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Calculating Aerodynamic-Stability DerivativesVORSTAB program developed to calculate lateral-directional characteristics of nonplanar wing/body combinations in subsonic flow. Mathematically determines effects of edge-separated vortex flow, including augmented vortex lift, strake-induced downwash, and vortex breakdown. VORSTAB written in FORTRAN IV.
Document ID
19860000337
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Lan, C. E. (University of Kansas Center for Research, Inc.)
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13471
ISSN: 0145-319X
Report Number: LAR-13471
Accession Number
86B10337
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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