The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines
Description:
An 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.
Date:
September 14, 1938
Creator:
Rothrock, A. M. & Biermann, Arnold E.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department