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Generalized dynamic engine simulation techniques for the digital computerRecently advanced simulation techniques have been developed for the digital computer and used as the basis for development of a generalized dynamic engine simulation computer program, called DYNGEN. This computer program can analyze the steady state and dynamic performance of many kinds of aircraft gas turbine engines. Without changes to the basic program DYNGEN can analyze one- or two-spool turbofan engines. The user must supply appropriate component performance maps and design-point information. Examples are presented to illustrate the capabilities of DYNGEN in the steady state and dynamic modes of operation. The analytical techniques used in DYNGEN are briefly discussed, and its accuracy is compared with a comparable simulation using the hybrid computer. The impact of DYNGEN and similar all-digital programs on future engine simulation philosophy is also discussed.
Document ID
19740019181
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sellers, J.
(NASA Lewis Research Center Cleveland, OH, United States)
Teren, F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-71552
E-7968
Report Number: NASA-TM-X-71552
Report Number: E-7968
Meeting Information
Meeting: Propulsion and Energetics Meeting
Location: Ankara
Start Date: September 9, 1974
End Date: September 13, 1974
Sponsors: AGARD
Accession Number
74N27294
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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