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Transonic flow past swept wingsFLO-22 computer program aids in numerical analysis of transonic potential flow past lifting, swept wing. FLO-22 uses relaxation method to solve finite-difference approximation of full-potential equation for transonic flow past configuration consisting of wing or arbitrary planform and dihedral extending from symmetry plane or wall. Comparisons of FLO-22 calculated results with experimental data for both conventional and super-critical transport wings show good agreement.
Document ID
19790000542
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Caughey, D. A. (Cornell Univ.)
Jameson, A. (New York Univ.)
Date Acquired
August 10, 2013
Publication Date
June 1, 1980
Publication Information
Publication: NASA Tech Briefs
Volume: 4
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12446
Report Number: LAR-12446
ISSN: 0145-319X
Accession Number
79B10542
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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