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An automated procedure for developing hybrid computer simulations of turbofan enginesThis paper offers a systematic, computer-aided, self-documenting methodology for developing hybrid computer simulations of turbofan engines. The methodology that is presented makes use of a host program that can run on a large digital computer and a machine-dependent target (hybrid) program. The host program performs all of the calculations and data manipulations that are needed to transform user-supplied engine design information to a form suitable for the hybrid computer. The host program also trims the self-contained engine model to match specified design point information. A test case is described and comparisons between hybrid simulation and specified engine performance data are presented.
Document ID
19810048140
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Szuch, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Krosel, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Bruton, W. M.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1981
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Annual Simulation Symposium
Location: Tampa, FL
Country: US
Start Date: March 18, 1981
End Date: March 20, 1981
Sponsors: IMACS, IEEE, ACM, SCS
Accession Number
81A32544
Distribution Limits
Public
Copyright
Other

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