On the basis of obtained analytical estimate of characteristics of hybrid solid-propellant rocket engine verification of earlier developed physical and mathematical model of processes in a hybrid solid-propellant rocket engine for quasi-steady-state flow regime was performed. Comparative analysis of calculated and analytical data indicated satisfactory comparability of simulation results.
|Journal||MATEC Web of Conferences|
|Publication status||Published - 9 Aug 2016|
|Event||Heat and Mass Transfer in the System of Thermal Modes of Energy - Technical and Technological Equipment, HMTTSC 2016 - Tomsk, Russian Federation|
Duration: 19 Apr 2016 → 21 Apr 2016
ASJC Scopus subject areas
- Materials Science(all)