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Improved multielement airfoil analysisProgram is revised of NASA/Lockheed program to numerically analyze complex viscous flow about slotted airfoils. Airfoil to be analyzed can contain as many as 10 components with negative or positive overlap. Program is written in FORTRAN IV and Assembled for batch execution on CYBER 175 only.
Document ID
19800000086
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Brune, G. W. (The Boeing Co.)
Manke, J. W. (The Boeing Co.)
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Publication Information
Publication: NASA Tech Briefs
Volume: 5
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12489
ISSN: 0145-319X
Report Number: LAR-12489
Accession Number
80B10086
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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