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Code For Analysis Of Wing-And-Flap SystemsSUBAERF2 program developed to provide for analysis of subsonic aerodynamics and design by iteration of low-speed wing/flap systems. Based on linearized-theory lifting-surface solution but also accounts for some nonlinear characteristics. Effects of leading- and trailing-edge flaps included. New and improved version of programs described in LAR-13116 and LAR-12987, and replaces both of them. Written in FORTRAN V.
Document ID
19900000536
Document Type
Other - NASA Tech Brief
Authors
Darden, Christine M. (NASA Langley Research Center, Hampton, VA.)
Carlson, Harry W. (Planning Research Corp.)
Date Acquired
August 14, 2013
Publication Date
October 1, 1990
Publication Information
Publication: NASA Tech Briefs
Volume: 14
Issue: 10
ISSN: 0145-319X
Subject Category
MECHANICS
Report/Patent Number
LAR-13994
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.