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HYTESS-Hypothetical Turbofan-Engine Simplified SimulationSimulated characteristics mimic those of advanced turbofan engines. Computer program developed to offer those interested in engine dynamics and controls research efficient, realistic, and easily-used engine simulation. Simulation developed from linearized operating-point models but still retains essential nonlinear engine effects. Representative of hypothetical, low-bypass-ratio, twin-spool, axialflow turbofan engine. Program written in FORTRAN IV.
Document ID
19860000242
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Merrill, W. (Pratt & Whitney Aircraft Co.)
Beattie, C. (Pratt & Whitney Aircraft Co.)
Laprad, R. (Systems Control Technology, Inc.)
Rock, S. (Systems Control Technologies, Inc.)
Akhter, M.
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LEW-14020
Report Number: LEW-14020
ISSN: 0145-319X
Accession Number
86B10242
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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