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Design geometry and design/off-design performance computer codes for compressors and turbinesThis report summarizes some NASA Lewis (i.e., government owned) computer codes capable of being used for airbreathing propulsion system studies to determine the design geometry and to predict the design/off-design performance of compressors and turbines. These are not CFD codes; velocity-diagram energy and continuity computations are performed fore and aft of the blade rows using meanline, spanline, or streamline analyses. Losses are provided by empirical methods. Both axial-flow and radial-flow configurations are included.
Document ID
19960008691
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Glassman, Arthur J. (Toledo Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1995
Publication Information
Publisher: NASA. Lewis Research Center
Subject Category
Aerodynamics
Report/Patent Number
E-10041
NASA-CR-198433
NAS 1.26:198433
NIPS-95-06493
Accession Number
96N15857
Funding Number(s)
PROJECT: RTOP 505-69-50
CONTRACT_GRANT: NAG3-1165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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