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Adaptation of NASTRAN to an integrated system of structural design analysisEfforts to integrate NASTRAN into a complete structural analysis system for use by large airframe design projects are discussed. NASTRAN was implemented as a major finite element structural analysis program to determine the static and dynamic behavior of complete airframes, as well as structural components. This requires modifications and additions to NASTRAN, to communicate with an existing system, and to provide facilities needed to work within the integrated structural analysis. For this purpose, several special DMAP modules were developed and introduced into the CALAC version of the NASTRAN system.
Document ID
19720025235
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haggenmacher, G. W.
(Lockheed-California Co. Burbank, CA, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1972
Publication Information
Publication: NASA. Langley Res. Center NASTRAN: Users' Experiences
Subject Category
Structural Mechanics
Accession Number
72N32885
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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