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You searched for +publisher:"University of Texas – Austin" +contributor:("Bogard, David G."). Showing records 1 – 19 of 19 total matches.

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University of Texas – Austin

1. Winka, James R. Effects of convex curvature on adiabatic effectiveness for a film cooled turbine vane.

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

 A series of experiments were carried out to measure the effects of convex surface curvature on film cooling. In the first series of experiments cooling… (more)

Subjects/Keywords: Convex curvature; curvature; film cooling; turbine; convex; vane; turbine vane

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APA (6th Edition):

Winka, J. R. (2013). Effects of convex curvature on adiabatic effectiveness for a film cooled turbine vane. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/22268

Chicago Manual of Style (16th Edition):

Winka, James R. “Effects of convex curvature on adiabatic effectiveness for a film cooled turbine vane.” 2013. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/22268.

MLA Handbook (7th Edition):

Winka, James R. “Effects of convex curvature on adiabatic effectiveness for a film cooled turbine vane.” 2013. Web. 06 Dec 2019.

Vancouver:

Winka JR. Effects of convex curvature on adiabatic effectiveness for a film cooled turbine vane. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/22268.

Council of Science Editors:

Winka JR. Effects of convex curvature on adiabatic effectiveness for a film cooled turbine vane. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/22268

2. Mosberg, Noah Avram. Experimental investigation of the performance of a fully cooled gas turbine vane with and without mainstream flow and experimental analysis supporting the redesign of a wind tunnel test section.

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

 This study focused on experimentally determining the cooling performance of a fully cooled, scaled-up model of a C3X turbine vane. The primary objective was to… (more)

Subjects/Keywords: Wind tunnel; Film cooling; Overall effectiveness; IR camera; Thermography; Turbulence generator; Planar rods; Turbulence; Coolant loop; Diffuser; Mainstream; Gas turbine, Cooling effectiveness; Hot wire; Turbulence intensity; Integral length scale; Isotropic turbulence; Isotropy; Experimental; C3X; Turbulence correlation

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APA (6th Edition):

Mosberg, N. A. (2013). Experimental investigation of the performance of a fully cooled gas turbine vane with and without mainstream flow and experimental analysis supporting the redesign of a wind tunnel test section. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/28499

Chicago Manual of Style (16th Edition):

Mosberg, Noah Avram. “Experimental investigation of the performance of a fully cooled gas turbine vane with and without mainstream flow and experimental analysis supporting the redesign of a wind tunnel test section.” 2013. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/28499.

MLA Handbook (7th Edition):

Mosberg, Noah Avram. “Experimental investigation of the performance of a fully cooled gas turbine vane with and without mainstream flow and experimental analysis supporting the redesign of a wind tunnel test section.” 2013. Web. 06 Dec 2019.

Vancouver:

Mosberg NA. Experimental investigation of the performance of a fully cooled gas turbine vane with and without mainstream flow and experimental analysis supporting the redesign of a wind tunnel test section. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/28499.

Council of Science Editors:

Mosberg NA. Experimental investigation of the performance of a fully cooled gas turbine vane with and without mainstream flow and experimental analysis supporting the redesign of a wind tunnel test section. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/28499


University of Texas – Austin

3. -3010-1887. Evaluation of film cooling superposition method on the suction side of a blade model.

Degree: MSin Engineering, Mechanical Engineering, 2019, University of Texas – Austin

 Film cooling is often used for turbine airfoil cooling, and there are numerous studies of the performance of a single row of holes. Typically, blades… (more)

Subjects/Keywords: Film cooling; Superposition; Blade; Suction side; Shaped hole

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APA (6th Edition):

-3010-1887. (2019). Evaluation of film cooling superposition method on the suction side of a blade model. (Masters Thesis). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/1454

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-3010-1887. “Evaluation of film cooling superposition method on the suction side of a blade model.” 2019. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://dx.doi.org/10.26153/tsw/1454.

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

MLA Handbook (7th Edition):

-3010-1887. “Evaluation of film cooling superposition method on the suction side of a blade model.” 2019. Web. 06 Dec 2019.

