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You searched for subject:(Turbine blade internal cooling). Showing records 1 – 30 of 11814 total matches.

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Louisiana State University

1. Segura, Del Alan. Internal Cooling Using Novel Swirl Enhancement Strategies in A Slot Shaped Single Pass Channel.

Degree: PhD, Engineering Science and Materials, 2016, Louisiana State University

 A series of heat transfer tests using a single pass slot shaped channel utilizing varying configurations of trapezoid shaped turbulence enhancement strip or varying configurations… (more)

Subjects/Keywords: Heat Transfer; Turbine Blade; Internal Cooling

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APA (6th Edition):

Segura, D. A. (2016). Internal Cooling Using Novel Swirl Enhancement Strategies in A Slot Shaped Single Pass Channel. (Doctoral Dissertation). Louisiana State University. Retrieved from etd-04112016-154606 ; https://digitalcommons.lsu.edu/gradschool_dissertations/3703

Chicago Manual of Style (16th Edition):

Segura, Del Alan. “Internal Cooling Using Novel Swirl Enhancement Strategies in A Slot Shaped Single Pass Channel.” 2016. Doctoral Dissertation, Louisiana State University. Accessed November 21, 2019. etd-04112016-154606 ; https://digitalcommons.lsu.edu/gradschool_dissertations/3703.

MLA Handbook (7th Edition):

Segura, Del Alan. “Internal Cooling Using Novel Swirl Enhancement Strategies in A Slot Shaped Single Pass Channel.” 2016. Web. 21 Nov 2019.

Vancouver:

Segura DA. Internal Cooling Using Novel Swirl Enhancement Strategies in A Slot Shaped Single Pass Channel. [Internet] [Doctoral dissertation]. Louisiana State University; 2016. [cited 2019 Nov 21]. Available from: etd-04112016-154606 ; https://digitalcommons.lsu.edu/gradschool_dissertations/3703.

Council of Science Editors:

Segura DA. Internal Cooling Using Novel Swirl Enhancement Strategies in A Slot Shaped Single Pass Channel. [Doctoral Dissertation]. Louisiana State University; 2016. Available from: etd-04112016-154606 ; https://digitalcommons.lsu.edu/gradschool_dissertations/3703


Louisiana State University

2. Saha, Krishnendu. Turbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance.

Degree: PhD, Mechanical Engineering, 2012, Louisiana State University

 Efficient cooling of gas turbine blade is imperative for safe operation of the gas turbine engine at high temperatures. In the present work, two converging… (more)

Subjects/Keywords: Turbine blade cooling; Internal cooling; Liquid crystal thermography; Lattice structure

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APA (6th Edition):

Saha, K. (2012). Turbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance. (Doctoral Dissertation). Louisiana State University. Retrieved from etd-08272012-145008 ; https://digitalcommons.lsu.edu/gradschool_dissertations/1774

Chicago Manual of Style (16th Edition):

Saha, Krishnendu. “Turbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance.” 2012. Doctoral Dissertation, Louisiana State University. Accessed November 21, 2019. etd-08272012-145008 ; https://digitalcommons.lsu.edu/gradschool_dissertations/1774.

MLA Handbook (7th Edition):

Saha, Krishnendu. “Turbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance.” 2012. Web. 21 Nov 2019.

Vancouver:

Saha K. Turbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance. [Internet] [Doctoral dissertation]. Louisiana State University; 2012. [cited 2019 Nov 21]. Available from: etd-08272012-145008 ; https://digitalcommons.lsu.edu/gradschool_dissertations/1774.

Council of Science Editors:

Saha K. Turbine Blade Internal Cooling: Trailing Edge, Coolant-Passage Entry, Bend Effect and Improvement in Thermal Performance. [Doctoral Dissertation]. Louisiana State University; 2012. Available from: etd-08272012-145008 ; https://digitalcommons.lsu.edu/gradschool_dissertations/1774


Virginia Tech

3. Song, Keun Min. Wall Modeled Large-Eddy Simulations in Rotating Systems for Applications to Turbine Blade Internal Cooling.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 Large-Eddy Simulations (LES or wall-resolved LES, WRLES) has been used extensively in capturing the physics of anisotropic turbulent flows. However, near wall turbulent scales in… (more)

Subjects/Keywords: Heat transfer; Large Eddy Simulation; Rotation; Turbine blade internal cooling; Wall layer modeling

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APA (6th Edition):

Song, K. M. (2012). Wall Modeled Large-Eddy Simulations in Rotating Systems for Applications to Turbine Blade Internal Cooling. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31080

Chicago Manual of Style (16th Edition):

Song, Keun Min. “Wall Modeled Large-Eddy Simulations in Rotating Systems for Applications to Turbine Blade Internal Cooling.” 2012. Masters Thesis, Virginia Tech. Accessed November 21, 2019. http://hdl.handle.net/10919/31080.

MLA Handbook (7th Edition):

Song, Keun Min. “Wall Modeled Large-Eddy Simulations in Rotating Systems for Applications to Turbine Blade Internal Cooling.” 2012. Web. 21 Nov 2019.

Vancouver:

Song KM. Wall Modeled Large-Eddy Simulations in Rotating Systems for Applications to Turbine Blade Internal Cooling. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/10919/31080.

Council of Science Editors:

Song KM. Wall Modeled Large-Eddy Simulations in Rotating Systems for Applications to Turbine Blade Internal Cooling. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/31080


Texas A&M University

4. 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 November 21, 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. 21 Nov 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 Nov 21]. 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


University of Kansas

5. 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 November 21, 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. 21 Nov 2019.

