University

7. Babaee, Hessam. Uncertainty quantification of film cooling effectiveness in gas turbines.

Degree: MS, Applied Mathematics, 2013, Louisiana State University

 In this study the effect of uncertainty of velocity ratio on jet in crossflow and particual- rly film cooling performance is studied. Direct numerical simulations… (more)

Subjects/Keywords: bifurcation; uncertainty quantification; Film cooling

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APA (6th Edition):

Babaee, H. (2013). Uncertainty quantification of film cooling effectiveness in gas turbines. (Masters Thesis). Louisiana State University. Retrieved from etd-07082013-005157 ; https://digitalcommons.lsu.edu/gradschool_theses/1389

Chicago Manual of Style (16th Edition):

Babaee, Hessam. “Uncertainty quantification of film cooling effectiveness in gas turbines.” 2013. Masters Thesis, Louisiana State University. Accessed September 17, 2019. etd-07082013-005157 ; https://digitalcommons.lsu.edu/gradschool_theses/1389.

MLA Handbook (7th Edition):

Babaee, Hessam. “Uncertainty quantification of film cooling effectiveness in gas turbines.” 2013. Web. 17 Sep 2019.

Vancouver:

Babaee H. Uncertainty quantification of film cooling effectiveness in gas turbines. [Internet] [Masters thesis]. Louisiana State University; 2013. [cited 2019 Sep 17]. Available from: etd-07082013-005157 ; https://digitalcommons.lsu.edu/gradschool_theses/1389.

Council of Science Editors:

Babaee H. Uncertainty quantification of film cooling effectiveness in gas turbines. [Masters Thesis]. Louisiana State University; 2013. Available from: etd-07082013-005157 ; https://digitalcommons.lsu.edu/gradschool_theses/1389


Louisiana State University

8. Drewes, Christopher Michael. The Design, Fabrication, and Validation of a Film Cooled Rotating Turbine Cascade with an Actively Cooled Shroud in a Closed Loop Wind Tunnel.

Degree: MSME, Mechanical Engineering, 2016, Louisiana State University

 To test shroud and blade cooling effectiveness, a closed loop, heated wind tunnel housing a film cooled rotating turbine cascade with prescribed blade and vane… (more)

Subjects/Keywords: shroud cooling; tip cooling; heat transfer; gas turbine; film cooling

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APA (6th Edition):

Drewes, C. M. (2016). The Design, Fabrication, and Validation of a Film Cooled Rotating Turbine Cascade with an Actively Cooled Shroud in a Closed Loop Wind Tunnel. (Masters Thesis). Louisiana State University. Retrieved from etd-04072016-074848 ; https://digitalcommons.lsu.edu/gradschool_theses/2030

Chicago Manual of Style (16th Edition):

Drewes, Christopher Michael. “The Design, Fabrication, and Validation of a Film Cooled Rotating Turbine Cascade with an Actively Cooled Shroud in a Closed Loop Wind Tunnel.” 2016. Masters Thesis, Louisiana State University. Accessed September 17, 2019. etd-04072016-074848 ; https://digitalcommons.lsu.edu/gradschool_theses/2030.

MLA Handbook (7th Edition):

Drewes, Christopher Michael. “The Design, Fabrication, and Validation of a Film Cooled Rotating Turbine Cascade with an Actively Cooled Shroud in a Closed Loop Wind Tunnel.” 2016. Web. 17 Sep 2019.

Vancouver:

Drewes CM. The Design, Fabrication, and Validation of a Film Cooled Rotating Turbine Cascade with an Actively Cooled Shroud in a Closed Loop Wind Tunnel. [Internet] [Masters thesis]. Louisiana State University; 2016. [cited 2019 Sep 17]. Available from: etd-04072016-074848 ; https://digitalcommons.lsu.edu/gradschool_theses/2030.

Council of Science Editors:

Drewes CM. The Design, Fabrication, and Validation of a Film Cooled Rotating Turbine Cascade with an Actively Cooled Shroud in a Closed Loop Wind Tunnel. [Masters Thesis]. Louisiana State University; 2016. Available from: etd-04072016-074848 ; https://digitalcommons.lsu.edu/gradschool_theses/2030


The Ohio State University

9. Prenter, Robin Michael Patrick. Investigating the Physics and Performance of Reverse-Oriented Film Cooling.

Degree: PhD, Aero/Astro Engineering, 2017, The Ohio State University

 Reverse-oriented film cooling, which consists of film cooling holes oriented to inject coolant in the opposite direction of the freestream, is experimentally and numerically investigated.… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Reverse film cooling; film cooling; backward injection

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APA (6th Edition):

Prenter, R. M. P. (2017). Investigating the Physics and Performance of Reverse-Oriented Film Cooling. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1500505248644198

Chicago Manual of Style (16th Edition):

Prenter, Robin Michael Patrick. “Investigating the Physics and Performance of Reverse-Oriented Film Cooling.” 2017. Doctoral Dissertation, The Ohio State University. Accessed September 17, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1500505248644198.

