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A Cascade Optimization Strategy for Solution of Difficult Multidisciplinary Design ProblemsA research project to comparatively evaluate 10 nonlinear optimization algorithms was recently completed. A conclusion was that no single optimizer could successfully solve all 40 problems in the test bed, even though most optimizers successfully solved at least one-third of the problems. We realized that improved search directions and step lengths, available in the 10 optimizers compared, were not likely to alleviate the convergence difficulties. For the solution of those difficult problems we have devised an alternative approach called cascade optimization strategy. The cascade strategy uses several optimizers, one followed by another in a specified sequence, to solve a problem. A pseudorandom scheme perturbs design variables between the optimizers. The cascade strategy has been tested successfully in the design of supersonic and subsonic aircraft configurations and air-breathing engines for high-speed civil transport applications. These problems could not be successfully solved by an individual optimizer. The cascade optimization strategy, however, generated feasible optimum solutions for both aircraft and engine problems. This paper presents the cascade strategy and solutions to a number of these problems.
Document ID
19960017711
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Patnaik, Surya N.
(NASA Lewis Research Center Cleveland, OH United States)
Coroneos, Rula M.
(NASA Lewis Research Center Cleveland, OH United States)
Hopkins, Dale A.
(NASA Lewis Research Center Cleveland, OH United States)
Berke, Laszlo
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-107189
AIAA-96-1628
E-10161
NAS 1.15:107189
Report Number: NASA-TM-107189
Report Number: AIAA-96-1628
Report Number: E-10161
Report Number: NAS 1.15:107189
Meeting Information
Meeting: 37th Structures, Structural Dynamics and Materials Conference
Location: Salt Lake City, UT
Country: United States
Start Date: April 15, 1996
End Date: April 17, 1996
Accession Number
96N23242
Funding Number(s)
PROJECT: RTOP 505-53-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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