CASPIAN JOURNAL

MANAGEMENT AND HIGH TECHNOLOGIES

Models of spatial supersonic flow of a perfect gas with transverse blowing jets

Read Beketaeva Asel O., Duyshenaliev Turatbek B. Models of spatial supersonic flow of a perfect gas with transverse blowing jets // Caspian journal : management and high technologies. — 2015. — №2. — pp. 119-129.

Beketaeva Asel O. - Ph.D. (Physical and Mathematical), Senior Researcher, Institute of Mathematics and Mathematical Modeling of Ministry of Education and Science, 125 Pushkin St., Almaty, 050010, Republic of Kazakhstan, azimaras@mail.ru

Duyshenaliev Turatbek B. - D.Sc. (Physical and Mathematical), Professor, Rector, Kyrgyz State Technical University named after I. Razzakov, 66 Mira Ave., Bishkek, 720044, Kyrgyz Republic, rector@kstu.kg; duishenaliev@mail.ru

In article is considered the problem of round stream cross input of in supersonic stream. This task has important applied value, concerning ensuring overall performance of aircraft engines - including with the truncated take off and landing, deck aircraft planes so forth. Authors are presented mathematical problem definition, proved its formalization for modeling. Modeling was carried out in number - with use of averaged by Reynolds Navier-Stokes's equations for perfect gas. In article are described used sampling in spatial-time area. Authors are investigated characteristics of a flow by the main stream at В«virtual obstacleВ», created by a cross input of additional stream. Results are visualized by means of В«fields of currentsВ» pictures and compared with the available experimental data. Received results of computer modeling for distribution of speed fields qualitatively coordinated with known experimental data.

Key words: число Рейнольдса, сверхзвуковой поток, число Прандля, коэффициент вязкости, тензор напряжения, турбулентность, компьютерное моделирование, методы визуализации, Reynolds number, supersonic flow, the Prandtl number, the coefficient of viscosity, stress tens