NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Finite-Element Modeling For Structural AnalysisReport presents study of finite-element mathematical modeling as used in analyzing stresses and strains at joints between thin, shell-like components (e.g., ducts) and thicker components (e.g., flanges or engine blocks). First approach uses global/local model to evaluate system. Provides correct total response and correct representation of stresses away from any discontinuities. Second approach involves development of special transition finite elements to model transitions between shells and thicker structural components.
Document ID
19950065571
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Min, J. B.
(NASA Marshall Space Flight Center, Huntsville, AL.)
Androlake, S. G.
(NASA Marshall Space Flight Center, Huntsville, AL.)
Date Acquired
August 17, 2013
Publication Date
August 1, 1995
Publication Information
Publication: NASA Tech Briefs
Volume: 19
Issue: 8
ISSN: 0145-319X
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MFS-28971
Accession Number
95B10412
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available