MLA Handbook (7th Edition):

Prenter, Robin Michael Patrick. “Investigating the Physics and Performance of Reverse-Oriented Film Cooling.” 2017. Web. 17 Sep 2019.

Vancouver:

Prenter RMP. Investigating the Physics and Performance of Reverse-Oriented Film Cooling. [Internet] [Doctoral dissertation]. The Ohio State University; 2017. [cited 2019 Sep 17]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1500505248644198.

Council of Science Editors:

Prenter RMP. Investigating the Physics and Performance of Reverse-Oriented Film Cooling. [Doctoral Dissertation]. The Ohio State University; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1500505248644198


University of Kansas

10. 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 September 17, 2019. 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. 17 Sep 2019.

Vancouver:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2019 Sep 17]. 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


University of Limerick

11. Lundy, Ross. Surface, interface and thin film studies for nano & heat transfer applications.

Degree: 2017, University of Limerick

peer-reviewed

This thesis is focused on the study of surfaces, interfaces and thin films. The main goal of this project is to produce and examine… (more)

Subjects/Keywords: heat transfer; cooling technology; thin film studies

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APA (6th Edition):

Lundy, R. (2017). Surface, interface and thin film studies for nano & heat transfer applications. (Thesis). University of Limerick. Retrieved from http://hdl.handle.net/10344/6771

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):

Lundy, Ross. “Surface, interface and thin film studies for nano & heat transfer applications.” 2017. Thesis, University of Limerick. Accessed September 17, 2019. http://hdl.handle.net/10344/6771.

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

MLA Handbook (7th Edition):

Lundy, Ross. “Surface, interface and thin film studies for nano & heat transfer applications.” 2017. Web. 17 Sep 2019.

Vancouver:

Lundy R. Surface, interface and thin film studies for nano & heat transfer applications. [Internet] [Thesis]. University of Limerick; 2017. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/10344/6771.

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

Council of Science Editors:

Lundy R. Surface, interface and thin film studies for nano & heat transfer applications. [Thesis]. University of Limerick; 2017. Available from: http://hdl.handle.net/10344/6771

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


Texas A&M University

12. Rice, Tyler Grant. Numerical Analysis of the Film Cooling Effectiveness on a Highly Loaded Low Pressure Turbine Blade in Conjunction with Endwall Effects.

Degree: 2017, Texas A&M University

 This thesis is a numerical investigation of the flow development of film coolant injected from a turbine blade with considerations to the effects of the… (more)

Subjects/Keywords: Turbine Blade; Film Cooling; Numerical Analysis

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APA (6th Edition):

Rice, T. G. (2017). Numerical Analysis of the Film Cooling Effectiveness on a Highly Loaded Low Pressure Turbine Blade in Conjunction with Endwall Effects. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/161663

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):

Rice, Tyler Grant. “Numerical Analysis of the Film Cooling Effectiveness on a Highly Loaded Low Pressure Turbine Blade in Conjunction with Endwall Effects.” 2017. Thesis, Texas A&M University. Accessed September 17, 2019. http://hdl.handle.net/1969.1/161663.

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

MLA Handbook (7th Edition):

Rice, Tyler Grant. “Numerical Analysis of the Film Cooling Effectiveness on a Highly Loaded Low Pressure Turbine Blade in Conjunction with Endwall Effects.” 2017. Web. 17 Sep 2019.

Vancouver:

Rice TG. Numerical Analysis of the Film Cooling Effectiveness on a Highly Loaded Low Pressure Turbine Blade in Conjunction with Endwall Effects. [Internet] [Thesis]. Texas A&M University; 2017. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/1969.1/161663.

