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Transonic Airfoil AnalysisProgram uses fast iteration scheme for solving transonic flow field around arbitrary airfoils. Transonic Airfoil Analysis Computer Code, TAIR, employs fast, fully implicit algorithm to solve conservative full-potiential equation for steady transonic flow field about arbitrary airfoil immersed in subsonic free stream. TAIR written in FORTRAN IV.
Document ID
19830000395
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Holst, T. L. (Informatics, Inc.)
Dougherty, F. C. (Informatics, Inc.)
Gundy, K. L. (Informatics, Inc.)
Thomas, S. D. (Informatics, Inc.)
Frick, J. (University of Santa Clara)
Fernquist, A.
Albert, J.
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11436
ISSN: 0145-319X
Report Number: ARC-11436
Accession Number
83B10395
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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