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Global function approach in structural analysis: Basic approach, numerical resultsThe structural response to a given environment is described by the differential equations of motion of deformable bodies. Analytic solutions of such problems for a reasonably large class of structural configurations are not within the realm of the possible. Consequently, the mathematical problem is recast into a numerical problem for solution on the computer. New technology in the space and energy fields led to a growing demand for accurate analysis which at times cannot be met due to the limits set by available budgets for computer time. In response to this need for more efficient numerical analysis, the possibilities of reducing the number of freedoms in the system through a revival of the global function approach were explored.
Document ID
19810023036
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Almroth, B. O.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Stehling, P.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Brogan, F. A.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-165669
Report Number: NASA-CR-165669
Accession Number
81N31579
Funding Number(s)
CONTRACT_GRANT: NAS1-10843
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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