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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 /
Record Type:
Language materials, printed : Monograph/item
Title/Author:
Loadings in thermal barrier coatings of jet engine turbine blades/ by Tomasz Sadowski, Przemyslaw Golewski.
Reminder of title:
an experimental research and numerical modeling /
Author:
Sadowski, Tomasz.
other author:
Golewski, Przemyslaw.
Published:
Singapore :Springer Singapore : : 2016.,
Description:
viii, 107 p. :ill. (some col.), digital ; : 24 cm.;
Contained By:
Springer eBooks
Subject:
Thermal barrier coatings. -
Online resource:
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 blades
an 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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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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Blades
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Continuum Mechanics and Mechanics of Materials.
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Characterization and Evaluation of Materials.
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Engineering (Springer-11647)
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