Vancouver:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2019 Nov 21]. 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 Pretoria

6. Scheepers, Gerard. An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole.

Degree: Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 Developments regarding internal cooling techniques have allowed the operation of modern gas turbine engines at turbine inlet temperatures which exceed the metallurgical capability of the… (more)

Subjects/Keywords: Coolant extraction; Computational fluid dynamics; Suction ratio; Heat transfer enhancement; Turbine blade; Film-cooling; Extraction angle; Internal cooling; Extraction hole; Augmentation; UCTD

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APA (6th Edition):

Scheepers, G. (2008). An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/27590

Chicago Manual of Style (16th Edition):

Scheepers, Gerard. “An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole.” 2008. Masters Thesis, University of Pretoria. Accessed November 21, 2019. http://hdl.handle.net/2263/27590.

MLA Handbook (7th Edition):

Scheepers, Gerard. “An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole.” 2008. Web. 21 Nov 2019.

Vancouver:

Scheepers G. An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/2263/27590.

Council of Science Editors:

Scheepers G. An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/27590


University of Pretoria

7. [No author]. An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole .

Degree: 2008, University of Pretoria

 Developments regarding internal cooling techniques have allowed the operation of modern gas turbine engines at turbine inlet temperatures which exceed the metallurgical capability of the… (more)

Subjects/Keywords: Coolant extraction; Computational fluid dynamics; Suction ratio; Heat transfer enhancement; Turbine blade; Film-cooling; Extraction angle; Internal cooling; Extraction hole; Augmentation; UCTD

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APA (6th Edition):

author], [. (2008). An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-08272008-163851/

Chicago Manual of Style (16th Edition):

author], [No. “An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole .” 2008. Masters Thesis, University of Pretoria. Accessed November 21, 2019. http://upetd.up.ac.za/thesis/available/etd-08272008-163851/.

MLA Handbook (7th Edition):

author], [No. “An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole .” 2008. Web. 21 Nov 2019.

Vancouver:

author] [. An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2019 Nov 21]. Available from: http://upetd.up.ac.za/thesis/available/etd-08272008-163851/.

Council of Science Editors:

author] [. An experimental and numerical study of heat transfer augmentation near the entrance to a film cooling hole . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-08272008-163851/


Virginia Tech

8. Parida, Pritish Ranjan. Optimization and Fabrication of Heat Exchangers for High-Density Power Control Unit Applications.

Degree: PhD, Mechanical Engineering, 2010, Virginia Tech

 The demand for more power and performance from electronic equipment has constantly been growing resulting in an increased amount of heat dissipation from these devices.… (more)

Subjects/Keywords: Electronic cooling; Swirl-impingement-Fin; Jet Impingement; Ribbed Mini-channel; Automotive Application; Power Converters for HEV; Thermal Management; Turbine Blade Internal Cooling

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APA (6th Edition):

Parida, P. R. (2010). Optimization and Fabrication of Heat Exchangers for High-Density Power Control Unit Applications. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77165

Chicago Manual of Style (16th Edition):

Parida, Pritish Ranjan. “Optimization and Fabrication of Heat Exchangers for High-Density Power Control Unit Applications.” 2010. Doctoral Dissertation, Virginia Tech. Accessed November 21, 2019. http://hdl.handle.net/10919/77165.

MLA Handbook (7th Edition):

Parida, Pritish Ranjan. “Optimization and Fabrication of Heat Exchangers for High-Density Power Control Unit Applications.” 2010. Web. 21 Nov 2019.

Vancouver:

Parida PR. Optimization and Fabrication of Heat Exchangers for High-Density Power Control Unit Applications. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/10919/77165.

Council of Science Editors:

Parida PR. Optimization and Fabrication of Heat Exchangers for High-Density Power Control Unit Applications. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/77165


Texas A&M University

9. 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 (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 November 21, 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. 21 Nov 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 Nov 21]. 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

10. Kistenmacher, David Alan. Experimental investigation of film cooling and thermal barrier coatings on a gas turbine vane with conjugate heat transfer effects.

Degree: MSin Engineering, Mechanical Engineering, 2013, University of Texas – Austin

 In the United States, natural gas turbine generators account for approximately 7% of the total primary energy consumed. A one percent increase in gas turbine(more)

Subjects/Keywords: Film cooling; Thermal barrier coating; TBC; Gas turbine; Heat transfer; Turbine; Combustion; Cooling; Turbine cooling; Internal cooling; Calibration; Wind tunnel; Turbine vane; Turbine blade; Vane; Blade; High temperature

…cooled first stage turbine blade (Leduc 2001). 1.3 TURBINE COOLING METHODS 1.3.1… …5 1.3 Turbine Cooling Methods… …Film Cooling Configuration on Internal Vane Cooling ........83 3.2 Effect of Varying TBC… …photograph of a film cooled first stage turbine blade (Leduc 2001). ..9 Figure 1.3.1… …Schematic of a typical internally cooled and film cooled turbine blade (Han et al. 2000)… 

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APA (6th Edition):

Kistenmacher, D. A. (2013). Experimental investigation of film cooling and thermal barrier coatings on a gas turbine vane with conjugate heat transfer effects. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/22266

Chicago Manual of Style (16th Edition):

Kistenmacher, David Alan. “Experimental investigation of film cooling and thermal barrier coatings on a gas turbine vane with conjugate heat transfer effects.” 2013. Masters Thesis, University of Texas – Austin. Accessed November 21, 2019. http://hdl.handle.net/2152/22266.

MLA Handbook (7th Edition):

Kistenmacher, David Alan. “Experimental investigation of film cooling and thermal barrier coatings on a gas turbine vane with conjugate heat transfer effects.” 2013. Web. 21 Nov 2019.

