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Grid sensitivity for aerodynamic optimization and flow analysisAfter reviewing relevant literature, it is apparent that one aspect of aerodynamic sensitivity analysis, namely grid sensitivity, has not been investigated extensively. The grid sensitivity algorithms in most of these studies are based on structural design models. Such models, although sufficient for preliminary or conceptional design, are not acceptable for detailed design analysis. Careless grid sensitivity evaluations, would introduce gradient errors within the sensitivity module, therefore, infecting the overall optimization process. Development of an efficient and reliable grid sensitivity module with special emphasis on aerodynamic applications appear essential. The organization of this study is as follows. The physical and geometric representations of a typical model are derived in chapter 2. The grid generation algorithm and boundary grid distribution are developed in chapter 3. Chapter 4 discusses the theoretical formulation and aerodynamic sensitivity equation. The method of solution is provided in chapter 5. The results are presented and discussed in chapter 6. Finally, some concluding remarks are provided in chapter 7.
Document ID
19930015928
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sadrehaghighi, I.
(Old Dominion Univ. Norfolk, VA, United States)
Tiwari, S. N.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-192980
NAS 1.26:192980
Report Number: NASA-CR-192980
Report Number: NAS 1.26:192980
Accession Number
93N25117
Funding Number(s)
CONTRACT_GRANT: NCC1-68
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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