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

Vancouver:

-3010-1887. Evaluation of film cooling superposition method on the suction side of a blade model. [Internet] [Masters thesis]. University of Texas – Austin; 2019. [cited 2019 Dec 06]. Available from: http://dx.doi.org/10.26153/tsw/1454.

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

Council of Science Editors:

-3010-1887. Evaluation of film cooling superposition method on the suction side of a blade model. [Masters Thesis]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/1454

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


University of Texas – Austin

4. Klavetter, Sean Robert. Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes.

Degree: MSin Engineering, Mechanical Engineering, 2014, University of Texas – Austin

 Internal crossflow is an important element to actual gas turbine blade cooling; however, there are very few studies in open literature that have documented its… (more)

Subjects/Keywords: Film cooling; Compound angle; Crossflow; Flat plate; Ribs; Effectiveness

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APA (6th Edition):

Klavetter, S. R. (2014). Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/26324

Chicago Manual of Style (16th Edition):

Klavetter, Sean Robert. “Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes.” 2014. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/26324.

MLA Handbook (7th Edition):

Klavetter, Sean Robert. “Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes.” 2014. Web. 06 Dec 2019.

Vancouver:

Klavetter SR. Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes. [Internet] [Masters thesis]. University of Texas – Austin; 2014. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/26324.

Council of Science Editors:

Klavetter SR. Internal crossflow effects on turbine airfoil film cooling adiabatic effectiveness with compound angle round holes. [Masters Thesis]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/26324


University of Texas – Austin

5. -2404-5268. Measurements of adiabatic effectiveness from full coverage film cooling on a scaled turbine vane with laidback fanshaped holes.

Degree: MSin Engineering, Mechanical Engineering, 2017, University of Texas – Austin

 This study was focused on measurements of adiabatic effectiveness on a scaled turbine vane which made use of a contoured endwall to match engine conditions.… (more)

Subjects/Keywords: Film cooling; Shaped holes; Full coverage; Laidback fanshaped holes; Adiabatic effectiveness; Turbine vane

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APA (6th Edition):

-2404-5268. (2017). Measurements of adiabatic effectiveness from full coverage film cooling on a scaled turbine vane with laidback fanshaped holes. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/64121

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-2404-5268. “Measurements of adiabatic effectiveness from full coverage film cooling on a scaled turbine vane with laidback fanshaped holes.” 2017. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/64121.

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

MLA Handbook (7th Edition):

-2404-5268. “Measurements of adiabatic effectiveness from full coverage film cooling on a scaled turbine vane with laidback fanshaped holes.” 2017. Web. 06 Dec 2019.

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

Vancouver:

-2404-5268. Measurements of adiabatic effectiveness from full coverage film cooling on a scaled turbine vane with laidback fanshaped holes. [Internet] [Masters thesis]. University of Texas – Austin; 2017. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/64121.

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

Council of Science Editors:

-2404-5268. Measurements of adiabatic effectiveness from full coverage film cooling on a scaled turbine vane with laidback fanshaped holes. [Masters Thesis]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/64121

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Author name may be incomplete


University of Texas – Austin

6. -9627-1539. Using contoured endwalls to achieve proper scaling for a gas turbine vane model using a low speed testing facility.

Degree: MSin Engineering, Mechanical Engineering, 2015, University of Texas – Austin

 The testing of gas turbine vane and blade models is often performed in low speed, large scale infinite cascade facilities to allow for more precise… (more)

Subjects/Keywords: Endwall; Heat transfer; Coefficient; Vane; Low speed facility; Simulated infinite cascade; Pressure distribution; Turbine cooling

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APA (6th Edition):

-9627-1539. (2015). Using contoured endwalls to achieve proper scaling for a gas turbine vane model using a low speed testing facility. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31987

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

Chicago Manual of Style (16th Edition):

-9627-1539. “Using contoured endwalls to achieve proper scaling for a gas turbine vane model using a low speed testing facility.” 2015. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/31987.

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

MLA Handbook (7th Edition):

-9627-1539. “Using contoured endwalls to achieve proper scaling for a gas turbine vane model using a low speed testing facility.” 2015. Web. 06 Dec 2019.

