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A microprocessor-based real-time simulator of a turbofan engineA real-time digital simulator of a Pratt and Whitney F 100 engine is discussed. This self-contained unit can operate in an open-loop stand-alone mode or as part of a closed-loop control system. It can also be used in control system design and development. It accepts five analog control inputs and its sixteen outputs are returned as analog signals.
Document ID
19880011779
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Litt, Jonathan S. (Army Aviation Research and Development Command Cleveland, Ohio., United States)
Delaat, John C. (NASA Lewis Research Center Cleveland, OH, United States)
Merrill, Walter C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AVSCOM-TR-88-C-011
NAS 1.15:100889
E-4124
NASA-TM-100889
AD-A202975
Report Number: AVSCOM-TR-88-C-011
Report Number: NAS 1.15:100889
Report Number: E-4124
Report Number: NASA-TM-100889
Report Number: AD-A202975
Accession Number
88N21163
Funding Number(s)
PROJECT: RTOP 505-62-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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