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Comparison of Traditional Design Nonlinear Programming Optimization and Stochastic Methods for Structural DesignStructural design generated by traditional method, optimization method and the stochastic design concept are compared. In the traditional method, the constraints are manipulated to obtain the design and weight is back calculated. In design optimization, the weight of a structure becomes the merit function with constraints imposed on failure modes and an optimization algorithm is used to generate the solution. Stochastic design concept accounts for uncertainties in loads, material properties, and other parameters and solution is obtained by solving a design optimization problem for a specified reliability. Acceptable solutions were produced by all the three methods. The variation in the weight calculated by the methods was modest. Some variation was noticed in designs calculated by the methods. The variation may be attributed to structural indeterminacy. It is prudent to develop design by all three methods prior to its fabrication. The traditional design method can be improved when the simplified sensitivities of the behavior constraint is used. Such sensitivity can reduce design calculations and may have a potential to unify the traditional and optimization methods. Weight versus reliabilitytraced out an inverted-S-shaped graph. The center of the graph corresponded to mean valued design. A heavy design with weight approaching infinity could be produced for a near-zero rate of failure. Weight can be reduced to a small value for a most failure-prone design. Probabilistic modeling of load and material properties remained a challenge.
Document ID
20110011998
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Patnaik, Surya N.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Pai, Shantaram S.
(NASA Glenn Research Center Cleveland, OH, United States)
Coroneos, Rula M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
September 13, 2010
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
E-17647
Report Number: E-17647
Meeting Information
Meeting: 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference Fort Worth, Texas
Location: Fort Worth, TX
Country: United States
Start Date: September 13, 2010
End Date: September 15, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, International Society for Structural and Multidisciplinary Optimization
Funding Number(s)
WBS: WBS 561581.02.08.03.13.05
Distribution Limits
Public
Copyright
Public Use Permitted.
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