Mathematical model of calculation thermo-physical properties of synthetic liquid fuel
Aerospace propulsion engineering
1. Zhukovsky Air Force Engineering Academy, 3, Planetnaya str., Moscow, 125190, Russia
2. Central Institute of Aviation Motors, CIAM, 2, Aviamotornaya St., Moscow, 111116, Russia
AbstractThe paper represents the mathematical model (MM) of thermo-physical properties of fuels and individual hydrocarbons (IH) and their mixes in various ratio, and also synthetic liquid fuel (SLF) is submitted. Results of experiments by determination thermo-physical properties individual hydrocarbons and their mixes which were compared with results of calculation of MM are submitted.
Keywords:mathematical model, synthetic liquid fuel