Vancouver:

Kistenmacher DA. Experimental investigation of film cooling and thermal barrier coatings on a gas turbine vane with conjugate heat transfer effects. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/2152/22266.

Council of Science Editors:

Kistenmacher DA. Experimental investigation of film cooling and thermal barrier coatings on a gas turbine vane with conjugate heat transfer effects. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/22266


Louisiana State University

11. Zhou, Fuguo. Internal cooling in ribbed rectangular (AR=4:1) passages at high rotation numbers and improvement in finning strategies.

Degree: PhD, Engineering Science and Materials, 2007, Louisiana State University

 Experimental studies have been performed on two-pass rectangular internal coolant channels with aspect ratio AR 4:1 with high rotation numbers. Three passages are investigated: smooth,… (more)

Subjects/Keywords: heat exchanger; internal passage; cooling; rotating; heat transfer; fin; turbine blade

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APA (6th Edition):

Zhou, F. (2007). Internal cooling in ribbed rectangular (AR=4:1) passages at high rotation numbers and improvement in finning strategies. (Doctoral Dissertation). Louisiana State University. Retrieved from etd-06122008-125449 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2484

Chicago Manual of Style (16th Edition):

Zhou, Fuguo. “Internal cooling in ribbed rectangular (AR=4:1) passages at high rotation numbers and improvement in finning strategies.” 2007. Doctoral Dissertation, Louisiana State University. Accessed November 21, 2019. etd-06122008-125449 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2484.

MLA Handbook (7th Edition):

Zhou, Fuguo. “Internal cooling in ribbed rectangular (AR=4:1) passages at high rotation numbers and improvement in finning strategies.” 2007. Web. 21 Nov 2019.

Vancouver:

Zhou F. Internal cooling in ribbed rectangular (AR=4:1) passages at high rotation numbers and improvement in finning strategies. [Internet] [Doctoral dissertation]. Louisiana State University; 2007. [cited 2019 Nov 21]. Available from: etd-06122008-125449 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2484.

Council of Science Editors:

Zhou F. Internal cooling in ribbed rectangular (AR=4:1) passages at high rotation numbers and improvement in finning strategies. [Doctoral Dissertation]. Louisiana State University; 2007. Available from: etd-06122008-125449 ; https://digitalcommons.lsu.edu/gradschool_dissertations/2484


Penn State University

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Kirsch, Kathryn Louise. “Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins.” 2013. Masters Thesis, Penn State University. Accessed November 21, 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. 21 Nov 2019.

Vancouver:

Kirsch KL. Pin Fin Surface Heat Transfer in Arrays of Oblong-shaped Pins. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 Nov 21]. 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


Virginia Tech

13. Lynch, Stephen P. The Effect of Endwall Contouring On Boundary Layer Development in a Turbine Blade Passage.

Degree: PhD, Mechanical Engineering, 2011, Virginia Tech

 Increased efficiency and durability of gas turbine components is driven by demands for reduced fuel consumption and increased reliability in aircraft and power generation applications.… (more)

Subjects/Keywords: Film Cooling; Turbine Blade Endwalls; Three-Dimensional Boundary Layers

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APA (6th Edition):

Lynch, S. P. (2011). The Effect of Endwall Contouring On Boundary Layer Development in a Turbine Blade Passage. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77202

Chicago Manual of Style (16th Edition):

Lynch, Stephen P. “The Effect of Endwall Contouring On Boundary Layer Development in a Turbine Blade Passage.” 2011. Doctoral Dissertation, Virginia Tech. Accessed November 21, 2019. http://hdl.handle.net/10919/77202.

MLA Handbook (7th Edition):

Lynch, Stephen P. “The Effect of Endwall Contouring On Boundary Layer Development in a Turbine Blade Passage.” 2011. Web. 21 Nov 2019.

Vancouver:

Lynch SP. The Effect of Endwall Contouring On Boundary Layer Development in a Turbine Blade Passage. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/10919/77202.

Council of Science Editors:

Lynch SP. The Effect of Endwall Contouring On Boundary Layer Development in a Turbine Blade Passage. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/77202


Northeastern University

14. Zhang, Tianshu. A combined numerical and experimental study of heat transfer of a turbine airfoil cooling channel with angled ribs and a 180-degree u-bend turn.

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

Turbine airfoils cooling technology has been developing for more than 60 years to protect turbine airfoils from high temperature airflow. Rib-roughened cooling channel inside turbine(more)

Subjects/Keywords: rib roughness; turbine blade cooling; u-bend channel

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APA (6th Edition):

Zhang, T. (2018). A combined numerical and experimental study of heat transfer of a turbine airfoil cooling channel with angled ribs and a 180-degree u-bend turn. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/D20292601

Chicago Manual of Style (16th Edition):

Zhang, Tianshu. “A combined numerical and experimental study of heat transfer of a turbine airfoil cooling channel with angled ribs and a 180-degree u-bend turn.” 2018. Masters Thesis, Northeastern University. Accessed November 21, 2019. http://hdl.handle.net/2047/D20292601.

MLA Handbook (7th Edition):

Zhang, Tianshu. “A combined numerical and experimental study of heat transfer of a turbine airfoil cooling channel with angled ribs and a 180-degree u-bend turn.” 2018. Web. 21 Nov 2019.

Vancouver:

Zhang T. A combined numerical and experimental study of heat transfer of a turbine airfoil cooling channel with angled ribs and a 180-degree u-bend turn. [Internet] [Masters thesis]. Northeastern University; 2018. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/2047/D20292601.

