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Experimental validation of structural optimization methodsThe topic of validating structural optimization methods by use of experimental results is addressed. The need for validating the methods as a way of effecting a greater and an accelerated acceptance of formal optimization methods by practicing engineering designers is described. The range of validation strategies is defined which includes comparison of optimization results with more traditional design approaches, establishing the accuracy of analyses used, and finally experimental validation of the optimization results. Examples of the use of experimental results to validate optimization techniques are described. The examples include experimental validation of the following: optimum design of a trussed beam; combined control-structure design of a cable-supported beam simulating an actively controlled space structure; minimum weight design of a beam with frequency constraints; minimization of the vibration response of helicopter rotor blade; minimum weight design of a turbine blade disk; aeroelastic optimization of an aircraft vertical fin; airfoil shape optimization for drag minimization; optimization of the shape of a hole in a plate for stress minimization; optimization to minimize beam dynamic response; and structural optimization of a low vibration helicopter rotor.
Document ID
19920010016
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Adelman, Howard M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:104203
NASA-TM-104203
Accession Number
92N19258
Funding Number(s)
PROJECT: RTOP 505-63-36-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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