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

Vancouver:

-9627-1539. Using contoured endwalls to achieve proper scaling for a gas turbine vane model using a low speed testing facility. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/31987.

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

Council of Science Editors:

-9627-1539. Using contoured endwalls to achieve proper scaling for a gas turbine vane model using a low speed testing facility. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31987

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Author name may be incomplete


University of Texas – Austin

7. -5775-5362. Experimentally determined external heat transfer coefficient of a turbine airfoil design at varying incidence angles.

Degree: MSin Engineering, Mechanical Engineering, 2015, University of Texas – Austin

 Predicting and measuring external heat transfer coefficients of hot gas path turbine components are important tools for gas turbine designers. Inlet temperatures often exceed the… (more)

Subjects/Keywords: Heat transfer coefficient; Turbine airfoil; Turbine; Experimental; Incidence; Incidence angle

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APA (6th Edition):

-5775-5362. (2015). Experimentally determined external heat transfer coefficient of a turbine airfoil design at varying incidence angles. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/40982

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

Chicago Manual of Style (16th Edition):

-5775-5362. “Experimentally determined external heat transfer coefficient of a turbine airfoil design at varying incidence angles.” 2015. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/40982.

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

MLA Handbook (7th Edition):

-5775-5362. “Experimentally determined external heat transfer coefficient of a turbine airfoil design at varying incidence angles.” 2015. Web. 06 Dec 2019.

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

Vancouver:

-5775-5362. Experimentally determined external heat transfer coefficient of a turbine airfoil design at varying incidence angles. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/40982.

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

Council of Science Editors:

-5775-5362. Experimentally determined external heat transfer coefficient of a turbine airfoil design at varying incidence angles. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/40982

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

8. McClintic, John W. Experimental investigation of overall effectiveness and coolant jet interactions on a fully cooled C3X turbine vane.

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

 This study focused on experimentally measuring the performance of a fully cooled, scaled up C3X turbine vane. Experimental measurements focused on investigating row-to-row interactions of… (more)

Subjects/Keywords: Film cooling; Overall effectiveness; Matched Biot number; C3X; Turbine; Heat transfer; Velocity fields; Thermal fields; Turbulence

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APA (6th Edition):

McClintic, J. W. (2013). Experimental investigation of overall effectiveness and coolant jet interactions on a fully cooled C3X turbine vane. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/22269

Chicago Manual of Style (16th Edition):

McClintic, John W. “Experimental investigation of overall effectiveness and coolant jet interactions on a fully cooled C3X turbine vane.” 2013. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/22269.

MLA Handbook (7th Edition):

McClintic, John W. “Experimental investigation of overall effectiveness and coolant jet interactions on a fully cooled C3X turbine vane.” 2013. Web. 06 Dec 2019.

Vancouver:

McClintic JW. Experimental investigation of overall effectiveness and coolant jet interactions on a fully cooled C3X turbine vane. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/22269.

Council of Science Editors:

McClintic JW. Experimental investigation of overall effectiveness and coolant jet interactions on a fully cooled C3X turbine vane. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/22269

9. Boyd, Emily June. Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation.

Degree: PhD, Mechanical Engineering, 2014, University of Texas – Austin

 Film cooling is used in gas turbine engines to cool turbine components. Cooler air is bled from the compressor, routed internally through turbine vanes and… (more)

Subjects/Keywords: Film cooling; Adiabatic effectiveness; Heat transfer coefficient augmentation; Scaling; Shaped holes; Flat plate

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APA (6th Edition):

Boyd, E. J. (2014). Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/24946

Chicago Manual of Style (16th Edition):

Boyd, Emily June. “Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation.” 2014. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/24946.

MLA Handbook (7th Edition):

Boyd, Emily June. “Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation.” 2014. Web. 06 Dec 2019.

Vancouver:

Boyd EJ. Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2014. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/24946.

