A correlation of the effects of compression ratio and inlet-air temperature on the knock limits of aviation fuels in a CFR engine 2
Description: Report presenting the knock-limited performance of nine fuels comprising isolated members of four classes of hydrocarbons in the form of three-dimensional plots of fuel-air ratio, compression temperature, and compression-air density.
Date: June 1946
Creator: Alqusit, Henry E.; O'Dell, Leon & Evvard, John C.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department