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Axial-compressor flow distortion with water ingestionThe objective of the investigation is as follows: to establish relations between the steady state mean flow distortion generated during water ingestion into an axial-flow compressor and (a) characteristic length and time scales pertaining to (1) the centrifugal action and (2) the heat and mass transfer processes and (b) aerodynamic parameters based on blade geometry, aspect ratio and blade loading. Analytical and experimental results are presented for a small compressor to illustrate the extent of the distortion introduced as a function of (1) the operating speed and (2) the mass-based water content in the ingested mixture. Methods of scaling the effects in compressors of different sizes are discussed.
Document ID
19830035238
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tsuchiya, T.
(Purdue Univ. West Lafayette, IN, United States)
Murthy, S. N. B.
(Purdue University West Lafayette, IN, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 83-0004
Report Number: AIAA PAPER 83-0004
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A16456
Funding Number(s)
CONTRACT_GRANT: NAG3-204
CONTRACT_GRANT: NAG3-63
CONTRACT_GRANT: F33615-78-C-2401
Distribution Limits
Public
Copyright
Other

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