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Coordinates for a High Performance 4:1 Pressure Ratio Centrifugal CompressorThe objective of this program was to define the aerodynamic design and manufacturing coordinates for an advanced 4:1 pressure ratio, single stage centrifugal compressor at a 10 lbm/sec flow size. The approach taken was to perform an exact scale of an existing DDA compressor originally designed at a flow size of 3.655 lbm/sec.
Document ID
19970024917
Document Type
Contractor Report (CR)
Authors
McKain, Ted F. (Detroit Diesel Allison Indianapolis, IN United States)
Holbrook, Greg J. (Detroit Diesel Allison Indianapolis, IN United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1997
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
E-10833
NAS 1.26:204134
NASA-CR-204134
Funding Number(s)
CONTRACT_GRANT: NAS3-23268
PROJECT: RTOP 523-26-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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