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A verification procedure for MSC/NASTRAN Finite Element ModelsFinite Element Models (FEM's) are used in the design and analysis of aircraft to mathematically describe the airframe structure for such diverse tasks as flutter analysis and actively controlled landing gear design. FEM's are used to model the entire airplane as well as airframe components. The purpose of this document is to describe recommended methods for verifying the quality of the FEM's and to specify a step-by-step procedure for implementing the methods.
Document ID
19950020950
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stockwell, Alan E.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1995
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:4675
NASA-CR-4675
Report Number: NAS 1.26:4675
Report Number: NASA-CR-4675
Accession Number
95N27371
Funding Number(s)
CONTRACT_GRANT: NAS1-19000
PROJECT: RTOP 233-01-01-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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