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

Council of Science Editors:

Rice TG. Numerical Analysis of the Film Cooling Effectiveness on a Highly Loaded Low Pressure Turbine Blade in Conjunction with Endwall Effects. [Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/161663

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


Louisiana State University

13. Vezier, Clementine. Dynamics of vortical structures in a low-blowing-ratio pulsed transverse jet.

Degree: MSME, Mechanical Engineering, 2009, Louisiana State University

 Large Eddy Simulation is used to study the interaction of a 35° inclined jet into a crossflow. Steady state cases, with a BR ranging from… (more)

Subjects/Keywords: POD; film cooling; jet in crossflow

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APA (6th Edition):

Vezier, C. (2009). Dynamics of vortical structures in a low-blowing-ratio pulsed transverse jet. (Masters Thesis). Louisiana State University. Retrieved from etd-11052009-182655 ; https://digitalcommons.lsu.edu/gradschool_theses/4248

Chicago Manual of Style (16th Edition):

Vezier, Clementine. “Dynamics of vortical structures in a low-blowing-ratio pulsed transverse jet.” 2009. Masters Thesis, Louisiana State University. Accessed September 17, 2019. etd-11052009-182655 ; https://digitalcommons.lsu.edu/gradschool_theses/4248.

MLA Handbook (7th Edition):

Vezier, Clementine. “Dynamics of vortical structures in a low-blowing-ratio pulsed transverse jet.” 2009. Web. 17 Sep 2019.

Vancouver:

Vezier C. Dynamics of vortical structures in a low-blowing-ratio pulsed transverse jet. [Internet] [Masters thesis]. Louisiana State University; 2009. [cited 2019 Sep 17]. Available from: etd-11052009-182655 ; https://digitalcommons.lsu.edu/gradschool_theses/4248.

Council of Science Editors:

Vezier C. Dynamics of vortical structures in a low-blowing-ratio pulsed transverse jet. [Masters Thesis]. Louisiana State University; 2009. Available from: etd-11052009-182655 ; https://digitalcommons.lsu.edu/gradschool_theses/4248


Louisiana State University

14. Post, James William. Aerodynamic and heat transfer studies in a combustor-fired, fixed-vane cascade with film cooling.

Degree: MSME, Mechanical Engineering, 2009, Louisiana State University

 Pressure and heat transfer data has been generated in a high-pressure, high-temperature vane cascade. This cascade differs from many others seen in typical low-pressure facilities… (more)

Subjects/Keywords: Heat Transfer; Vane Cascade; Film Cooling; Aerodynamics

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APA (6th Edition):

Post, J. W. (2009). Aerodynamic and heat transfer studies in a combustor-fired, fixed-vane cascade with film cooling. (Masters Thesis). Louisiana State University. Retrieved from etd-04172009-120423 ; https://digitalcommons.lsu.edu/gradschool_theses/2497

Chicago Manual of Style (16th Edition):

Post, James William. “Aerodynamic and heat transfer studies in a combustor-fired, fixed-vane cascade with film cooling.” 2009. Masters Thesis, Louisiana State University. Accessed September 17, 2019. etd-04172009-120423 ; https://digitalcommons.lsu.edu/gradschool_theses/2497.

MLA Handbook (7th Edition):

Post, James William. “Aerodynamic and heat transfer studies in a combustor-fired, fixed-vane cascade with film cooling.” 2009. Web. 17 Sep 2019.

Vancouver:

Post JW. Aerodynamic and heat transfer studies in a combustor-fired, fixed-vane cascade with film cooling. [Internet] [Masters thesis]. Louisiana State University; 2009. [cited 2019 Sep 17]. Available from: etd-04172009-120423 ; https://digitalcommons.lsu.edu/gradschool_theses/2497.

Council of Science Editors:

Post JW. Aerodynamic and heat transfer studies in a combustor-fired, fixed-vane cascade with film cooling. [Masters Thesis]. Louisiana State University; 2009. Available from: etd-04172009-120423 ; https://digitalcommons.lsu.edu/gradschool_theses/2497


Louisiana State University

15. Babaee, Hessam. Analysis and optimization of film cooling effectiveness.

Degree: PhD, Mechanical Engineering, 2013, Louisiana State University

  In the first part, an optimization strategy is described that combines high-fidelity simu- lations with response surface construction, and is applied to pulsed film(more)

Subjects/Keywords: film cooling; spectral method; polynomial chaos

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APA (6th Edition):

Babaee, H. (2013). Analysis and optimization of film cooling effectiveness. (Doctoral Dissertation). Louisiana State University. Retrieved from etd-07082013-001815 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2178

Chicago Manual of Style (16th Edition):

Babaee, Hessam. “Analysis and optimization of film cooling effectiveness.” 2013. Doctoral Dissertation, Louisiana State University. Accessed September 17, 2019. etd-07082013-001815 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2178.

MLA Handbook (7th Edition):

Babaee, Hessam. “Analysis and optimization of film cooling effectiveness.” 2013. Web. 17 Sep 2019.

