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High Temperature Hydrocarbon Fuels and Subsonic Flight Environments
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1965 by SAE International in United States
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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.
CitationHager, J., "High Temperature Hydrocarbon Fuels and Subsonic Flight Environments," SAE Technical Paper 650115, 1965, https://doi.org/10.4271/650115.
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