NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
A numerical method for interface problems in elastodynamicsThe numerical implementation of a formulation for a class of interface problems in elastodynamics is discussed. This formulation combines the use of the finite element and boundary integral methods to represent the interior and the exteriro regions, respectively. In particular, the response of a semicylindrical alluvial valley in a homogeneous halfspace to incident antiplane SH waves is considered to determine the accuracy and convergence of the numerical procedure. Numerical results are obtained from several combinations of the incidence angle, frequency of excitation, and relative stiffness between the inclusion and the surrounding halfspace. The results tend to confirm the theoretical estimates that the convergence is of the order H(2) for the piecewise linear elements used. It was also observed that the accuracy descreases as the frequency of excitation increases or as the relative stiffness of the inclusion decreases.
Document ID
19850009082
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mcghee, D. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1984
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-86488
NAS 1.15:86488
Report Number: NASA-TM-86488
Report Number: NAS 1.15:86488
Accession Number
85N17391
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available