Vancouver:

Babaee H. Analysis and optimization of film cooling effectiveness. [Internet] [Doctoral dissertation]. Louisiana State University; 2013. [cited 2019 Sep 17]. Available from: etd-07082013-001815 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2178.

Council of Science Editors:

Babaee H. Analysis and optimization of film cooling effectiveness. [Doctoral Dissertation]. Louisiana State University; 2013. Available from: etd-07082013-001815 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2178

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

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 September 17, 2019. 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. 17 Sep 2019.

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 2019 Sep 17]. 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

17. Busche, Mitch. Experimental Investigation Of The Effect Of Turbulence On Slot-Fed Film Cooling Adiabatic Effectiveness And Downstream Heat Transfer.

Degree: MS, Mechanical Engineering, 2013, University of North Dakota

  Modern turbine designers are greatly concerned with power out and the efficiency of their engines. One way to increase the power output and effectiveness… (more)

Subjects/Keywords: Effectiveness; Film Cooling; Heat Transfer; Slot; Turbulence

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APA (6th Edition):

Busche, M. (2013). Experimental Investigation Of The Effect Of Turbulence On Slot-Fed Film Cooling Adiabatic Effectiveness And Downstream Heat Transfer. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/1405

Chicago Manual of Style (16th Edition):

Busche, Mitch. “Experimental Investigation Of The Effect Of Turbulence On Slot-Fed Film Cooling Adiabatic Effectiveness And Downstream Heat Transfer.” 2013. Masters Thesis, University of North Dakota. Accessed September 17, 2019. https://commons.und.edu/theses/1405.

MLA Handbook (7th Edition):

Busche, Mitch. “Experimental Investigation Of The Effect Of Turbulence On Slot-Fed Film Cooling Adiabatic Effectiveness And Downstream Heat Transfer.” 2013. Web. 17 Sep 2019.

Vancouver:

Busche M. Experimental Investigation Of The Effect Of Turbulence On Slot-Fed Film Cooling Adiabatic Effectiveness And Downstream Heat Transfer. [Internet] [Masters thesis]. University of North Dakota; 2013. [cited 2019 Sep 17]. Available from: https://commons.und.edu/theses/1405.

Council of Science Editors:

Busche M. Experimental Investigation Of The Effect Of Turbulence On Slot-Fed Film Cooling Adiabatic Effectiveness And Downstream Heat Transfer. [Masters Thesis]. University of North Dakota; 2013. Available from: https://commons.und.edu/theses/1405


Texas A&M University

18. Qureshi, Shamsul Arfin. Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique.

Degree: 2017, Texas A&M University

 A detailed study of various geometric & flow parameters that influence the film cooling effectiveness of gas turbine blade leading edge region was carried out.… (more)

Subjects/Keywords: Gas Turbine Blade Cooling; Film Cooling Effectiveness; Leading Edge; Showerhead; PSP

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

APA (6th Edition):

Qureshi, S. A. (2017). Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/161266

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):

Qureshi, Shamsul Arfin. “Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique.” 2017. Thesis, Texas A&M University. Accessed September 17, 2019. http://hdl.handle.net/1969.1/161266.

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

MLA Handbook (7th Edition):

Qureshi, Shamsul Arfin. “Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique.” 2017. Web. 17 Sep 2019.

Vancouver:

Qureshi SA. Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique. [Internet] [Thesis]. Texas A&M University; 2017. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/1969.1/161266.

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

Council of Science Editors:

Qureshi SA. Gas Turbine Blade Leading Edge Profile Effect on Film Cooling Effectiveness Using PSP Technique. [Thesis]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/161266

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


Penn State University

19. Thrift, Alan Albright. Cooling of a Turbine Vane Endwall Through Contouring and Flow Injection.

Degree: PhD, Mechanical Engineering, 2011, Penn State University

 High oil prices and environmental concerns serve to drive up the efficiencies of land based, power generation gas turbines. Increasing efficiencies requires raising the temperature… (more)

Subjects/Keywords: Gas Turbine Cooling; Endwall Contouring; Film Cooling; First Stage Vane

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

APA (6th Edition):

Thrift, A. A. (2011). Cooling of a Turbine Vane Endwall Through Contouring and Flow Injection. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/12136

Chicago Manual of Style (16th Edition):

Thrift, Alan Albright. “Cooling of a Turbine Vane Endwall Through Contouring and Flow Injection.” 2011. Doctoral Dissertation, Penn State University. Accessed September 17, 2019. https://etda.libraries.psu.edu/catalog/12136.