Council of Science Editors:

Zhang T. A combined numerical and experimental study of heat transfer of a turbine airfoil cooling channel with angled ribs and a 180-degree u-bend turn. [Masters Thesis]. Northeastern University; 2018. Available from: http://hdl.handle.net/2047/D20292601


Northeastern University

15. Dorlus, Gidley E. Experimental convective heat transfer in entrance portion of rib roughened channels.

Degree: MS, Department of Mechanical and Industrial Engineering, 2013, Northeastern University

 Leading edge cooling of turbine blades is essential in the advancement of the turbine industry. There are many different methods of blade cooling, from jet… (more)

Subjects/Keywords: convective cooling; rib; roughened channel; turbine blade cooling; turbulator; Mechanical Engineering; Tribology

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

APA (6th Edition):

Dorlus, G. E. (2013). Experimental convective heat transfer in entrance portion of rib roughened channels. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/d20003321

Chicago Manual of Style (16th Edition):

Dorlus, Gidley E. “Experimental convective heat transfer in entrance portion of rib roughened channels.” 2013. Masters Thesis, Northeastern University. Accessed November 21, 2019. http://hdl.handle.net/2047/d20003321.

MLA Handbook (7th Edition):

Dorlus, Gidley E. “Experimental convective heat transfer in entrance portion of rib roughened channels.” 2013. Web. 21 Nov 2019.

Vancouver:

Dorlus GE. Experimental convective heat transfer in entrance portion of rib roughened channels. [Internet] [Masters thesis]. Northeastern University; 2013. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/2047/d20003321.

Council of Science Editors:

Dorlus GE. Experimental convective heat transfer in entrance portion of rib roughened channels. [Masters Thesis]. Northeastern University; 2013. Available from: http://hdl.handle.net/2047/d20003321


Texas A&M University

16. Krad, Belal. Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques.

Degree: 2013, Texas A&M University

 Various compound internal cooling techniques were investigated in this experiment to see which combinations can offer the greatest heat transfer. Combinations of rib turbulators as… (more)

Subjects/Keywords: Heat Transfer; Compound Cooling Techniques; Rib turbulators; Pin-Fins; Jet impingement; gas turbine; internal cooling; Nusselt number; thermal performance; mid-chord region of blade; rectangular channel; Reynolds number; copper plate; steady state; thermocouples

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APA (6th Edition):

Krad, B. (2013). Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/151917

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):

Krad, Belal. “Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques.” 2013. Thesis, Texas A&M University. Accessed November 21, 2019. http://hdl.handle.net/1969.1/151917.

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

MLA Handbook (7th Edition):

Krad, Belal. “Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques.” 2013. Web. 21 Nov 2019.

Vancouver:

Krad B. Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques. [Internet] [Thesis]. Texas A&M University; 2013. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/1969.1/151917.

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

Council of Science Editors:

Krad B. Heat Transfer Enhancement in Rectangular Channel with Compound Cooling Techniques. [Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/151917

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


University of Manchester

17. Jousselin, Olivier Yves Jean pierre. Development of Blade Tip Timing Techniques in Turbo Machinery.

Degree: 2013, University of Manchester

 In the current gas turbine market, the traditional design-test-redesign loop is not a viable solution to deploy new products within short timeframes. Hence, to keep… (more)

Subjects/Keywords: Blade Tip Timing; Turbine Blade

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

APA (6th Edition):

Jousselin, O. Y. J. p. (2013). Development of Blade Tip Timing Techniques in Turbo Machinery. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:211617

Chicago Manual of Style (16th Edition):

Jousselin, Olivier Yves Jean pierre. “Development of Blade Tip Timing Techniques in Turbo Machinery.” 2013. Doctoral Dissertation, University of Manchester. Accessed November 21, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:211617.

MLA Handbook (7th Edition):

Jousselin, Olivier Yves Jean pierre. “Development of Blade Tip Timing Techniques in Turbo Machinery.” 2013. Web. 21 Nov 2019.

Vancouver:

Jousselin OYJp. Development of Blade Tip Timing Techniques in Turbo Machinery. [Internet] [Doctoral dissertation]. University of Manchester; 2013. [cited 2019 Nov 21]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:211617.

Council of Science Editors:

Jousselin OYJp. Development of Blade Tip Timing Techniques in Turbo Machinery. [Doctoral Dissertation]. University of Manchester; 2013. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:211617


University of Manchester

18. Jousselin, Olivier. Development of blade tip timing techniques in turbo machinery.

Degree: Thesis (Eng.D.), 2013, University of Manchester

 In the current gas turbine market, the traditional design-test-redesign loop is not a viable solution to deploy new products within short timeframes. Hence, to keep… (more)

Subjects/Keywords: Blade Tip Timing; Turbine Blade

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

APA (6th Edition):

Jousselin, O. (2013). Development of blade tip timing techniques in turbo machinery. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/development-of-blade-tip-timing-techniques-in-turbo-machinery(da682144-7009-4cdc-8f52-ff7cd0cf1cf1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.764241

Chicago Manual of Style (16th Edition):

Jousselin, Olivier. “Development of blade tip timing techniques in turbo machinery.” 2013. Doctoral Dissertation, University of Manchester. Accessed November 21, 2019. https://www.research.manchester.ac.uk/portal/en/theses/development-of-blade-tip-timing-techniques-in-turbo-machinery(da682144-7009-4cdc-8f52-ff7cd0cf1cf1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.764241.

MLA Handbook (7th Edition):

Jousselin, Olivier. “Development of blade tip timing techniques in turbo machinery.” 2013. Web. 21 Nov 2019.

Vancouver:

Jousselin O. Development of blade tip timing techniques in turbo machinery. [Internet] [Doctoral dissertation]. University of Manchester; 2013. [cited 2019 Nov 21]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/development-of-blade-tip-timing-techniques-in-turbo-machinery(da682144-7009-4cdc-8f52-ff7cd0cf1cf1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.764241.

