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FORTRAN program for calculating velocities in the meridional plane of a turbomachine 1: Centrifugal compressorThe program will determine the velocities in the meridional plane of a backward-swept impeller, a radial impeller, and a vaned diffuser. The velocity gradient equation with the assumption of a hub-to-shroud mean stream surface is solved along arbitrary quasi-orthogonals in the meridional plane. These quasi-orthogonals are fixed straight lines.
Document ID
19720010338
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Vanco, M. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
E-6592
NASA-TN-D-6701
Accession Number
72N17988
Funding Number(s)
PROJECT: RTOP 132-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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