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Aerodynamic design using numerical optimizationThe procedure of using numerical optimization methods coupled with computational fluid dynamic (CFD) codes for the development of an aerodynamic design is examined. Several approaches that replace wind tunnel tests, develop pressure distributions and derive designs, or fulfill preset design criteria are presented. The method of Aerodynamic Design by Numerical Optimization (ADNO) is described and illustrated with examples.
Document ID
19840018593
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Murman, E. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Chapman, G. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1983
Publication Information
Publisher: MIT
Subject Category
Aerodynamics
Report/Patent Number
CFDL-TR-83-2
NASA-TM-85550
NAS 1.15:85550
Report Number: CFDL-TR-83-2
Report Number: NASA-TM-85550
Report Number: NAS 1.15:85550
Accession Number
84N26661
Funding Number(s)
CONTRACT_GRANT: NAG2-115
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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