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A streamline curvature method for design of supercritical and subcritical airfoilsAn airfoil design procedure, applicable to both subcritical and supercritical airfoils, is described. The method is based on the streamline curvature velocity equation. Several examples illustrating this method are presented and discussed.
Document ID
19740024303
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Barger, R. L. (NASA Langley Research Center Hampton, VA, United States)
Brooks, C. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
L-9747
NASA-TN-D-7770
Accession Number
74N32416
Funding Number(s)
PROJECT: RTOP 501-06-05-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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