NDLI: Advanced technologies impact on compressor design and development: a perspective

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Advanced technologies impact on compressor design and development: a perspective

Content Provider	NASA Technical Reports Server (NTRS)
Author	Ball, Calvin L.
Copyright Year	1989
Description	A 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.
File Size	1569933
Page Count	18
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19900001575
Archival Resource Key	ark:/13960/t9b61gh9p
Language	English
Publisher Date	1989-09-01
Access Restriction	Open
Subject Keyword	Aircraft Propulsion And Power Equipment Specifications Compressor Rotors Engine Design Systems Engineering Turbine Wheels Gas Turbine Engines Performance Prediction Research Projects Turbofan Engines Aircraft Engines Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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