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Swept wing aerodynamicsTechnique analyzes viscosity-dependent aerodynamic characteristics of multielement infinite swept wings in incompressible flow. Use of source distributions rather than displacement thickness to represent boundary layer effect on potential flow and of iterative technique for matrix inversion reduces computer time for overall analysis.
Document ID
19760000403
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dvorak, F. A. (Flow Res., Inc.)
Woodward, F. A. (Flow Res., Inc.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1977
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-10790
Report Number: ARC-10790
ISSN: 0145-319X
Accession Number
76B10403
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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