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Computer simulation of engine systemsThe paper discusses the availability throughout the government and industry of analytical methods for calculating both the steady state and transient performance of an aircraft engine during an entire flight regime. The historical development of some of the analytical tools capable of evaluating installation effects on engine performance is traced and their present status is described.
Document ID
19800034083
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fishbach, L. H. (NASA Lewis Research Center Flight Performance Section, Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 80-0051
Report Number: AIAA PAPER 80-0051
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A18253
Distribution Limits
Public
Copyright
Other

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