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High-Lift Separated Flow About AirfoilsTRANSEP Calculates flow field about low-speed single-element airfoil at high-angle-of-attack and high-lift conditions with massive boundary-layer separation. TRANSEP includes effects of weak viscous interactions and can be used for subsonic/transonic airfoil design and analysis. The approach used in TRANSEP is based on direct-inverse method and its ability to use either displacement surface or pressure as airfoil boundary condition.
Document ID
19810000324
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carlson, L. A.
(Texas A & M University)
Date Acquired
August 11, 2013
Publication Date
December 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 3
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12853
Accession Number
81B10324
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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