NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Finite Element model refinement with actual forced responses of structuresThe formulation and computer algorithm for Finite Element model refinement based on correlation with frequency response test results have been developed. The proposed approach is derived from the direct frequency response formulation of dynamic systems. The computer algorithm has been effectively implemented in MSC/NASTRAN's DMAP language. Numerical examples are given to show the effectiveness of the method. Also, numerical difficulties and their possible solutions are discussed.
Document ID
19920064600
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Ting, T.
(Bridgeport, University CT, United States)
Chen, T. L. C.
(NASA Langley Research Center Hampton, VA, United States)
Twomey, W. J.
(Sikorsky Aircraft Stratford, CT, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Publication Information
Publication: Finite Elements in Analysis and Design
Volume: 11
Issue: 3, Ju
ISSN: 0168-874X
Subject Category
Computer Programming And Software
Report/Patent Number
ISSN: 0168-874X
Accession Number
92A47224
Distribution Limits
Public
Copyright
Other

Available Downloads

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