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Film cooling from inclined cylindric...

Peet, Yulia V.

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Film cooling from inclined cylindrical holes using large eddy simulations.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Film cooling from inclined cylindrical holes using large eddy simulations./
作者:	Peet, Yulia V.
面頁冊數:	238 p.
附註:	Source: Dissertation Abstracts International, Volume: 67-09, Section: B, page: 5223.
Contained By:	Dissertation Abstracts International67-09B.
標題:	Engineering, Aerospace. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3235321
ISBN:	9780542895364

Film cooling from inclined cylindrical holes using large eddy simulations.
Peet, Yulia V.

Film cooling from inclined cylindrical holes using large eddy simulations. - 238 p.

Source: Dissertation Abstracts International, Volume: 67-09, Section: B, page: 5223.

Thesis (Ph.D.)--Stanford University, 2006.

The goal of the present study is to investigate numerically the physics of the flow, which occurs during the film cooling from inclined cylindrical holes, Film cooling is a technique used in gas turbine industry to reduce heat fluxes to the turbine blade surface. Large Eddy Simulation (LES) is performed modeling a realistic film cooling configuration, which consists of a large stagnation-type reservoir, feeding an array of discrete cooling holes (film holes) flowing into a flat plate turbulent boundary layer. Special computational methodology is developed for this problem, involving coupled simulations using multiple computational codes. A fully compressible LES code is used in the area above the flat plate, while a low Mach number LES code is employed in the plenum and film holes. The motivation for using different codes comes from the essential difference in the nature of the flow in these different regions.

ISBN: 9780542895364Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Film cooling from inclined cylindrical holes using large eddy simulations.
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245 1 0 $a Film cooling from inclined cylindrical holes using large eddy simulations.
300 $a 238 p.
500 $a Source: Dissertation Abstracts International, Volume: 67-09, Section: B, page: 5223.
500 $a Adviser: Sanjiva K. Lele.
502 $a Thesis (Ph.D.)--Stanford University, 2006.
520 $a The goal of the present study is to investigate numerically the physics of the flow, which occurs during the film cooling from inclined cylindrical holes, Film cooling is a technique used in gas turbine industry to reduce heat fluxes to the turbine blade surface. Large Eddy Simulation (LES) is performed modeling a realistic film cooling configuration, which consists of a large stagnation-type reservoir, feeding an array of discrete cooling holes (film holes) flowing into a flat plate turbulent boundary layer. Special computational methodology is developed for this problem, involving coupled simulations using multiple computational codes. A fully compressible LES code is used in the area above the flat plate, while a low Mach number LES code is employed in the plenum and film holes. The motivation for using different codes comes from the essential difference in the nature of the flow in these different regions.
520 $a Flowfield is analyzed inside the plenum, film hole and a crossflow region. Flow inside the plenum is stagnating, except for the region close to the exit, where it accelerates rapidly to turn into the hole. The sharp radius of turning at the trailing edge of the plenum pipe connection causes the flow to separate from the downstream wall of the film hole. After coolant injection occurs, a complex flowfield is formed consisting of coherent vortical structures responsible for bringing hot crossflow fluid in contact with the walls of either the film hole or the blade, thus reducing cooling protection.
520 $a Mean velocity and turbulent statistics are compared to experimental measurements, yielding good agreement for the mean flowfield and satisfactory agreement for the turbulence quantities. LES results are used to assess the applicability of basic assumptions of conventional eddy viscosity turbulence models used with Reynolds-averaged (RANS) approach, namely the isotropy of an eddy viscosity and thermal diffusivity. It is shown here that these assumptions do not hold for the film cooling flows.
520 $a Comparison of film cooling effectiveness with experiments shows fair agreement for the centerline and laterally-averaged effectiveness. Lateral growth of the jet as judged from the lateral distribution of effectiveness is predicted correctly.
590 $a School code: 0212.
650 4 $a Engineering, Aerospace. $3 1018395
650 4 $a Engineering, Mechanical. $3 783786
650 4 $a Physics, Fluid and Plasma. $3 1018402
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790 $a 0212
791 $a Ph.D.
792 $a 2006
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