Mathematical model of calculation thermo-physical properties of synthetic liquid fuel
Aerospace propulsion engineering
Аuthors
1, 2*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
*e-mail: Demskaya.Ilyana@mail.ru
Abstract
The 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 fuelDownload