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Advanced technologies impact on compressor design and development: A perspectiveA historical perspective of the impact of advanced technologies on compression system design and development for aircraft gas turbine applications is presented. A bright view of the future is projected in which further advancements in compression system technologies will be made. These advancements will have a significant impact on the ability to meet the ever-more-demanding requirements being imposed on the propulsion system for advanced aircraft. Examples are presented of advanced compression system concepts now being studied. The status and potential impact of transitioning from an empirically derived design system to a computationally oriented system are highlighted. A current NASA Lewis Research Center program to enhance this transitioning is described.
Document ID
19900001575
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ball, Calvin L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-102341
E-5039
NAS 1.15:102341
Meeting Information
Meeting: Aerotech ''89
Location: Anaheim, CA
Country: United States
Start Date: September 25, 1989
End Date: September 28, 1989
Sponsors: SAE
Accession Number
90N10891
Funding Number(s)
PROJECT: RTOP 535-505-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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