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Optimality of a Fully Stressed DesignFor a truss a fully stressed state is reached and when all its members are utilized to their full strength capacity. Historically, engineers considered such a design optimum. But recently this optimality has been questioned, especially since the weight of the structure is not explicitly used in fully stressed design calculations. This paper examines optimality of the full stressed design (FSD) with analytical and graphical illustrations. Solutions for a set of examples obtained by using the FSD method and optimization methods numerically confirm the optimality of the FSD. The FSD, which can be obtained with a small amount of calculation, can be extended to displacement constraints and to nontruss-type structures.
Document ID
19980148007
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Patnaik, Surya N.
(Ohio Aerospace Inst. Cleveland, OH United States)
Hopkins, Dale A.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1998
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-1998-207411
NAS 1.15:207411
E-10284-1
Report Number: NASA/TM-1998-207411
Report Number: NAS 1.15:207411
Report Number: E-10284-1
Funding Number(s)
PROJECT: RTOP 505-53-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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