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The knocking characteristics of fuels in relation to maximum permissible performance of aircraft enginesAn analysis is presented of the relationship of various engine factors to knock in preignition in an aircraft engine. From this analysis and from the available experimental data, a method of evaluating the knocking characteristics of the fuel in an aircraft-engine cylinder is suggested.
Document ID
19930091730
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rothrock, A M
Biermann, Arnold E
Date Acquired
September 6, 2013
Publication Date
January 1, 1939
Report/Patent Number
NACA-TR-655
Report Number: NACA-TR-655
Accession Number
93R21020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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