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Dynamic Performance of High Bypass Ratio Turbine Engines With Water IngestionThe research on dynamic performance of high bypass turbofan engines includes studies on inlets, turbomachinery and the total engine system operating with air-water mixture; the water may be in vapor, droplet, or film form, and their combinations. Prediction codes (WISGS, WINCOF, WINCOF-1, WINCLR, and Transient Engine Performance Code) for performance changes, as well as changes in blade-casing clearance, have been established and demonstrated in application to actual, generic engines. In view of the continuous changes in water distribution in turbomachinery, the performance of both components and the total engine system must be determined in a time-dependent mode; hence, the determination of clearance changes also requires a time-dependent approach. In general, the performance and clearances changes cannot be scaled either with respect to operating or ingestion conditions. Removal of water prior to phase change is the most effective means of avoiding ingestion effects. Sufficient background has been established to perform definitive, full scale tests on a set of components and a complete engine to establish engine control and operability with various air-water vapor-water mixtures.
Document ID
19960018580
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Murthy, S. N. B.
(Purdue Univ. West Lafayette, IN United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1996
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-CR-4703
M/NAFA/95-F
E-10085
DOT/FAA/AR95-96
NAS 1.26:4703
Report Number: NASA-CR-4703
Report Number: M/NAFA/95-F
Report Number: E-10085
Report Number: DOT/FAA/AR95-96
Report Number: NAS 1.26:4703
Accession Number
96N23782
Funding Number(s)
OTHER: DTFA03-83-A-00328
CONTRACT_GRANT: NAG3-481
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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