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The structure of separated flow regions occurring near the leading edge of airfoils, including transitionThe structure and behavior of the separation bubble including transition and the redeveloping boundary layer after reattachment over an airfoil at low Reynolds numbers was studied. The intent is to further the understanding of the complex flow phenomena so that analytic methods for predicting their formation and development can be improved. These analytic techniques have applications in the design and performance prediction of airfoils operating in the low Reynolds number flight regime.
Document ID
19850015392
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mueller, T. J.
(Notre Dame Univ. IN, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:175670
NASA-CR-175670
Report Number: NAS 1.26:175670
Report Number: NASA-CR-175670
Accession Number
85N23703
Funding Number(s)
CONTRACT_GRANT: NSG-1419
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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