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Slave finite elements for nonlinear analysis of engine structures, volume 1A 336 degrees of freedom slave finite element processing capability to analyze engine structures under severe thermomechanical loading is presented. Description of the theoretical development and demonstration of that element is presented in this volume.
Document ID
19920010258
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gellin, S. (Textron Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
BAT-2538-953002-VOL-1
NASA-CR-187224
NAS 1.26:187224
Report Number: BAT-2538-953002-VOL-1
Report Number: NASA-CR-187224
Report Number: NAS 1.26:187224
Accession Number
92N19500
Funding Number(s)
CONTRACT_GRANT: NAS3-23279
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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