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Two Programs for Supersonic Wing Design and AnalysisCOREL and W12SC3 useful in aerodynamic design and analysis of wings for supersonic speeds. COREL (Conical Relaxation) program solves nonlinear full potential equation for spanwise section of wing in crossflow plane, and option exists to correct result for nonconical geometry. W12SC3 applies lineartheory panel methods to compute solutions for wing/body configuration. Programs restricted to supersonic flows and useful for many design, analysis, and optimization applications. COREL and W12SC3 written in FORTRAN IV for batch execution.
Document ID
19860000157
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mason, W. H.
(Grumman Aerospace Corp.)
Rosen, B. S.
(Grumman Aerospace Corp.)
Grossman, B.
(Grumman Aerospace Corp.)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 2
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LAR-13239
Accession Number
86B10157
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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