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DYNGENSteady-state and transient performance of turbofan and turbojet engines are analyzed. Program uses large time steps, gives analyst freedom in selecting equations needed to describe system, and eliminates discrepancies in answers often generated by transient and steady-state simulations.
Document ID
19760000108
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Sellers, J. F.
Daniele, C. J.
Date Acquired
August 8, 2013
Publication Date
March 1, 1976
Publication Information
Publication: NASA Tech Briefs
Volume: 1
Issue: 1
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LEW-12506
Report Number: LEW-12506
ISSN: 0145-319X
Accession Number
76B10108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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