A swirlingstyle propellant water ramjet model was established on the basis of a particular model of columnstyle propellant water ramjet. The effect of swirling flow on the flow and reaction characteristics in the water ramjet was simulated by Fluent software. Turbulent flow simulation was performed using the standard kε two equation functions
and combustion reaction was calculated by finiterate/eddydissipation model. The functions were solved by implicit coupling calculation method based on the density. Results show that
adding swirling vanes and increasing the swirling angle can improve the maximum temperature
the average temperature
the outlet velocity and the specific impulse
which proves that adding swirling vanes make drastic improvements of flow and combustion reaction in the water ramjet engine
and the greater swirling angle means the better results.
Unsteady swirling flow in low emissions stirred swirls combustor
Dynamic response characteristic of concentric stage swirling structure
基于三维接触摩擦单元的套齿连接解析建模研究
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
基于自适应MOMEDA滚动轴承故障特征提取方法
Related Author
QIN Hao
DING Zhi-lei
LI Hai-tao
LIN Yu-zhen
LI Ji-bao
QIN Hao
DING Zhi-lei
LIN Yu-zhen
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics of Astronautics
Commercial Aircraft Engine Company Limited, Aviation Industry Corporation of China
School of Energy and Power Engineering, Beijing University of Aeronautics of Astronautics