Unsteady thermo-gasdynamic processes in rectangular scramjet combustion chamber with periodical input of cold air


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Combustion of hydrogen-air mixture under a periodical perpendicular injection of cold air is modeled. Fields of chemical species concentrations, pressure, and temperature are calculated by two-dimensional computational model based on unsteady governing equations including Navier-Stokes equations, energy conservation and diffusion equations together with system of chemical kinetic equations. Two-dimensional temperature, pressure and velocity visualization are presented. Method of the numerical simulation and details of the problem under consideration are presented in Ref.4.

сombustion, hydrogen, scramjet, chemical kinetics.


Volume 16, issue 3, 2015 year


Нестационарные газодинамические процессы в прямоугольном канале ГПВРД с периодическим вдувом холодного воздуха

В работе моделируется процесс горения водородо-воздушной смеси при периодическом вдуве холодного воздуха поперек основного сверхзвукового потока. Поля концентраций химических компонент, давления и температуры рассчитываются с помощью двумерной вычислительной модели, основанной на нестационарных уравнениях Навье-Стокса, сохранения энергии, уравнений диффузии и системы уравнений химической кинетики. Представлена визуализация двумерных расчетов полей температуры, скорости, давления и концентраций химических компонент.

горение, водород, ГПВРД, химическая кинетика


Volume 16, issue 3, 2015 year



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