Council of Science Editors:

Boyd EJ. Parameters that affect shaped hole film cooling performance and the effect of density ratio on heat transfer coefficient augmentation. [Doctoral Dissertation]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/24946

10. Anderson, Joshua Brian. Superposition in the leading edge region of a film cooled gas turbine vane.

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

 The leading edge of a turbine vane is subject to some of the highest temperature loading within an engine, and an accurate understanding of leading… (more)

Subjects/Keywords: Gas turbine; Film cooling; Leading edge; Superposition; IR thermography; Wind tunnel; Experimental

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APA (6th Edition):

Anderson, J. B. (2013). Superposition in the leading edge region of a film cooled gas turbine vane. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/23792

Chicago Manual of Style (16th Edition):

Anderson, Joshua Brian. “Superposition in the leading edge region of a film cooled gas turbine vane.” 2013. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/23792.

MLA Handbook (7th Edition):

Anderson, Joshua Brian. “Superposition in the leading edge region of a film cooled gas turbine vane.” 2013. Web. 06 Dec 2019.

Vancouver:

Anderson JB. Superposition in the leading edge region of a film cooled gas turbine vane. [Internet] [Masters thesis]. University of Texas – Austin; 2013. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/23792.

Council of Science Editors:

Anderson JB. Superposition in the leading edge region of a film cooled gas turbine vane. [Masters Thesis]. University of Texas – Austin; 2013. Available from: http://hdl.handle.net/2152/23792

11. 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

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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 December 06, 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. 06 Dec 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 Dec 06]. 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


University of Texas – Austin

12. Shin, Jeong-Heon. Scale effects on the latent heat of phase change & the effect of dynamic contact angles on dynamic capillary pressure: Scale effects on the latent heat of phase change and the effect of dynamic contact angles on dynamic capillary pressure.

Degree: PhD, Mechanical Engineering, 2014, University of Texas – Austin

 Surface tension is an important material property that affects the behavior of micro/nano size thermal-fluid systems. In this dissertation, I investigate how surface tension affects… (more)

Subjects/Keywords: Phase change; Latent heat; Nano; Surface energy; Capillary pressure

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APA (6th Edition):

Shin, J. (2014). Scale effects on the latent heat of phase change & the effect of dynamic contact angles on dynamic capillary pressure: Scale effects on the latent heat of phase change and the effect of dynamic contact angles on dynamic capillary pressure. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/46515

Chicago Manual of Style (16th Edition):

Shin, Jeong-Heon. “Scale effects on the latent heat of phase change & the effect of dynamic contact angles on dynamic capillary pressure: Scale effects on the latent heat of phase change and the effect of dynamic contact angles on dynamic capillary pressure.” 2014. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/46515.

MLA Handbook (7th Edition):

Shin, Jeong-Heon. “Scale effects on the latent heat of phase change & the effect of dynamic contact angles on dynamic capillary pressure: Scale effects on the latent heat of phase change and the effect of dynamic contact angles on dynamic capillary pressure.” 2014. Web. 06 Dec 2019.

Vancouver:

Shin J. Scale effects on the latent heat of phase change & the effect of dynamic contact angles on dynamic capillary pressure: Scale effects on the latent heat of phase change and the effect of dynamic contact angles on dynamic capillary pressure. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2014. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/46515.

Council of Science Editors:

Shin J. Scale effects on the latent heat of phase change & the effect of dynamic contact angles on dynamic capillary pressure: Scale effects on the latent heat of phase change and the effect of dynamic contact angles on dynamic capillary pressure. [Doctoral Dissertation]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/46515


University of Texas – Austin

13. -7892-5500. Variable incidence angle film cooling experiments on a scaled up turbine airfoil model.

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

 This study focused on three main areas of research - the development of a new type of low-speed, closed-loop wind tunnel design to test at… (more)

Subjects/Keywords: Film-cooling; Gas turbine; Low-speed; Wind tunnel; Heat transfer; Incidence angle; Facility design

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APA (6th Edition):

-7892-5500. (2016). Variable incidence angle film cooling experiments on a scaled up turbine airfoil model. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68221

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-7892-5500. “Variable incidence angle film cooling experiments on a scaled up turbine airfoil model.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/68221.

