Finite Element Applications to Explore the Effects of Partial Bonding on Metal Matrix Composite Properties

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781722236717


Pages:   26
Publication Date:   03 July 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Finite Element Applications to Explore the Effects of Partial Bonding on Metal Matrix Composite Properties


Overview

The mechanics of materials approach (definition of E, G, Nu, and Alpha) and the finite element method are used to explore the effects of partial bonding and fiber fracture on the behavior of high temperature metal matrix composites. Composite ply properties are calculated for various degrees of disbonding to evaluate the sensitivity of these properties to the presence of fiber/matrix disbonding and fiber fracture. The mechanics of materials approach allows for the determination of the basic ply material properties needed for design/analysis of composites. The finite element method provides the necessary structural response (forces and displacements) for the mechanics of materials equations. Results show that disbonding of fractured fibers affect only E sub (111) and alpha sub (111) significantly. Caruso, J. J. and Trowbridge, D. and Chamis, C. C. Glenn Research Center RTOP 505-63-11...

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Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.10cm , Length: 27.90cm
Weight:   0.086kg
ISBN:  

9781722236717


ISBN 10:   172223671
Pages:   26
Publication Date:   03 July 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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