Temperature Dependent Nonlinear Metal Matrix Laminate Behavior

Temperature Dependent Nonlinear Metal Matrix Laminate Behavior PDF Author: David J. Barrett
Publisher:
ISBN:
Category : Metals
Languages : en
Pages : 128

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Temperature Dependent Nonlinear Metal Matrix Laminate Behavior

Temperature Dependent Nonlinear Metal Matrix Laminate Behavior PDF Author: David J. Barrett
Publisher:
ISBN:
Category : Metals
Languages : en
Pages : 128

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Book Description


Temperature Dependent Nonlinear Metal Matrix Laminae Behavior

Temperature Dependent Nonlinear Metal Matrix Laminae Behavior PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 128

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An analytical method is described for computing the nonlinear thermal and mechanical response of laminated plates. The material model focuses upon the behavior of metal matrix materials by relating the nonlinear composite response to plasticity effects in the matrix. The foundation of the analysis is the unidirectional material model which is used to compute the instantaneous properties of the lamina based upon the properties of the fibers and matrix. The unidirectional model assumes that the fibers properties are constant with temperature and assumes that the matrix can be modelled as a temperature dependent, bilinear, kinematically hardening material. An incremental approach is used to compute average stresses in the fibers and matrix caused by arbitrary mechanical and thermal loads. The layer model is incorporated in an incremental laminated plate theory to compute the nonlinear response of laminated metal matrix composites of general orientation and stacking sequence. The report includes comparisons of the method with other analytical approaches and compares theoretical calculations with measured experimental material behavior. A section is included which describes the limitations of the material model.

Thermomechanical fatigue behavior of materials

Thermomechanical fatigue behavior of materials PDF Author: Michael J. Verrilli
Publisher: ASTM International
ISBN: 080312001X
Category :
Languages : en
Pages : 382

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500

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Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986

Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1986 PDF Author: Langley Research Center. Research Information and Applications Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 270

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1282

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Response of Metal Matrix Laminates with Temperature-Dependent Properties

Response of Metal Matrix Laminates with Temperature-Dependent Properties PDF Author: F. Mirzadeh
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 9

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An analytical, inelastic micromechanical model, with temperature-dependent matrix properties, is employed to study metal matrix composite (MMC) laminates subjected to thermomechanical loading. The predictions are based on knowledge of the thermomechanical response of transversely isotropic, elastic graphite or silicon carbide fibers and elastic-viscoplastic, work-hardening, temperature-dependent titanium or aluminum matrix. The model is applied to predict initial yielding and thermomechanical response of silicon carbide/titanium and graphite/aluminum laminates. The results demonstrate the effect of cooling from a stress-free temperature and the mismatch of thermal and mechanical properties of the constituent phases on the laminate's subsequent mechanical response. Typical results are presented for [±45], laminates subjected to monotonic tension, cyclic tension/compression, biaxial tension, and thermal loadings. It is shown that inclusion of temperature-dependent properties has a significant influence on both the initial yield surface and the inelastic response of metal matrix composites. It is also shown that the degree of applied biaxial loading has a significant effect on the response of laminates.

Energy Research Abstracts

Energy Research Abstracts PDF Author:
Publisher:
ISBN:
Category : Power resources
Languages : en
Pages : 648

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Engine Structures

Engine Structures PDF Author:
Publisher:
ISBN:
Category : Engines
Languages : en
Pages : 232

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1638

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