Council of Science Editors:

Jousselin O. Development of blade tip timing techniques in turbo machinery. [Doctoral Dissertation]. University of Manchester; 2013. Available from: https://www.research.manchester.ac.uk/portal/en/theses/development-of-blade-tip-timing-techniques-in-turbo-machinery(da682144-7009-4cdc-8f52-ff7cd0cf1cf1).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.764241


University of Manchester

19. Al-Zurfi, Nabeel Mohammed Jasim. Large Eddy Simulation of Cooling Practices for Improved Film Cooling Performance of a Gas Turbine Blade.

Degree: 2016, University of Manchester

 The Large Eddy Simulation approach is employed to predict the flow physics and heat transfer characteristics of a film-cooling problem that is formed from the… (more)

Subjects/Keywords: Film cooling effectiveness; Flat plate; Gas turbine blade; rotor blade; Anti-vortex holes; Large eddy simulation

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

APA (6th Edition):

Al-Zurfi, N. M. J. (2016). Large Eddy Simulation of Cooling Practices for Improved Film Cooling Performance of a Gas Turbine Blade. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:305150

Chicago Manual of Style (16th Edition):

Al-Zurfi, Nabeel Mohammed Jasim. “Large Eddy Simulation of Cooling Practices for Improved Film Cooling Performance of a Gas Turbine Blade.” 2016. Doctoral Dissertation, University of Manchester. Accessed November 21, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:305150.

MLA Handbook (7th Edition):

Al-Zurfi, Nabeel Mohammed Jasim. “Large Eddy Simulation of Cooling Practices for Improved Film Cooling Performance of a Gas Turbine Blade.” 2016. Web. 21 Nov 2019.

Vancouver:

Al-Zurfi NMJ. Large Eddy Simulation of Cooling Practices for Improved Film Cooling Performance of a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Manchester; 2016. [cited 2019 Nov 21]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:305150.

Council of Science Editors:

Al-Zurfi NMJ. Large Eddy Simulation of Cooling Practices for Improved Film Cooling Performance of a Gas Turbine Blade. [Doctoral Dissertation]. University of Manchester; 2016. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:305150


University of Manchester

20. Al-Zurfi, Nabeel. Large eddy simulation of cooling practices for improved film cooling performance of a gas turbine blade.

Degree: PhD, 2017, University of Manchester

 The Large Eddy Simulation approach is employed to predict the flow physics and heat transfer characteristics of a film-cooling problem that is formed from the… (more)

Subjects/Keywords: 621.43; Large eddy simulation; rotor blade; Anti-vortex holes; Flat plate; Film cooling effectiveness; Gas turbine blade

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APA (6th Edition):

Al-Zurfi, N. (2017). Large eddy simulation of cooling practices for improved film cooling performance of a gas turbine blade. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/large-eddy-simulation-of-cooling-practices-for-improved-film-cooling-performance-of-a-gas-turbine-blade(966b0252-4b0e-45de-9c1f-effe007261b0).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728056

Chicago Manual of Style (16th Edition):

Al-Zurfi, Nabeel. “Large eddy simulation of cooling practices for improved film cooling performance of a gas turbine blade.” 2017. Doctoral Dissertation, University of Manchester. Accessed November 21, 2019. https://www.research.manchester.ac.uk/portal/en/theses/large-eddy-simulation-of-cooling-practices-for-improved-film-cooling-performance-of-a-gas-turbine-blade(966b0252-4b0e-45de-9c1f-effe007261b0).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728056.

MLA Handbook (7th Edition):

Al-Zurfi, Nabeel. “Large eddy simulation of cooling practices for improved film cooling performance of a gas turbine blade.” 2017. Web. 21 Nov 2019.

Vancouver:

Al-Zurfi N. Large eddy simulation of cooling practices for improved film cooling performance of a gas turbine blade. [Internet] [Doctoral dissertation]. University of Manchester; 2017. [cited 2019 Nov 21]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/large-eddy-simulation-of-cooling-practices-for-improved-film-cooling-performance-of-a-gas-turbine-blade(966b0252-4b0e-45de-9c1f-effe007261b0).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728056.

Council of Science Editors:

Al-Zurfi N. Large eddy simulation of cooling practices for improved film cooling performance of a gas turbine blade. [Doctoral Dissertation]. University of Manchester; 2017. Available from: https://www.research.manchester.ac.uk/portal/en/theses/large-eddy-simulation-of-cooling-practices-for-improved-film-cooling-performance-of-a-gas-turbine-blade(966b0252-4b0e-45de-9c1f-effe007261b0).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.728056


University of Cincinnati

21. MISHRA, SUMAN. Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model.

Degree: MS, Engineering : Mechanical Engineering, 2008, University of Cincinnati

 The present study numerically investigates the effectiveness of film cooling on a turbine blade leading-edge model through a single-hole coolant exit. The model used in… (more)

Subjects/Keywords: Engineering, Mechanical; Film cooling blowing ratio turbine blade leading edge cylindrical model

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APA (6th Edition):

MISHRA, S. (2008). Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205156648

Chicago Manual of Style (16th Edition):

MISHRA, SUMAN. “Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model.” 2008. Masters Thesis, University of Cincinnati. Accessed November 21, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205156648.

MLA Handbook (7th Edition):

MISHRA, SUMAN. “Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model.” 2008. Web. 21 Nov 2019.

Vancouver:

MISHRA S. Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model. [Internet] [Masters thesis]. University of Cincinnati; 2008. [cited 2019 Nov 21]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205156648.

