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Gas turbine system simulation: An object-oriented approachA prototype gas turbine engine simulation has been developed that offers a generalized framework for the simulation of engines subject to steady-state and transient operating conditions. The prototype is in preliminary form, but it successfully demonstrates the viability of an object-oriented approach for generalized simulation applications. Although object oriented programming languages are-relative to FORTRAN-somewhat austere, it is proposed that gas turbine simulations of an interdisciplinary nature will benefit significantly in terms of code reliability, maintainability, and manageability. This report elucidates specific gas turbine simulation obstacles that an object-oriented framework can overcome and describes the opportunity for interdisciplinary simulation that the approach offers.
Document ID
19930016484
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Drummond, Colin K.
(NASA Lewis Research Center Cleveland, OH, United States)
Follen, Gregory J.
(NASA Lewis Research Center Cleveland, OH, United States)
Putt, Charles W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-106044
NAS 1.15:106044
E-7632
Report Number: NASA-TM-106044
Report Number: NAS 1.15:106044
Report Number: E-7632
Meeting Information
Meeting: Annual Pittsburgh Conference on Modeling and Simulation
Location: Pittsburgh, PA
Country: United States
Start Date: April 30, 1992
End Date: May 1, 1992
Sponsors: SCS, IEEE, ISA, Univ. of Pittsburgh
Accession Number
93N25673
Funding Number(s)
PROJECT: RTOP 505-62-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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