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Loadings in thermal barrier coatings...

Golewski, Przemyslaw.

Loadings in thermal barrier coatings of jet engine turbine blades = an experimental research and numerical modeling /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Loadings in thermal barrier coatings of jet engine turbine blades/ by Tomasz Sadowski, Przemyslaw Golewski.
其他題名:	an experimental research and numerical modeling /
作者:	Sadowski, Tomasz.
其他作者:	Golewski, Przemyslaw.
出版者:	Singapore :Springer Singapore : : 2016.,
面頁冊數:	viii, 107 p. :ill. (some col.), digital ; : 24 cm.;
Contained By:	Springer eBooks
標題:	Thermal barrier coatings. -
電子資源:	http://dx.doi.org/10.1007/978-981-10-0919-8
ISBN:	9789811009198

Loadings in thermal barrier coatings of jet engine turbine blades = an experimental research and numerical modeling /
Sadowski, Tomasz.

Loadings in thermal barrier coatings of jet engine turbine bladesan experimental research and numerical modeling /[electronic resource] :by Tomasz Sadowski, Przemyslaw Golewski. - Singapore :Springer Singapore :2016. - viii, 107 p. :ill. (some col.), digital ;24 cm. - SpringerBriefs in applied sciences and technology,2191-530X. - SpringerBriefs in applied sciences and technology..

This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories.

ISBN: 9789811009198

Standard No.: 10.1007/978-981-10-0919-8doiSubjects--Topical Terms:

1029539
Thermal barrier coatings.

LC Class. No.: TA418.76

Dewey Class. No.: 667.9

Loadings in thermal barrier coatings of jet engine turbine blades = an experimental research and numerical modeling /
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490 1 $a SpringerBriefs in applied sciences and technology, $x 2191-530X
520 $a This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories.
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650 2 4 $a Mathematical Modeling and Industrial Mathematics. $3 669172
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