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Shock Free Airfoil CascadesThe CAS22 computer program developed to provide for fast design and analysis of shock free airfoil cascades. CAS22 applicable to aerodynamic analysis and transonic shock free redesign of existing two-dimensional cascades of airfoils. Program is written in FORTRAN IV.
Document ID
19830000076
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dulikravich, D. S. (Universities Space Research Association)
Date Acquired
August 11, 2013
Publication Date
August 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-13842
Report Number: LEW-13842
ISSN: 0145-319X
Accession Number
83B10076
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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