國立虎尾科技大學 |

Jet Impingement Heat Transfer Over Rotating Surfaces.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Jet Impingement Heat Transfer Over Rotating Surfaces./
作者:	Bhansali, Pratik Santosh.
面頁冊數:	1 online resource (130 pages)
附註:	Source: Dissertations Abstracts International, Volume: 84-11, Section: B.
Contained By:	Dissertations Abstracts International84-11B.
標題:	Heat transfer. -
電子資源:	click for full text (PQDT)
ISBN:	9798379471606

Jet Impingement Heat Transfer Over Rotating Surfaces.
Bhansali, Pratik Santosh.

Jet Impingement Heat Transfer Over Rotating Surfaces. - 1 online resource (130 pages)

Source: Dissertations Abstracts International, Volume: 84-11, Section: B.

Thesis (Ph.D.)--North Carolina State University, 2023.

Includes bibliographical references

The environmental impact and the operational economy of systems such as the gas turbine engines is a major and a growing concern across the globe. As the demand for the systems like aircrafts employing the gas turbine increases, and advances are made in enhancement of the capabilities of such systems, it becomes increasingly important to push towards better efficiencies while catering these needs. Higher operating temperatures are essential in obtaining better efficiencies and also to meet the higher power demands. This however, exposes the components to harsh environments. The material limitations of such components however, prove to be a hurdle in achieving this objective. Therefore, the components need to be cooled efficiently to protect them for safe operation of the engine. In a gas turbine engine, between 20-30% of the core inlet air is bled off after compression, which imposes a performance penalty on the engine. It is therefore necessary to use this air economically and improve the performance of the cooling arrangements utilizing this cooling air.A gas turbine consists of rotating components like the gas turbine disk which support the blades mounted on it circumferentially and transfer power to the drive shaft. This disk is also subjected to ingress of hot turbine gases. Jet impingement is and effective way to cool these disks and also counter the ingress problem. In addition to gas turbine engines, rotating surfaces are encountered in many other systems like rotary heat exchangers, automobile components, etc., where better thermal efficiencies and thermal management play a key role from safety as well as economic perspective. Since rotating surfaces encounter flow structures different that stationary surfaces, it is essential to conduct investigations under rotating conditions.The present study aims at improving the heat transfer performance of rotating disks under jet impingement by introducing extended surfaces like pins and ribs on the surfaces. The primary objective of this work is to investigate the impact of various factors such as the rotational speed, dimensions and shape of the features, characteristics of the impinging jet, impingement location and angles of impingement. This investigation also aims at creating a pool of data to serve as the foundation for further investigation by the community. Experimental and computational studies have been conducted to present a detailed analysis of the heat transfer characteristics and understand some fundamental differences between heat transfer involving stationary and rotating surfaces.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9798379471606Subjects--Topical Terms:

1085480
Heat transfer.
Index Terms--Genre/Form:

554714
Electronic books.

Jet Impingement Heat Transfer Over Rotating Surfaces.
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500 $a Source: Dissertations Abstracts International, Volume: 84-11, Section: B.
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502 $a Thesis (Ph.D.)--North Carolina State University, 2023.
504 $a Includes bibliographical references
520 $a The environmental impact and the operational economy of systems such as the gas turbine engines is a major and a growing concern across the globe. As the demand for the systems like aircrafts employing the gas turbine increases, and advances are made in enhancement of the capabilities of such systems, it becomes increasingly important to push towards better efficiencies while catering these needs. Higher operating temperatures are essential in obtaining better efficiencies and also to meet the higher power demands. This however, exposes the components to harsh environments. The material limitations of such components however, prove to be a hurdle in achieving this objective. Therefore, the components need to be cooled efficiently to protect them for safe operation of the engine. In a gas turbine engine, between 20-30% of the core inlet air is bled off after compression, which imposes a performance penalty on the engine. It is therefore necessary to use this air economically and improve the performance of the cooling arrangements utilizing this cooling air.A gas turbine consists of rotating components like the gas turbine disk which support the blades mounted on it circumferentially and transfer power to the drive shaft. This disk is also subjected to ingress of hot turbine gases. Jet impingement is and effective way to cool these disks and also counter the ingress problem. In addition to gas turbine engines, rotating surfaces are encountered in many other systems like rotary heat exchangers, automobile components, etc., where better thermal efficiencies and thermal management play a key role from safety as well as economic perspective. Since rotating surfaces encounter flow structures different that stationary surfaces, it is essential to conduct investigations under rotating conditions.The present study aims at improving the heat transfer performance of rotating disks under jet impingement by introducing extended surfaces like pins and ribs on the surfaces. The primary objective of this work is to investigate the impact of various factors such as the rotational speed, dimensions and shape of the features, characteristics of the impinging jet, impingement location and angles of impingement. This investigation also aims at creating a pool of data to serve as the foundation for further investigation by the community. Experimental and computational studies have been conducted to present a detailed analysis of the heat transfer characteristics and understand some fundamental differences between heat transfer involving stationary and rotating surfaces.
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650 4 $a Reynolds number. $3 839681
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650 4 $a Compressed air. $3 1437768
650 4 $a Chemical vapor deposition. $3 903407
650 4 $a Fluid mechanics. $3 555551
650 4 $a Materials science. $3 557839
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650 4 $a Thermodynamics. $3 596513
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