Council of Science Editors:

MISHRA S. Single-Hole Film Cooling on a Turbine-Blade Leading-Edge Model. [Masters Thesis]. University of Cincinnati; 2008. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1205156648


Louisiana State University

22. Kramer, Gregory. Gas Turbine Blade Tip and Near Tip Heat Transfer with Film Cooling.

Degree: MSME, Mechanical Engineering, 2011, Louisiana State University

 Gas turbine blade tips experience very high thermal loads due to high temperature combustion gases and tip leakage flows. This leads to the tip region… (more)

Subjects/Keywords: film cooling effectiveness; infrared; heat flux reconstruction; heat transfer coefficients; gas turbine blade tip

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APA (6th Edition):

Kramer, G. (2011). Gas Turbine Blade Tip and Near Tip Heat Transfer with Film Cooling. (Masters Thesis). Louisiana State University. Retrieved from etd-04272011-140713 ; https://digitalcommons.lsu.edu/gradschool_theses/2212

Chicago Manual of Style (16th Edition):

Kramer, Gregory. “Gas Turbine Blade Tip and Near Tip Heat Transfer with Film Cooling.” 2011. Masters Thesis, Louisiana State University. Accessed November 21, 2019. etd-04272011-140713 ; https://digitalcommons.lsu.edu/gradschool_theses/2212.

MLA Handbook (7th Edition):

Kramer, Gregory. “Gas Turbine Blade Tip and Near Tip Heat Transfer with Film Cooling.” 2011. Web. 21 Nov 2019.

Vancouver:

Kramer G. Gas Turbine Blade Tip and Near Tip Heat Transfer with Film Cooling. [Internet] [Masters thesis]. Louisiana State University; 2011. [cited 2019 Nov 21]. Available from: etd-04272011-140713 ; https://digitalcommons.lsu.edu/gradschool_theses/2212.

Council of Science Editors:

Kramer G. Gas Turbine Blade Tip and Near Tip Heat Transfer with Film Cooling. [Masters Thesis]. Louisiana State University; 2011. Available from: etd-04272011-140713 ; https://digitalcommons.lsu.edu/gradschool_theses/2212


Northeastern University

23. Fong, Michael Ka Hing. An experimental investigation of impingement heat transfer in a rib-roughened trailing-edge channel with crossover holes.

Degree: MS, Department of Mechanical and Industrial Engineering, 2010, Northeastern University

 A modern day turbine blade for a typical gas turbine usually contains rib roughened cavities which increases the cooling rate. There are several methods of… (more)

Subjects/Keywords: mechanical engineering; aerospace; impingement cooling; rib roughened; trailing edge; turbine blade; Mechanical Engineering

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APA (6th Edition):

Fong, M. K. H. (2010). An experimental investigation of impingement heat transfer in a rib-roughened trailing-edge channel with crossover holes. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/d20000328

Chicago Manual of Style (16th Edition):

Fong, Michael Ka Hing. “An experimental investigation of impingement heat transfer in a rib-roughened trailing-edge channel with crossover holes.” 2010. Masters Thesis, Northeastern University. Accessed November 21, 2019. http://hdl.handle.net/2047/d20000328.

MLA Handbook (7th Edition):

Fong, Michael Ka Hing. “An experimental investigation of impingement heat transfer in a rib-roughened trailing-edge channel with crossover holes.” 2010. Web. 21 Nov 2019.

Vancouver:

Fong MKH. An experimental investigation of impingement heat transfer in a rib-roughened trailing-edge channel with crossover holes. [Internet] [Masters thesis]. Northeastern University; 2010. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/2047/d20000328.

Council of Science Editors:

Fong MKH. An experimental investigation of impingement heat transfer in a rib-roughened trailing-edge channel with crossover holes. [Masters Thesis]. Northeastern University; 2010. Available from: http://hdl.handle.net/2047/d20000328


University of Manchester

24. Al-Aabidy, Qahtan. Modelling of turbulent flow and heat transfer in porous media for gas turbine blade cooling.

Degree: PhD, 2018, University of Manchester

 This thesis focuses on the study of flow and heat transfer in porous media in both laminar and turbulent flow regimes, by using Volume Averaged… (more)

Subjects/Keywords: fluid-porous interface; gas turbine blade cooling; turbulence modelling in porous media; porous ribs

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APA (6th Edition):

Al-Aabidy, Q. (2018). Modelling of turbulent flow and heat transfer in porous media for gas turbine blade cooling. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/modelling-of-turbulent-flow-and-heat-transfer-in-porous-media-for-gas-turbine-blade-cooling(f7781d8e-bb1e-4bb7-a57e-4e77875ad6d6).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.740417

Chicago Manual of Style (16th Edition):

Al-Aabidy, Qahtan. “Modelling of turbulent flow and heat transfer in porous media for gas turbine blade cooling.” 2018. Doctoral Dissertation, University of Manchester. Accessed November 21, 2019. https://www.research.manchester.ac.uk/portal/en/theses/modelling-of-turbulent-flow-and-heat-transfer-in-porous-media-for-gas-turbine-blade-cooling(f7781d8e-bb1e-4bb7-a57e-4e77875ad6d6).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.740417.

MLA Handbook (7th Edition):

Al-Aabidy, Qahtan. “Modelling of turbulent flow and heat transfer in porous media for gas turbine blade cooling.” 2018. Web. 21 Nov 2019.

Vancouver:

Al-Aabidy Q. Modelling of turbulent flow and heat transfer in porous media for gas turbine blade cooling. [Internet] [Doctoral dissertation]. University of Manchester; 2018. [cited 2019 Nov 21]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/modelling-of-turbulent-flow-and-heat-transfer-in-porous-media-for-gas-turbine-blade-cooling(f7781d8e-bb1e-4bb7-a57e-4e77875ad6d6).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.740417.

