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Investigation of the jet-wake flow of a highly loaded centrifugal compressor impellerInvestigations, aimed at developing a better understanding of the complex flow field in high performance centrifugal compressors were performed. Newly developed measuring techniques for unsteady static and total pressures as well as flow directions, and a digital data analysis system for fluctuating signals were thoroughly tested. The loss-affected mixing process of the distorted impeller discharge flow was investigated in detail, in the absolute and relative system, at impeller tip speeds up to 380 m/s. A theoretical analysis proved good coincidence of the test results with the DEAN-SENOO theory, which was extended to compressible flows.
Document ID
19780008108
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Eckardt, D.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1978
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-75232
Report Number: NASA-TM-75232
Accession Number
78N16051
Funding Number(s)
CONTRACT_GRANT: NASW-2790
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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