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A computer program for the design and analysis of low-speed airfoilsA conformal mapping method for the design of airfoils with prescribed velocity distribution characteristics, a panel method for the analysis of the potential flow about given airfoils, and a boundary layer method have been combined. With this combined method, airfoils with prescribed boundary layer characteristics can be designed and airfoils with prescribed shapes can be analyzed. All three methods are described briefly. The program and its input options are described. A complete listing is given as an appendix.
Document ID
19800020753
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Eppler, R.
(Stuttgart Univ. Hampton, VA, United States)
Somers, D. M.
(NASA Langley Research Center)
Date Acquired
September 4, 2013
Publication Date
August 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-80210
L-12937
Accession Number
80N29254
Funding Number(s)
PROJECT: RTOP 505-31-33-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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