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WINCOF-I code for prediction of fan compressor unit with water ingestionThe PURDUE-WINCOF code, which provides a numerical method of obtaining the performance of a fan-compressor unit of a jet engine with water ingestion into the inlet, was modified to take into account: (1) the scoop factor, (2) the time required for the setting-in of a quasi-steady distribution of water, and (3) the heat and mass transfer processes over the time calculated under 2. The modified code, named WINCOF-I was utilized to obtain the performance of a fan-compressor unit of a generic jet engine. The results illustrate the manner in which quasi-equilibrium conditions become established in the machine and the redistribution of ingested water in various stages in the form of a film out of the casing wall, droplets across the span, and vapor due to mass transfer.
Document ID
19900012408
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Murthy, S. N. B.
(Purdue Univ. West Lafayette, IN, United States)
Mullican, A.
(Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-CR-185157
NAS 1.26:185157
M/NAFA/89-1
DOT/FAA/CT-TN89/63
Report Number: NASA-CR-185157
Report Number: NAS 1.26:185157
Report Number: M/NAFA/89-1
Report Number: DOT/FAA/CT-TN89/63
Accession Number
90N21724
Funding Number(s)
PROJECT: RTOP 505-62-21
CONTRACT_GRANT: DTFA03-83-A-00328
CONTRACT_GRANT: NAG3-481
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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