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Real-time simulation of F100-PW-100 turbofan engine using the hybrid computerA real-time hybrid computer simulation of the F100-PW-100 augmented turbofan is presented. The digital portion of the hybrid computer is used to perform the bivariate function generation associated with modeling the performance of the engine's rotating components. The remaining calculations are performed on the analog computer. Steady state simulation data along with sea level, static, transient data are presented to show that the real-time simulation matches baseline digital simulation results over a wide range of power settings and flight conditions. Steady state simulation data are compared with sea level, experimental data to show that the real-time hybrid and baseline digital simulations do adequately predict the performance of the actual engine. FORTRAN listings and analog patching diagrams are provided.
Document ID
19750019996
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Szuch, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Seldner, K.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8136
NASA-TM-X-3261
Accession Number
75N28068
Funding Number(s)
PROJECT: RTOP 505-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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