Experimental and Computational Studies of Film Cooling with Compound Angle Injection

Experimental and Computational Studies of Film Cooling with Compound Angle Injection PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

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Book Description
The thermal efficiency of gas turbine systems depends largely on the turbine inlet temperature. Recent decades have seen a steady rise in the inlet temperature and a resulting reduction in fuel consumption. At the same time, it has been necessary to employ intensive cooling of the hot components. Among various cooling methods, film cooling has become a standard method for cooling of the turbine airfoils and combustion chamber walls. The University of Minnesota program is a combined experimental and computational study of various film-cooling configurations. Whereas a large number of parameters influence film cooling processes, this research focuses on compound angle injection through a single row and through two rows of holes. Later work will investigate the values of contoured hole designs. An appreciation of the advantages of compound angle injection has risen recently with the demand for more effective cooling and with improved understanding of the flow; this project should continue to further this understanding. Approaches being applied include: (1) a new measurement system that extends the mass/heat transfer analogy to obtain both local film cooling and local mass (heat) transfer results in a single system, (2) direct measurement of three-dimensional turbulent transport in a highly-disturbed flow, (3) the use of compound angle and shaped holes to optimize film cooling performance, and (4) an exploration of anisotropy corrections to turbulence modeling of film cooling jets.

Experimental and Computational Studies of Film Cooling with Compound Angle Injection

Experimental and Computational Studies of Film Cooling with Compound Angle Injection PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

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Book Description
The thermal efficiency of gas turbine systems depends largely on the turbine inlet temperature. Recent decades have seen a steady rise in the inlet temperature and a resulting reduction in fuel consumption. At the same time, it has been necessary to employ intensive cooling of the hot components. Among various cooling methods, film cooling has become a standard method for cooling of the turbine airfoils and combustion chamber walls. The University of Minnesota program is a combined experimental and computational study of various film-cooling configurations. Whereas a large number of parameters influence film cooling processes, this research focuses on compound angle injection through a single row and through two rows of holes. Later work will investigate the values of contoured hole designs. An appreciation of the advantages of compound angle injection has risen recently with the demand for more effective cooling and with improved understanding of the flow; this project should continue to further this understanding. Approaches being applied include: (1) a new measurement system that extends the mass/heat transfer analogy to obtain both local film cooling and local mass (heat) transfer results in a single system, (2) direct measurement of three-dimensional turbulent transport in a highly-disturbed flow, (3) the use of compound angle and shaped holes to optimize film cooling performance, and (4) an exploration of anisotropy corrections to turbulence modeling of film cooling jets.

A Computational Study of Discrete Jet Film Cooling with Compound-angle Injection

A Computational Study of Discrete Jet Film Cooling with Compound-angle Injection PDF Author: Kevin Thomas McGovern
Publisher:
ISBN:
Category :
Languages : en
Pages : 214

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Book Description


Computational Methods and Experimental Measurements XV

Computational Methods and Experimental Measurements XV PDF Author: G. M. Carlomagno
Publisher: WIT Press
ISBN: 1845645405
Category : Mathematics
Languages : en
Pages : 737

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Book Description
Containing edited versions of most of the papers presented at the Fifteenth International Conference on Computational Methods and Experimental Measurements, this book reviews the latest work on these two approaches, and the interaction between them.

Benchmarking of Computational Models Against Experimental Data for Adiabatic Film-cooling Effectiveness for Large Spacing Compound Angle Full Coverage Film Cooling Arrays

Benchmarking of Computational Models Against Experimental Data for Adiabatic Film-cooling Effectiveness for Large Spacing Compound Angle Full Coverage Film Cooling Arrays PDF Author: Simon R. Martinez
Publisher:
ISBN:
Category : Adiabatic demagnetization
Languages : en
Pages : 152

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Book Description


Theoretical, Computational, and Experimental Solutions to Thermo-Fluid Systems

Theoretical, Computational, and Experimental Solutions to Thermo-Fluid Systems PDF Author: Muthukumar Palanisamy
Publisher: Springer Nature
ISBN: 9813341653
Category : Technology & Engineering
Languages : en
Pages : 505

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Book Description
This book presents select proceedings of the International Conference on Innovations in Thermo-Fluid Engineering and Sciences (ICITFES 2020). It covers topics in theoretical and experimental fluid dynamics, numerical methods in heat transfer and fluid mechanics, different modes of heat transfer, multiphase flow, fluid machinery, fluid power, refrigeration and air conditioning, and cryogenics. The book will be helpful to the researchers, scientists, and professionals working in the field of fluid mechanics and machinery, and thermal engineering.

