An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization /

Bibliographic Details
Main Author: Axdahl, Erik L. (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
Series:NASA technical memorandum ; 2015-218796.
Subjects:
Online Access:https://purl.fdlp.gov/GPO/gpo62868
http://purl.fdlp.gov/GPO/gpo62868

MARC

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245 1 3 |a An automated DAKOTA and VULCAN-CFD framework with application to supersonic facility nozzle flowpath optimization /  |c Erik L. Axdahl. 
246 3 |a Automated design analysis kit for optimization and terascale applications and viscous upwind algorithm for complex flow analysis computational fluid dynamics framework with application to supersonic facility nozzle flowpath optimization 
264 1 |a Hampton, Virginia :  |b National Aeronautics and Space Administration, Langley Research Center,  |c August 2015. 
300 |a 1 online resource (31 pages) :  |b color illustrations. 
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500 |a Title from title screen (viewed on Nov. 19, 2015). 
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504 |a Includes bibliographical references (pages 14-15). 
513 |a Technical memorandum;  |b 10/2013-9/2014. 
536 |a Sponsored by the National Aeronautics and Space Administration  |h 110076.02.07.05 
536 |d L-20571 
650 7 |a Computational fluid dynamics.  |2 nasat 
650 7 |a Design optimization.  |2 nasat 
650 7 |a Supersonic nozzles.  |2 nasat 
650 7 |a Numerical analysis.  |2 nasat 
650 7 |a Test facilities.  |2 nasat 
710 2 |a Langley Research Center,  |e issuing body. 
710 1 |a United States.  |b National Aeronautics and Space Administration,  |e sponsoring body. 
830 0 |a NASA technical memorandum ;  |v 2015-218796. 
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