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Loadings in Thermal Barrier Coatings...
~
Sadowski, Tomasz.
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, Przemysław Golewski.
Reminder of title:
An Experimental Research and Numerical Modeling /
Author:
Sadowski, Tomasz.
other author:
Golewski, Przemysław.
Description:
VIII, 107 p. 30 illus., 20 illus. in color.online resource. :
Contained By:
Springer Nature eBook
Subject:
Mechanics. -
Online resource:
https://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, Przemysław Golewski. - 1st ed. 2016. - VIII, 107 p. 30 illus., 20 illus. in color.online resource. - SpringerBriefs in Computational Mechanics,2191-5342. - SpringerBriefs in Computational Mechanics,.
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:
527684
Mechanics.
LC Class. No.: TA349-359
Dewey Class. No.: 531
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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