Increases in aircraft and engine performance are increasing the heat load being transferred into an aircraft's primary coolant--the fuel. This research is aimed at understanding the limitations of operation of fuel heated to 48 deg C (90 deg F) and beyond. Important issues are expected to be thermal stability, heat transfer/flow instabilities, and injection/combustion properties.
Advanced Supercritical Fuels
2001
4 pages
Report
Keine Angabe
Englisch
Combustion , Heat transfer , Coolants , Aviation fuels , Thermal stability , Physical & Theoretical Chemistry , Fuel injection , Rocket fuels , Chemical propulsion , Jp-8 fuel , Combustion & Ignition , Fuel additives , Component report , Symposia , Jet engine fuels , Crude oil , Hydrocarbons , Fuels , Supercritical flow , Propulsion systems
USAF supercritical hydrocarbon fuels interests
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