MLA Handbook (7th Edition):

Thrift, Alan Albright. “Cooling of a Turbine Vane Endwall Through Contouring and Flow Injection.” 2011. Web. 17 Sep 2019.

Vancouver:

Thrift AA. Cooling of a Turbine Vane Endwall Through Contouring and Flow Injection. [Internet] [Doctoral dissertation]. Penn State University; 2011. [cited 2019 Sep 17]. Available from: https://etda.libraries.psu.edu/catalog/12136.

Council of Science Editors:

Thrift AA. Cooling of a Turbine Vane Endwall Through Contouring and Flow Injection. [Doctoral Dissertation]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/12136


Texas A&M University

20. Meador, Charles Michael. Massively-Parallel Direct Numerical Simulation of Gas Turbine Endwall Film-Cooling Conjugate Heat Transfer.

Degree: 2011, Texas A&M University

 Improvements to gas turbine efficiency depend closely on cooling technologies, as efficiency increases with turbine inlet temperature. To aid in this process, simulations that consider… (more)

Subjects/Keywords: Parallel; Film; Cooling; Film Cooling; Conjugate; Heat Transfer; Gas; Gas Turbine; Endwall; Efficiency

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APA (6th Edition):

Meador, C. M. (2011). Massively-Parallel Direct Numerical Simulation of Gas Turbine Endwall Film-Cooling Conjugate Heat Transfer. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8952

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):

Meador, Charles Michael. “Massively-Parallel Direct Numerical Simulation of Gas Turbine Endwall Film-Cooling Conjugate Heat Transfer.” 2011. Thesis, Texas A&M University. Accessed September 17, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8952.

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

MLA Handbook (7th Edition):

Meador, Charles Michael. “Massively-Parallel Direct Numerical Simulation of Gas Turbine Endwall Film-Cooling Conjugate Heat Transfer.” 2011. Web. 17 Sep 2019.

Vancouver:

Meador CM. Massively-Parallel Direct Numerical Simulation of Gas Turbine Endwall Film-Cooling Conjugate Heat Transfer. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8952.

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

Council of Science Editors:

Meador CM. Massively-Parallel Direct Numerical Simulation of Gas Turbine Endwall Film-Cooling Conjugate Heat Transfer. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-12-8952

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


Penn State University

21. Baek, Seung. EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AND BLOWING RATIOS.

Degree: 2018, Penn State University

 The objective of this study was to investigate the effects of oscillations in the main flow on gas turbine film cooling at various single frequencies… (more)

Subjects/Keywords: Film cooling; Turbulent flows; Numerical simulation; Film cooling effectiveness; Stanton number ratio

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

APA (6th Edition):

Baek, S. (2018). EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AND BLOWING RATIOS. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/15762sub208

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):

Baek, Seung. “EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AND BLOWING RATIOS.” 2018. Thesis, Penn State University. Accessed September 17, 2019. https://etda.libraries.psu.edu/catalog/15762sub208.

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

MLA Handbook (7th Edition):

Baek, Seung. “EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AND BLOWING RATIOS.” 2018. Web. 17 Sep 2019.

Vancouver:

Baek S. EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AND BLOWING RATIOS. [Internet] [Thesis]. Penn State University; 2018. [cited 2019 Sep 17]. Available from: https://etda.libraries.psu.edu/catalog/15762sub208.

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

Council of Science Editors:

Baek S. EFFECTS OF OSCILLATIONS IN THE MAIN FLOW ON FILM COOLING AT VARIOUS FREQUENCIES AND BLOWING RATIOS. [Thesis]. Penn State University; 2018. Available from: https://etda.libraries.psu.edu/catalog/15762sub208

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


NSYSU

22. Yeh, Yi-Fan. Spray Cooling Thermal and Flow Characteristics for High Power Electronic Devices.

Degree: Master, Mechanical and Electro-Mechanical Engineering, 2017, NSYSU

 The purpose of this experiment is to use the piezoelectric atomizer film as a nozzle, set up a high-power electronic devices (⥠100W COB LED)… (more)

Subjects/Keywords: LED cooling; μPIV; μIPI; High powered electronic devices; Spray cooling; Piezoelectric atomizer film

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APA (6th Edition):

Yeh, Y. (2017). Spray Cooling Thermal and Flow Characteristics for High Power Electronic Devices. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0711117-201256

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):

Yeh, Yi-Fan. “Spray Cooling Thermal and Flow Characteristics for High Power Electronic Devices.” 2017. Thesis, NSYSU. Accessed September 17, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0711117-201256.