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

MLA Handbook (7th Edition):

-7892-5500. “Variable incidence angle film cooling experiments on a scaled up turbine airfoil model.” 2016. Web. 06 Dec 2019.

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

Vancouver:

-7892-5500. Variable incidence angle film cooling experiments on a scaled up turbine airfoil model. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/68221.

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

Council of Science Editors:

-7892-5500. Variable incidence angle film cooling experiments on a scaled up turbine airfoil model. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/68221

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


University of Texas – Austin

14. -7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.

Degree: PhD, Civil Engineering, 2018, University of Texas – Austin

 The goal of this research is to reduce the computational cost of a fully unsteady RANS simulation for the multibody interaction problems in the ship… (more)

Subjects/Keywords: Propeller hydrodynamics; BEM/RANS; Hull propeller interaction

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APA (6th Edition):

-7364-0506. (2018). Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/68081

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-7364-0506. “Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.” 2018. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/68081.

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

MLA Handbook (7th Edition):

-7364-0506. “Numerical study of the steady/unsteady multibody interaction in ship propulsion systems.” 2018. Web. 06 Dec 2019.

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

Vancouver:

-7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2018. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/68081.

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Council of Science Editors:

-7364-0506. Numerical study of the steady/unsteady multibody interaction in ship propulsion systems. [Doctoral Dissertation]. University of Texas – Austin; 2018. Available from: http://hdl.handle.net/2152/68081

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University of Texas – Austin

15. Anderson, Joshua Brian. Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements.

Degree: PhD, Mechanical Engineering, 2017, University of Texas – Austin

 Film cooling is widely used in gas turbine engines to manage temperatures within the hot section of the engine. In this work, several investigations are… (more)

Subjects/Keywords: Film cooling; Gas turbines; Shaped film cooling holes; Compound-angle shaped holes; Boundary layer measurements

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APA (6th Edition):

Anderson, J. B. (2017). Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/76038

Chicago Manual of Style (16th Edition):

Anderson, Joshua Brian. “Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/76038.

MLA Handbook (7th Edition):

Anderson, Joshua Brian. “Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements.” 2017. Web. 06 Dec 2019.

Vancouver:

Anderson JB. Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/76038.

Council of Science Editors:

Anderson JB. Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://hdl.handle.net/2152/76038


University of Texas – Austin

16. Anderson, Joshua Brian. Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements.

Degree: PhD, Mechanical Engineering, 2017, University of Texas – Austin

 Film cooling is widely used in gas turbine engines to manage temperatures within the hot section of the engine. In this work, several investigations are… (more)

Subjects/Keywords: Film cooling; Gas turbines; Shaped film cooling holes; Compound-angle shaped holes; Boundary layer measurements

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Anderson, J. B. (2017). Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/3137

Chicago Manual of Style (16th Edition):

Anderson, Joshua Brian. “Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://dx.doi.org/10.26153/tsw/3137.

MLA Handbook (7th Edition):

Anderson, Joshua Brian. “Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements.” 2017. Web. 06 Dec 2019.

Vancouver:

Anderson JB. Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2019 Dec 06]. Available from: http://dx.doi.org/10.26153/tsw/3137.

Council of Science Editors:

Anderson JB. Investigation of approach flow parameters, scaling factors, and measurement accuracy for film cooling effectiveness and heat transfer coefficient measurements. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://dx.doi.org/10.26153/tsw/3137


University of Texas – Austin

17. -8135-3980. Multi-resolution modeling of the mitral valve : a novel computational pipeline for patient-specific simulations of valve repair.

Degree: PhD, Mechanical Engineering, 2019, University of Texas – Austin

 The mitral valve (MV) is the left atrio-ventricular heart valve that regulates blood flow direction during the cardiac cycle. Among the four heart valves, MV… (more)

Subjects/Keywords: Mitral valve; Ischemic mitral regurgitation; Mitral valve repair surgery; Computational modeling; Finite element analysis; Large deformation continuum mechanics; Structural constitutive relations; Fourier analysis; Nonlinear programming

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APA (6th Edition):

-8135-3980. (2019). Multi-resolution modeling of the mitral valve : a novel computational pipeline for patient-specific simulations of valve repair. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/1371

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-8135-3980. “Multi-resolution modeling of the mitral valve : a novel computational pipeline for patient-specific simulations of valve repair.” 2019. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://dx.doi.org/10.26153/tsw/1371.

