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Aeronautical propulsion: Present status and future directionsThe advancement of aeropropulsion systems continues to provide technology to various portions of the gas turbine field. It is recognized that this area is undergoing considerale change, which will result in substantially improved gas turbine components and systems. These changes are occurring in a number of technical areas including advanced analytical and physical measurement methods, the application of large scientific computers, the dynamic modeling of components and systems, the application of integrated control systems that optimize and improve performance and system condition monitoring, and the development of new and unique materials and structures. As these areas evolve, the ways in which technology will advance, and factors affecting the design and development of new systems, will probably be considerably different than those of today. It is also anticipated that the necessary skilled work force will be different. Certainly there will be changes, but the nature, extent, and rate of those changes can only be surmised at this time.
Document ID
19840008051
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hartmann, M. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:83589
NASA-TM-83589
E-1987
Report Number: NAS 1.15:83589
Report Number: NASA-TM-83589
Report Number: E-1987
Meeting Information
Meeting: Intern. Gas Turbine Conference
Location: Amsterdam
Start Date: June 3, 1984
End Date: June 7, 1984
Accession Number
84N16119
Funding Number(s)
PROJECT: RTOP 505-40-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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