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A computer program for calculating design and off-design performance of two- and three-spool turbofans with as many as three nozzlesProgram uses component performance maps to enable user to do analytical engine cycle calculations. Either convergent or convergent-divergent nozzles may be used.
Document ID
19730000245
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Fishbach, L. H.
Koenig, R. W.
Date Acquired
August 7, 2013
Publication Date
November 1, 1973
Subject Category
Mathematics And Information Sciences
Report/Patent Number
LEW-12011
Report Number: LEW-12011
Accession Number
73B10245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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