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The design and analysis of low-speed airfoilsPROFILE program solves diverse and inverse airfoil-flow problems. It combines conformational mapping method for design of airfoils with prescribed velocity-distribution characteristics, panel method for potential-flow analysis, and boundary-layer method. PROFILE is written in FORTRAN IV for implementation on CDC 6000-series computer.
Document ID
19800000524
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Eppler, R.
(University of Stuttgart)
Somers, D. M.
Date Acquired
August 10, 2013
Publication Date
April 1, 1981
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12727
Accession Number
80B10524
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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