Council of Science Editors:

Al-Aabidy Q. Modelling of turbulent flow and heat transfer in porous media for gas turbine blade cooling. [Doctoral Dissertation]. University of Manchester; 2018. Available from: https://www.research.manchester.ac.uk/portal/en/theses/modelling-of-turbulent-flow-and-heat-transfer-in-porous-media-for-gas-turbine-blade-cooling(f7781d8e-bb1e-4bb7-a57e-4e77875ad6d6).html ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.740417


Delft University of Technology

25. Velez Isaza, A. Understanding the Mechanisms of Aero-Structural Optimization of a Wind Turbine Blade:.

Degree: 2012, Delft University of Technology

 The process of designing a wind turbine blade involves many disciplines and is of an iterative character, making it cumbersome and sometimes inefficient. In this… (more)

Subjects/Keywords: wind turbine blade

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APA (6th Edition):

Velez Isaza, A. (2012). Understanding the Mechanisms of Aero-Structural Optimization of a Wind Turbine Blade:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:824b7de5-af42-45cb-b7ad-4bb55f7c49c0

Chicago Manual of Style (16th Edition):

Velez Isaza, A. “Understanding the Mechanisms of Aero-Structural Optimization of a Wind Turbine Blade:.” 2012. Masters Thesis, Delft University of Technology. Accessed November 21, 2019. http://resolver.tudelft.nl/uuid:824b7de5-af42-45cb-b7ad-4bb55f7c49c0.

MLA Handbook (7th Edition):

Velez Isaza, A. “Understanding the Mechanisms of Aero-Structural Optimization of a Wind Turbine Blade:.” 2012. Web. 21 Nov 2019.

Vancouver:

Velez Isaza A. Understanding the Mechanisms of Aero-Structural Optimization of a Wind Turbine Blade:. [Internet] [Masters thesis]. Delft University of Technology; 2012. [cited 2019 Nov 21]. Available from: http://resolver.tudelft.nl/uuid:824b7de5-af42-45cb-b7ad-4bb55f7c49c0.

Council of Science Editors:

Velez Isaza A. Understanding the Mechanisms of Aero-Structural Optimization of a Wind Turbine Blade:. [Masters Thesis]. Delft University of Technology; 2012. Available from: http://resolver.tudelft.nl/uuid:824b7de5-af42-45cb-b7ad-4bb55f7c49c0


Virginia Tech

26. Tyagi, Kartikeya. Detailed Experimental Measurements of Heat Transfer Augmentation in Internal Channels Using a Thermochromic Liquid Crystal Technique.

Degree: MS, Mechanical Engineering, 2015, Virginia Tech

 Design of internal cooling channels for gas turbine blade is critical to system performance. To achieve maximum efficiency, i.e. maximum cooling with minimum coolant usage,… (more)

Subjects/Keywords: Heat Transfer; Gas Turbine Cooling; Internal Channel Cooling; Thermochromic Liquid Crystal Technique

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APA (6th Edition):

Tyagi, K. (2015). Detailed Experimental Measurements of Heat Transfer Augmentation in Internal Channels Using a Thermochromic Liquid Crystal Technique. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/52990

Chicago Manual of Style (16th Edition):

Tyagi, Kartikeya. “Detailed Experimental Measurements of Heat Transfer Augmentation in Internal Channels Using a Thermochromic Liquid Crystal Technique.” 2015. Masters Thesis, Virginia Tech. Accessed November 21, 2019. http://hdl.handle.net/10919/52990.

MLA Handbook (7th Edition):

Tyagi, Kartikeya. “Detailed Experimental Measurements of Heat Transfer Augmentation in Internal Channels Using a Thermochromic Liquid Crystal Technique.” 2015. Web. 21 Nov 2019.

Vancouver:

Tyagi K. Detailed Experimental Measurements of Heat Transfer Augmentation in Internal Channels Using a Thermochromic Liquid Crystal Technique. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/10919/52990.

Council of Science Editors:

Tyagi K. Detailed Experimental Measurements of Heat Transfer Augmentation in Internal Channels Using a Thermochromic Liquid Crystal Technique. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/52990


University of New South Wales

27. Forbes, Gareth Llewellyn. Non-contact gas turbine blade vibration monitoring using internal pressure and casing response measurements.

Degree: Mechanical & Manufacturing Engineering, 2010, University of New South Wales

 This thesis addresses the non-contact measurement of rotor blade vibrations in gas turbines. Specifically, use is made of internal casing wall pressure, and external casing… (more)

Subjects/Keywords: Condition monitoring; Gas Turbine; Blade vibration; Casing vibration; Internal pressure; Structural dynamics

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APA (6th Edition):

Forbes, G. L. (2010). Non-contact gas turbine blade vibration monitoring using internal pressure and casing response measurements. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/44936 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8233/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Forbes, Gareth Llewellyn. “Non-contact gas turbine blade vibration monitoring using internal pressure and casing response measurements.” 2010. Doctoral Dissertation, University of New South Wales. Accessed November 21, 2019. http://handle.unsw.edu.au/1959.4/44936 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8233/SOURCE02?view=true.

MLA Handbook (7th Edition):

Forbes, Gareth Llewellyn. “Non-contact gas turbine blade vibration monitoring using internal pressure and casing response measurements.” 2010. Web. 21 Nov 2019.

Vancouver:

Forbes GL. Non-contact gas turbine blade vibration monitoring using internal pressure and casing response measurements. [Internet] [Doctoral dissertation]. University of New South Wales; 2010. [cited 2019 Nov 21]. Available from: http://handle.unsw.edu.au/1959.4/44936 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8233/SOURCE02?view=true.

