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PANEL Code for Planar CascadesPlane cascade flow solved using improved surface-singularity methods. Current external aerodynamic integral-equation techniques adapted for use in internal flow calculation. Inherent computational speed and flexibility of integral equation solutions make them useful for design calculations.
Document ID
19830000190
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Mcfarland, E. R.
Date Acquired
August 11, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13862
Report Number: LEW-13862
ISSN: 0145-319X
Accession Number
83B10190
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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