NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Using Plate Finite Elements for Modeling Fillets in Design, Optimization, and Dynamic AnalysisA methodology has been developed that allows the use of plate elements instead of numerically inefficient solid elements for modeling structures with 90 degree fillets. The technique uses plate bridges with pseudo Young's modulus (Eb) and thickness (tb) values placed between the tangent points of the fillets. These parameters are obtained by solving two nonlinear simultaneous equations in terms of the independent variables rlt and twallt. These equations are generated by equating the rotation at the tangent point of a bridge system with that of a fillet, where both rotations are derived using beam theory. Accurate surface fits of the solutions are also presented to provide the user with closed-form equations for the parameters. The methodology was verified on the subcomponent level and with a representative filleted structure, where the technique yielded a plate model exhibiting a level of accuracy better than or equal to a high-fidelity solid model and with a 90-percent reduction in the number of DOFs. The application of this method for parametric design studies, optimization, and dynamic analysis should prove extremely beneficial for the finite element practitioner. Although the method does not attempt to produce accurate stresses in the filleted region, it can also be used to obtain stresses elsewhere in the structure for preliminary analysis. A future avenue of study is to extend the theory developed here to other fillet geometries, including fillet angles other than 90 and multifaceted intersections.
Document ID
20030033869
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Brown, A. M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Seugling, R. M.
(North Carolina Univ. Charlotte, NC, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2003
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TP-2003-212340
M-1068
NAS 1.60:212340
Report Number: NASA/TP-2003-212340
Report Number: M-1068
Report Number: NAS 1.60:212340
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available