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

MLA Handbook (7th Edition):

Yeh, Yi-Fan. “Spray Cooling Thermal and Flow Characteristics for High Power Electronic Devices.” 2017. Web. 17 Sep 2019.

Vancouver:

Yeh Y. Spray Cooling Thermal and Flow Characteristics for High Power Electronic Devices. [Internet] [Thesis]. NSYSU; 2017. [cited 2019 Sep 17]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0711117-201256.

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

Council of Science Editors:

Yeh Y. Spray Cooling Thermal and Flow Characteristics for High Power Electronic Devices. [Thesis]. NSYSU; 2017. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0711117-201256

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


University of Cincinnati

23. LITZLER, JEFFREY W. COMPUTATIONAL SIMULATION AND ANALYSIS OF FILM COOLING FOR THE LEADING-EDGE MODEL OF A TURBINE BLADE.

Degree: MS, Engineering : Mechanical Engineering, 2007, University of Cincinnati

 The application of interest is the cooling of turbine blades in large gas combustion engines where hot gases from the combustor cause thermal deterioration of… (more)

Subjects/Keywords: Engineering, Mechanical; film-cooling; cooling effectiveness; leading-edge; bluff-body; heat transfer

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APA (6th Edition):

LITZLER, J. W. (2007). COMPUTATIONAL SIMULATION AND ANALYSIS OF FILM COOLING FOR THE LEADING-EDGE MODEL OF A TURBINE BLADE. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1179521120

Chicago Manual of Style (16th Edition):

LITZLER, JEFFREY W. “COMPUTATIONAL SIMULATION AND ANALYSIS OF FILM COOLING FOR THE LEADING-EDGE MODEL OF A TURBINE BLADE.” 2007. Masters Thesis, University of Cincinnati. Accessed September 17, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1179521120.

MLA Handbook (7th Edition):

LITZLER, JEFFREY W. “COMPUTATIONAL SIMULATION AND ANALYSIS OF FILM COOLING FOR THE LEADING-EDGE MODEL OF A TURBINE BLADE.” 2007. Web. 17 Sep 2019.

Vancouver:

LITZLER JW. COMPUTATIONAL SIMULATION AND ANALYSIS OF FILM COOLING FOR THE LEADING-EDGE MODEL OF A TURBINE BLADE. [Internet] [Masters thesis]. University of Cincinnati; 2007. [cited 2019 Sep 17]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1179521120.

Council of Science Editors:

LITZLER JW. COMPUTATIONAL SIMULATION AND ANALYSIS OF FILM COOLING FOR THE LEADING-EDGE MODEL OF A TURBINE BLADE. [Masters Thesis]. University of Cincinnati; 2007. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1179521120


Penn State University

24. Topcuoglu, Ilker. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades.

Degree: MS, Aerospace Engineering, 2013, Penn State University

 A detailed review of the literature on losses associated with film cooling is given. An experimental case with two different cooling-hole geometries (Round Cylindrical Hole… (more)

Subjects/Keywords: Film cooling; gas turbine cooling; aerodynamic loss prediction; total pressure loss model

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APA (6th Edition):

Topcuoglu, I. (2013). Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19150

Chicago Manual of Style (16th Edition):

Topcuoglu, Ilker. “Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades.” 2013. Masters Thesis, Penn State University. Accessed September 17, 2019. https://etda.libraries.psu.edu/catalog/19150.

MLA Handbook (7th Edition):

Topcuoglu, Ilker. “Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades.” 2013. Web. 17 Sep 2019.

Vancouver:

Topcuoglu I. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 Sep 17]. Available from: https://etda.libraries.psu.edu/catalog/19150.

Council of Science Editors:

Topcuoglu I. Aerodynamic Loss Models and Multi-Dimensional Prediction of Discrete Hole Film Cooling on Gas Turbine Blades. [Masters Thesis]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19150


Penn State University

25. Mensch, Amy. Using Conjugate Heat Transfer to Assess the Cooling Performance on a Turbine Endwall.

Degree: PhD, Mechanical Engineering, 2015, Penn State University

 Advancements in cooling for applications such as gas turbines components require improved understanding of the complex heat transfer mechanisms and the interactions between those mechanisms.… (more)

Subjects/Keywords: gas turbine endwall; conjugate heat transfer; contoured endwall; film cooling; impingement cooling; thermal barrier coating

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

APA (6th Edition):

Mensch, A. (2015). Using Conjugate Heat Transfer to Assess the Cooling Performance on a Turbine Endwall. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/24899

Chicago Manual of Style (16th Edition):

Mensch, Amy. “Using Conjugate Heat Transfer to Assess the Cooling Performance on a Turbine Endwall.” 2015. Doctoral Dissertation, Penn State University. Accessed September 17, 2019. https://etda.libraries.psu.edu/catalog/24899.

