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The use of AntiMisting Kerosene (AMK) in turbojet enginesThe effect of antimisting kerosene (AMK) flow characteristics on fan jet engines and the impact of degradation requirements on the fuel system was evaluated. It was determined from the present program that AMK fuel cannot be used without predegradation, although some degradation occurs throughout the fuel feed system, expecially in the fuel pumps. There is a tendency toward FM-9 AMK additive agglomeration and gel formation when the liquid flows at a critical velocity through very small passages. The data indicate this phenomenon to be a function of the degree of degradation, the passage size, the differential pressure, the fluid temperature, and the accumulated flow time. Additionally, test results indicate that the long term cumulative effects of this phenomenon may require more degradation than the theoretical requirement determined from short term tests.
Document ID
19810010537
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmidt, H. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1981
Publication Information
Publication: NASA. Langley Research Center The 1980 Aircraft Safety and Operating Probl., Pt. 2
Subject Category
Air Transportation And Safety
Accession Number
81N19063
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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