Mathematical model of calculation thermo-physical properties of synthetic liquid fuel

Aerospace propulsion engineering


Аuthors

Raznoschikov V. V.1, Demskaya I. A.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 fuel


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