MLA Handbook (7th Edition):

Mensch, Amy. “Using Conjugate Heat Transfer to Assess the Cooling Performance on a Turbine Endwall.” 2015. Web. 17 Sep 2019.

Vancouver:

Mensch A. Using Conjugate Heat Transfer to Assess the Cooling Performance on a Turbine Endwall. [Internet] [Doctoral dissertation]. Penn State University; 2015. [cited 2019 Sep 17]. Available from: https://etda.libraries.psu.edu/catalog/24899.

Council of Science Editors:

Mensch A. Using Conjugate Heat Transfer to Assess the Cooling Performance on a Turbine Endwall. [Doctoral Dissertation]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/24899


University of Oxford

26. Thomas, Mitra. Optimization of endwall film-cooling in axial turbines.

Degree: PhD, 2014, University of Oxford

 Considerable reductions in gas turbine weight and fuel consumption can be achieved by operating at a higher turbine entry temperature. The move to lean combustors… (more)

Subjects/Keywords: 621.43; Aerodynamics and heat transfer; aerodynamics; heat transfer; film cooling; turbine endwall cooling

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APA (6th Edition):

Thomas, M. (2014). Optimization of endwall film-cooling in axial turbines. (Doctoral Dissertation). University of Oxford. Retrieved from http://ora.ox.ac.uk/objects/uuid:e369eb63-0c99-4ded-ab05-6b050004ce4c ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.629557

Chicago Manual of Style (16th Edition):

Thomas, Mitra. “Optimization of endwall film-cooling in axial turbines.” 2014. Doctoral Dissertation, University of Oxford. Accessed September 17, 2019. http://ora.ox.ac.uk/objects/uuid:e369eb63-0c99-4ded-ab05-6b050004ce4c ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.629557.

MLA Handbook (7th Edition):

Thomas, Mitra. “Optimization of endwall film-cooling in axial turbines.” 2014. Web. 17 Sep 2019.

Vancouver:

Thomas M. Optimization of endwall film-cooling in axial turbines. [Internet] [Doctoral dissertation]. University of Oxford; 2014. [cited 2019 Sep 17]. Available from: http://ora.ox.ac.uk/objects/uuid:e369eb63-0c99-4ded-ab05-6b050004ce4c ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.629557.

Council of Science Editors:

Thomas M. Optimization of endwall film-cooling in axial turbines. [Doctoral Dissertation]. University of Oxford; 2014. Available from: http://ora.ox.ac.uk/objects/uuid:e369eb63-0c99-4ded-ab05-6b050004ce4c ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.629557


Northeastern University

27. Yao, Yuan. An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique.

Degree: MS, Department of Mechanical and Industrial Engineering, 2019, Northeastern University

 Since the invention of the gas turbine technology, countless engineers and scientists have been trying their best to refine this type of machine. One of… (more)

Subjects/Keywords: Anti-counter-rotating vortices; Blowing ratio; Film cooling; Film cooling effectiveness; Pressure Sensitive Paint; 'V-shaped' film cooling hole; Mechanical engineering; Aerospace engineering

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APA (6th Edition):

Yao, Y. (2019). An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20317909

Chicago Manual of Style (16th Edition):

Yao, Yuan. “An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique.” 2019. Masters Thesis, Northeastern University. Accessed September 17, 2019. http://hdl.handle.net/2047/D20317909.

MLA Handbook (7th Edition):

Yao, Yuan. “An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique.” 2019. Web. 17 Sep 2019.

Vancouver:

Yao Y. An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique. [Internet] [Masters thesis]. Northeastern University; 2019. [cited 2019 Sep 17]. Available from: http://hdl.handle.net/2047/D20317909.

Council of Science Editors:

Yao Y. An Experimental Film Cooling Effectiveness Introducing A New Film Hole Geometry Using Pressure Sensitive Paint Technique. [Masters Thesis]. Northeastern University; 2019. Available from: http://hdl.handle.net/2047/D20317909

28. Lambert, Océane. Solutions architecturées par fabrication additive pour refroidissement de parois de chambres de combustion : Architectured materials fabricated by additive manufacturing for surface cooling of combustion chambers.

