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HYTESS: A hypothetical turbofan engine simplified simulationA users manual for a hypothetical turbofan engine simplified simulation is presented. This digital simulation exists as FORTRAN source code. The program is self-contained and was developed to offer those interested in engine dynamics and controls research an efficient, realistic, and easily used engine simulation. The engine is modeled using a state space formulation. Matrix elements within the linear state space structure are nonlinear functions of various engine variables.
Document ID
19840008116
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Merrill, W. C. (NASA Lewis Research Center Cleveland, OH, United States)
Beattie, E. C. (United Technologies Corp. East Hartford, Conn., United States)
Laprad, R. F. (United Technologies Corp. East Hartford, Conn., United States)
Rock, S. M. (Systems Control Technologies, Inc., Palo Alto Calif., United States)
Akhter, M. M. (Systems Control Technologies, Inc., Palo Alto Calif., United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-83561
NAS 1.15:83561
E-1940
Report Number: NASA-TM-83561
Report Number: NAS 1.15:83561
Report Number: E-1940
Accession Number
84N16184
Funding Number(s)
PROJECT: RTOP 505-32-6B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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