NASA Technical Reports Server (NTRS) 19920007153: Differential Continuum Damage Mechanics Models For Creep And Fatigue Of Unidirectional Metal Matrix Composites - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 19920007153: Differential Continuum Damage Mechanics Models For Creep And Fatigue Of Unidirectional Metal Matrix Composites" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 19920007153: Differential Continuum Damage Mechanics Models For Creep And Fatigue Of Unidirectional Metal Matrix Composites” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 19920007153: Differential Continuum Damage Mechanics Models For Creep And Fatigue Of Unidirectional Metal Matrix Composites
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
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- Internet Archive ID: NASA_NTRS_Archive_19920007153
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"NASA Technical Reports Server (NTRS) 19920007153: Differential Continuum Damage Mechanics Models For Creep And Fatigue Of Unidirectional Metal Matrix Composites" Description:
The Internet Archive:
Three multiaxial isothermal continuum damage mechanics models for creep, fatigue, and creep/fatigue interaction of a unidirectional metal matrix composite volume element are presented, only one of which will be discussed in depth. Each model is phenomenological and stress based, with varying degrees of complexity to accurately predict the initiation and propagation of intergranular and transgranular defects over a wide range of loading conditions. The development of these models is founded on the definition of an initially transversely isotropic fatigue limit surface, static fracture surface, normalized stress amplitude function and isochronous creep damage failure surface, from which both fatigue and creep damage evolutionary laws can be obtained. The anisotropy of each model is defined through physically meaningful invariants reflecting the local stress and material orientation. All three transversely isotropic models have been shown, when taken to their isotropic limit, to directly simplify to previously developed and validated creep and fatigue continuum damage theories. Results of a nondimensional parametric study illustrate (1) the flexibility of the present formulation when attempting to characterize a large class of composite materials, and (2) its ability to predict anticipated qualitative trends in the fatigue behavior of unidirectional metal matrix composites. Additionally, the potential for the inclusion of various micromechanical effects (e.g., fiber/matrix bond strength, fiber volume fraction, etc.), into the phenomenological anisotropic parameters is noted, as well as a detailed discussion regarding the necessary exploratory and characterization experiments needed to utilize the featured damage theories.
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