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TRANSEP: A program for high lift separated flow about airfoilsA method and program called TRANSEP is presented that can be used for the analysis of the flow about a low speed airfoil under high lift, massive separation conditions. Since the present program is a modification of the direct-inverse TRANDES code, it can also be used for the design and analysis of transonic airfoils, including the effects of weak viscous interaction. Interactions on program usage, program modifications to convert TRANDES to TRANSEP, and sample cases and results are given.
Document ID
19840025315
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carlson, L. A. (Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3376
NAS 1.26:3376
Accession Number
84N33386
Funding Number(s)
PROJECT: RTOP 505-31-33
CONTRACT_GRANT: NSG-1174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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