Degree: Docteur es, 2MGE : Matériaux, Mécanique, Génie civil, Electrochimie, 2017, Grenoble Alpes

En vue de leur refroidissement, les parois de chambres de combustion aéronautiques sont perforées de trous à travers lesquels de l’air plus froid est injecté.… (more)

Subjects/Keywords: Fabrication additive; Electron Beam Melting; Matériaux poreux; Refroidissement par transpiration; Film cooling; Additive manufacturing; Electron Beam Melting; Porous materials; Transpiration cooling; Film cooling; 600

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APA (6th Edition):

Lambert, O. (2017). Solutions architecturées par fabrication additive pour refroidissement de parois de chambres de combustion : Architectured materials fabricated by additive manufacturing for surface cooling of combustion chambers. (Doctoral Dissertation). Grenoble Alpes. Retrieved from http://www.theses.fr/2017GREAI048

Chicago Manual of Style (16th Edition):

Lambert, Océane. “Solutions architecturées par fabrication additive pour refroidissement de parois de chambres de combustion : Architectured materials fabricated by additive manufacturing for surface cooling of combustion chambers.” 2017. Doctoral Dissertation, Grenoble Alpes. Accessed September 17, 2019. http://www.theses.fr/2017GREAI048.

MLA Handbook (7th Edition):

Lambert, Océane. “Solutions architecturées par fabrication additive pour refroidissement de parois de chambres de combustion : Architectured materials fabricated by additive manufacturing for surface cooling of combustion chambers.” 2017. Web. 17 Sep 2019.

Vancouver:

Lambert O. Solutions architecturées par fabrication additive pour refroidissement de parois de chambres de combustion : Architectured materials fabricated by additive manufacturing for surface cooling of combustion chambers. [Internet] [Doctoral dissertation]. Grenoble Alpes; 2017. [cited 2019 Sep 17]. Available from: http://www.theses.fr/2017GREAI048.

Council of Science Editors:

Lambert O. Solutions architecturées par fabrication additive pour refroidissement de parois de chambres de combustion : Architectured materials fabricated by additive manufacturing for surface cooling of combustion chambers. [Doctoral Dissertation]. Grenoble Alpes; 2017. Available from: http://www.theses.fr/2017GREAI048


Loughborough University

29. Martin, Damian. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.

Degree: PhD, 2013, Loughborough University

 Full-coverage or effusion cooling is commonly used in the thermal management of gas turbine combustion systems. The combustor environment is characterised by highly turbulent free-stream… (more)

Subjects/Keywords: 621.43; Heat transfer; Film cooling; Combustor; Turbulence; Effusion

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

APA (6th Edition):

Martin, D. (2013). Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844

Chicago Manual of Style (16th Edition):

Martin, Damian. “Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.” 2013. Doctoral Dissertation, Loughborough University. Accessed September 17, 2019. https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844.

MLA Handbook (7th Edition):

Martin, Damian. “Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling.” 2013. Web. 17 Sep 2019.

Vancouver:

Martin D. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2019 Sep 17]. Available from: https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844.

Council of Science Editors:

Martin D. Effects of high intensity, large-scale free-stream turbulence on combustor effusion cooling. [Doctoral Dissertation]. Loughborough University; 2013. Available from: https://dspace.lboro.ac.uk/2134/14725 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.617844


NSYSU

30. Chang, Wei-Che. Thin Film Roughened Surface Effect On Spray Cooling Heat Transfer.

Degree: Master, Mechanical and Electro-Mechanical Engineering, 2017, NSYSU

 The objective of this study was to investigate the effect of coated thin films (several nanometers thick) made from different materials on enhancing the cooling(more)

Subjects/Keywords: Thin film surface; roughness; piezoelectric plate; spray cooling; boiling curves

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

APA (6th Edition):

Chang, W. (2017). Thin Film Roughened Surface Effect On Spray Cooling Heat Transfer. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0715117-093212

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):

Chang, Wei-Che. “Thin Film Roughened Surface Effect On Spray Cooling Heat Transfer.” 2017. Thesis, NSYSU. Accessed September 17, 2019. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0715117-093212.

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

MLA Handbook (7th Edition):

Chang, Wei-Che. “Thin Film Roughened Surface Effect On Spray Cooling Heat Transfer.” 2017. Web. 17 Sep 2019.

Vancouver:

Chang W. Thin Film Roughened Surface Effect On Spray Cooling Heat Transfer. [Internet] [Thesis]. NSYSU; 2017. [cited 2019 Sep 17]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0715117-093212.

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

Council of Science Editors:

Chang W. Thin Film Roughened Surface Effect On Spray Cooling Heat Transfer. [Thesis]. NSYSU; 2017. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0715117-093212

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

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