Council of Science Editors:

Forbes GL. Non-contact gas turbine blade vibration monitoring using internal pressure and casing response measurements. [Doctoral Dissertation]. University of New South Wales; 2010. Available from: http://handle.unsw.edu.au/1959.4/44936 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:8233/SOURCE02?view=true


Virginia Tech

28. Viswanathan, Aroon Kumar. Detached Eddy Simulation of Turbulent Flow and Heat Transfer in Turbine Blade Internal Cooling Ducts.

Degree: PhD, Mechanical Engineering, 2006, Virginia Tech

 Detached Eddy Simulations (DES) is a hybrid URANS-LES technique that was proposed to obtain computationally feasible solutions of high Reynolds number flows undergoing massive separation… (more)

Subjects/Keywords: Detached Eddy Simulations (DES); turbine blade internal cooling; ribbed ducts; centrifugal buoyancy; Coriolis forces

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

APA (6th Edition):

Viswanathan, A. K. (2006). Detached Eddy Simulation of Turbulent Flow and Heat Transfer in Turbine Blade Internal Cooling Ducts. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28518

Chicago Manual of Style (16th Edition):

Viswanathan, Aroon Kumar. “Detached Eddy Simulation of Turbulent Flow and Heat Transfer in Turbine Blade Internal Cooling Ducts.” 2006. Doctoral Dissertation, Virginia Tech. Accessed November 21, 2019. http://hdl.handle.net/10919/28518.

MLA Handbook (7th Edition):

Viswanathan, Aroon Kumar. “Detached Eddy Simulation of Turbulent Flow and Heat Transfer in Turbine Blade Internal Cooling Ducts.” 2006. Web. 21 Nov 2019.

Vancouver:

Viswanathan AK. Detached Eddy Simulation of Turbulent Flow and Heat Transfer in Turbine Blade Internal Cooling Ducts. [Internet] [Doctoral dissertation]. Virginia Tech; 2006. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/10919/28518.

Council of Science Editors:

Viswanathan AK. Detached Eddy Simulation of Turbulent Flow and Heat Transfer in Turbine Blade Internal Cooling Ducts. [Doctoral Dissertation]. Virginia Tech; 2006. Available from: http://hdl.handle.net/10919/28518


Penn State University

29. Ostanek, Jason. ESTABLISHING A METHODOLOGY FOR RESOLVING CONVECTIVE HEAT TRANSFER FROM COMPLEX GEOMETRIES.

Degree: MS, Mechanical Engineering, 2008, Penn State University

 Current turbine airfoils must operate at extreme temperatures, which are continuously driven higher by the demand for high output engines. Internal cooling plays a key… (more)

Subjects/Keywords: rib turbulators; internal cooling; gas turbine heat transfer; ribbed channels

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

APA (6th Edition):

Ostanek, J. (2008). ESTABLISHING A METHODOLOGY FOR RESOLVING CONVECTIVE HEAT TRANSFER FROM COMPLEX GEOMETRIES. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8142

Chicago Manual of Style (16th Edition):

Ostanek, Jason. “ESTABLISHING A METHODOLOGY FOR RESOLVING CONVECTIVE HEAT TRANSFER FROM COMPLEX GEOMETRIES.” 2008. Masters Thesis, Penn State University. Accessed November 21, 2019. https://etda.libraries.psu.edu/catalog/8142.

MLA Handbook (7th Edition):

Ostanek, Jason. “ESTABLISHING A METHODOLOGY FOR RESOLVING CONVECTIVE HEAT TRANSFER FROM COMPLEX GEOMETRIES.” 2008. Web. 21 Nov 2019.

Vancouver:

Ostanek J. ESTABLISHING A METHODOLOGY FOR RESOLVING CONVECTIVE HEAT TRANSFER FROM COMPLEX GEOMETRIES. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2019 Nov 21]. Available from: https://etda.libraries.psu.edu/catalog/8142.

Council of Science Editors:

Ostanek J. ESTABLISHING A METHODOLOGY FOR RESOLVING CONVECTIVE HEAT TRANSFER FROM COMPLEX GEOMETRIES. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8142


Virginia Tech

30. He, Long. A Study of Immersed Boundary Method in a Ribbed Duct for the Internal Cooling of Turbine Blades.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 In this dissertation, Immersed Boundary Method (IBM) is evaluated in ribbed duct geometries to show the potential of simulating complex geometry with a simple structured… (more)

Subjects/Keywords: turbine heat transfer; Immersed boundary method; wall model; internal cooling

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

APA (6th Edition):

He, L. (2014). A Study of Immersed Boundary Method in a Ribbed Duct for the Internal Cooling of Turbine Blades. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78069

Chicago Manual of Style (16th Edition):

He, Long. “A Study of Immersed Boundary Method in a Ribbed Duct for the Internal Cooling of Turbine Blades.” 2014. Masters Thesis, Virginia Tech. Accessed November 21, 2019. http://hdl.handle.net/10919/78069.

MLA Handbook (7th Edition):

He, Long. “A Study of Immersed Boundary Method in a Ribbed Duct for the Internal Cooling of Turbine Blades.” 2014. Web. 21 Nov 2019.

Vancouver:

He L. A Study of Immersed Boundary Method in a Ribbed Duct for the Internal Cooling of Turbine Blades. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2019 Nov 21]. Available from: http://hdl.handle.net/10919/78069.

Council of Science Editors:

He L. A Study of Immersed Boundary Method in a Ribbed Duct for the Internal Cooling of Turbine Blades. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/78069

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