In the present study calculations algorithm of gas flow of ramjet engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for ramjet model which consists of air intake, combustion chamber, nozzle and supersonic jet. The results in agreement with known solutions for cold blowing of ramjet gas-dynamic paths.
Перспективы развития фундаментальных наук : сборник научных трудов XIV Международной конференции студентов, аспирантов и молодых ученых, Россия, Томск, 25-28 апреля 2017 г.. Томск, 2017. Т. 1 : Физика. С. 174-176