Computational Methods and Experimental Measurements XVI

Computational Methods and Experimental Measurements XVI PDF Author: G. M. Carlomagno
Publisher: WIT Press
ISBN: 1845647327
Category : Mathematics
Languages : en
Pages : 497

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Book Description
This book contains the results of the sixteenth in a biennial series of meetings organised by the Wessex Institute of Technology to facilitate that communication between scientists who perform experiments, researchers who develop computer codes, and those who carry out measurements on prototypes. The conference was first held in 1984. While computer models are now more reliable and better able to represent more realistic problems, experimental measurements need to be conditioned to the requirements of the computational models. Progress of engineering sciences depends on the orderly and progressive concurrent development of all three fields.The papers contained in the book cover such topics as: Computational and experimental methods; Computer interaction and control of experiments; Fluid flow; Structural and stress analysis; Computer methods; Materials characterization; Heat transfer and thermal processes; Data acquisition and signal processing; Advances in measurements and data acquisition; Multiscale modelling; Industrial applications.

Prediction of Three-dimensional Film-cooling Situations

Prediction of Three-dimensional Film-cooling Situations PDF Author: Amiram Leitner
Publisher:
ISBN:
Category :
Languages : en
Pages : 524

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Book Description


Experimental and Computational Investigation of Film Cooling on a Large Scale C3X Turbine Vane Including Conjugate Effects

Experimental and Computational Investigation of Film Cooling on a Large Scale C3X Turbine Vane Including Conjugate Effects PDF Author: Thomas Earl Dyson
Publisher:
ISBN:
Category :
Languages : en
Pages : 576

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Book Description
This study focused on the improvement of film cooling for gas turbine vanes using both computational and experimental techniques. The experimental component used a matched Biot number model to measure scaled surface temperature (overall effectiveness) distributions representative of engine conditions for two new configurations. One configuration consisted of a single row of holes on the pressure surface while the other used numerous film cooling holes over the entire vane including a showerhead. Both configurations used internal impingement cooling representative of a 1st vane. Adiabatic effectiveness was also measured. No previous studies had shown the effect of injection on the mean and fluctuating velocity profiles for the suction surface, so measurements were made at two locations immediately upstream of film cooling holes from the fully cooled cooling configuration. Different blowing conditions were evaluated. Computational tools are increasingly important in the design of advanced gas turbine engines and validation of these tools is required prior to integration into the design process. Two film cooling configurations were simulated and compared to past experimental work. Data from matched Biot number experiments was used to validate the overall effectiveness from conjugate simulations in addition to adiabatic effectiveness. A simulation of a single row of cooling holes on the suction side also gave additional insight into the interaction of film cooling jets with the thermal boundary layer. A showerhead configuration was also simulated. The final portion of this study sought to evaluate the performance of six RANS models (standard, realizable, and renormalization group k-[epsilon]; standard k-[omega]; k-[omega] SST; and Transition SST) with respect to the prediction of thermal boundary layers. The turbulent Prandtl number was varied to test a simple method for improvement of the thermal boundary layer predictions.

Recent Advances In Computational Science And Engineering - Proceedings Of The International Conference On Scientific And Engineering Computation (Ic-sec) 2002

Recent Advances In Computational Science And Engineering - Proceedings Of The International Conference On Scientific And Engineering Computation (Ic-sec) 2002 PDF Author: Justin Kwok
Publisher: World Scientific
ISBN: 1783261064
Category : Computers
Languages : en
Pages : 952

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Book Description
IC-SEC 2002 serves as a forum for engineers and scientists who are involved in the use of high performance computers, advanced numerical strategies, computational methods and simulation in various scientific and engineering disciplines. The conference creates a platform for presenting and discussing the latest trends and findings about the state of the art in their particular field(s) of interest. IC-SEC also provides a forum for the interdisciplinary blending of computational efforts in various diversified areas of science, such as biology, chemistry, physics and materials science, as well as all branches of engineering. The proceedings cover a broad range of topics and an application area which involves modelling and simulation work using high performance computers.

Experimental and Computational Study of the Effect of Shocks on Film Cooling Effectiveness in Scramjet Combustors

Experimental and Computational Study of the Effect of Shocks on Film Cooling Effectiveness in Scramjet Combustors PDF Author: Pradeep S. Kamath
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description