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Modified Fully Utilized Design (MFUD) Method for Stress and Displacement ConstraintsThe traditional fully stressed method performs satisfactorily for stress-limited structural design. When this method is extended to include displacement limitations in addition to stress constraints, it is known as the fully utilized design (FUD). Typically, the FUD produces an overdesign, which is the primary limitation of this otherwise elegant method. We have modified FUD in an attempt to alleviate the limitation. This new method, called the modified fully utilized design (MFUD) method, has been tested successfully on a number of designs that were subjected to multiple loads and had both stress and displacement constraints. The solutions obtained with MFUD compare favorably with the optimum results that can be generated by using nonlinear mathematical programming techniques. The MFUD method appears to have alleviated the overdesign condition and offers the simplicity of a direct, fully stressed type of design method that is distinctly different from optimization and optimality criteria formulations. The MFUD method is being developed for practicing engineers who favor traditional design methods rather than methods based on advanced calculus and nonlinear mathematical programming techniques. The Integrated Force Method (IFM) was found to be the appropriate analysis tool in the development of the MFUD method. In this paper, the MFUD method and its optimality are presented along with a number of illustrative examples.
Document ID
19970028850
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Patnaik, Surya
(Ohio Aerospace Inst. Cleveland, OH United States)
Gendy, Atef
(National Academy of Sciences - National Research Council Cleveland, OH United States)
Berke, Laszlo
(NASA Lewis Research Center Cleveland, OH United States)
Hopkins, Dale
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1997
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-4743
NAS 1.15:4743
E-10267
Report Number: NASA-TM-4743
Report Number: NAS 1.15:4743
Report Number: E-10267
Accession Number
97N27573
Funding Number(s)
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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