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Author name may be incomplete

MLA Handbook (7th Edition):

-8135-3980. “Multi-resolution modeling of the mitral valve : a novel computational pipeline for patient-specific simulations of valve repair.” 2019. Web. 06 Dec 2019.

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

Vancouver:

-8135-3980. Multi-resolution modeling of the mitral valve : a novel computational pipeline for patient-specific simulations of valve repair. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2019. [cited 2019 Dec 06]. Available from: http://dx.doi.org/10.26153/tsw/1371.

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

Council of Science Editors:

-8135-3980. Multi-resolution modeling of the mitral valve : a novel computational pipeline for patient-specific simulations of valve repair. [Doctoral Dissertation]. University of Texas – Austin; 2019. Available from: http://dx.doi.org/10.26153/tsw/1371

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Author name may be incomplete


University of Texas – Austin

18. -9663-3352. Diffused-exit film cooling holes fed by an internal crossflow.

Degree: PhD, Mechanical Engineering, 2017, University of Texas – Austin

 Film cooling is an essential technology to the operation of modern gas turbine engines, allowing for greater efficiency and part durability. Due to film cooling’s… (more)

Subjects/Keywords: Film cooling; Gas turbine heat transfer; Crossflow; Experimental

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

APA (6th Edition):

-9663-3352. (2017). Diffused-exit film cooling holes fed by an internal crossflow. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://dx.doi.org/10.26153/tsw/2638

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Author name may be incomplete

Chicago Manual of Style (16th Edition):

-9663-3352. “Diffused-exit film cooling holes fed by an internal crossflow.” 2017. Doctoral Dissertation, University of Texas – Austin. Accessed December 06, 2019. http://dx.doi.org/10.26153/tsw/2638.

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

MLA Handbook (7th Edition):

-9663-3352. “Diffused-exit film cooling holes fed by an internal crossflow.” 2017. Web. 06 Dec 2019.

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

Vancouver:

-9663-3352. Diffused-exit film cooling holes fed by an internal crossflow. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2017. [cited 2019 Dec 06]. Available from: http://dx.doi.org/10.26153/tsw/2638.

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

Council of Science Editors:

-9663-3352. Diffused-exit film cooling holes fed by an internal crossflow. [Doctoral Dissertation]. University of Texas – Austin; 2017. Available from: http://dx.doi.org/10.26153/tsw/2638

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

19. -9176-1870. PIV experiment and CFD simulation of flow around cylinder.

Degree: MSin Engineering, Environmental and Water Resources Engineering, 2015, University of Texas – Austin

 This work focuses on the study of flow around cylinder with both Particle Image Velocimetry (PIV) experiment and Computational Fluid Dynamics (CFD) simulation. PIV measurements… (more)

Subjects/Keywords: PIV experiment; CFD simulation; VIV

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

APA (6th Edition):

-9176-1870. (2015). PIV experiment and CFD simulation of flow around cylinder. (Masters Thesis). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31761

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Chicago Manual of Style (16th Edition):

-9176-1870. “PIV experiment and CFD simulation of flow around cylinder.” 2015. Masters Thesis, University of Texas – Austin. Accessed December 06, 2019. http://hdl.handle.net/2152/31761.

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

MLA Handbook (7th Edition):

-9176-1870. “PIV experiment and CFD simulation of flow around cylinder.” 2015. Web. 06 Dec 2019.

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

Vancouver:

-9176-1870. PIV experiment and CFD simulation of flow around cylinder. [Internet] [Masters thesis]. University of Texas – Austin; 2015. [cited 2019 Dec 06]. Available from: http://hdl.handle.net/2152/31761.

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

Council of Science Editors:

-9176-1870. PIV experiment and CFD simulation of flow around cylinder. [Masters Thesis]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31761

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

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