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Development of dynamic simulation of TF34-GE-100 turbofan engine with post-stall capabilityThis paper describes the development of a hybrid computer simulation of a TF34-GE-100 turbofan engine with post-stall capability. The simulation operates in real-time and will be used to test and evaluate stall recovery control modes for this engine. The simulation calculations are performed by an analog computer with a peripheral multivariable function generation unit used for computing bivariate functions. Tabular listings of a simulation variables are obtained by interfacing to a digital computer and using a custom software package for data collection and display.
Document ID
19840017644
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Krosel, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-2104
NASA-TM-83660
AIAA PAPER 84-1184
NAS 1.15:83660
Report Number: E-2104
Report Number: NASA-TM-83660
Report Number: AIAA PAPER 84-1184
Report Number: NAS 1.15:83660
Meeting Information
Meeting: Joint Propulsion Conf.
Location: Cincinnati, OH
Country: United States
Start Date: June 11, 1984
End Date: June 13, 1984
Accession Number
84N25712
Funding Number(s)
PROJECT: RTOP 505-40-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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