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An Automated DAKOTA and VULCAN-CFD Framework with Application to Supersonic Facility Nozzle Flowpath OptimizationRemoving human interaction from design processes by using automation may lead to gains in both productivity and design precision. This memorandum describes efforts to incorporate high fidelity numerical analysis tools into an automated framework and applying that framework to applications of practical interest. The purpose of this effort was to integrate VULCAN-CFD into an automated, DAKOTA-enabled framework with a proof-of-concept application being the optimization of supersonic test facility nozzles. It was shown that the optimization framework could be deployed on a high performance computing cluster with the flow of information handled effectively to guide the optimization process. Furthermore, the application of the framework to supersonic test facility nozzle flowpath design and optimization was demonstrated using multiple optimization algorithms.
Document ID
20150017613
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Axdahl, Erik L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 10, 2015
Publication Date
August 1, 2015
Subject Category
Systems Analysis And Operations Research
Report/Patent Number
NF1676L-21745
NASA/TM-2015-218796
L-20571
Report Number: NF1676L-21745
Report Number: NASA/TM-2015-218796
Report Number: L-20571
Funding Number(s)
WBS: WBS 110076.02.07.05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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