Studies on the effects of a subsonic flight environment on fuels refined for high Mach number application are reported. Requirements and hydrocarbon composition for fuel to withstand high Mach number stresses are cited and their compatibility with conventional systems at low temperatures is discussed.
High Temperature Hydrocarbon Fuels and Subsonic Flight Environments
Sae Technical Papers
1965 International Automotive Engineering Congress and Exposition ; 1965
1965-02-01
Conference paper
English
High temperature hydrocarbon fuels and subsonic flight environments
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