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Flow Characteristics and Stability of Induced Shock Waves in the Isolator of Rotating Detonation Ramjet under Flight Mach Number 2.5 Conditions

AEROSPACE SCIENCE AND TECHNOLOGY(2023)

Sun Yat Sen Univ

Cited 1|Views14
Abstract
A 3D numerical simulation of a rotating detonation ramjet engine (RDRE) with isolator and combustor was performed under flight Mach number 2.5 conditions. Factors that influence the stable operation of isolator, such as equivalence ratio, length and expansion ratio of the isolator, were systematically investigated. The structure and stability mechanism of shock wave in the isolator wave were also investigated. Results show that the shock waves in the isolator are mainly composed of the spiral shock wave band (SSWB) and the leading shock wave (LSW), which are induced by the detonation wave and the strong disturbance of SSWB in the supersonic incoming flow, respectively. The airflow behind the LSW obtains the total pressure gain caused by the work of SSWB, when SSWB moves toward the isolator inlet. The speed of LSW is mainly affected by the pressure of detonation wave. The greater the pressure of the detonation wave, the faster the speed of LSW. When the total pressure at the leading edge of SSWB is lower than that of the incoming flow, LSW will stabilize in the isolator. A concept of critical pressure ratio was proposed in the present study, which is the ratio of the average total pressure of the rotating detonation wave to the total pressure at the isolator inlet. In the research configuration and working conditions of this paper, the critical pressure ratio is slightly smaller than 6 when the equivalence ratio of H2/Air premixed mixture is 0.7, below which the isolator can work continuously and stably.
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Key words
Flow stability,Isolator,Rotating detonation,The spiral shock band,The critical pressure ratio
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要点】:本文通过3D数值模拟研究了旋转爆震冲压发动机隔离器内激波特性及其稳定性,提出了临界压力比的概念,确定了影响隔离器稳定性的关键因素。

方法】:采用3D数值模拟方法对旋转爆震冲压发动机的隔离器和燃烧室进行模拟,在飞行马赫数2.5的条件下,系统研究了当量比、隔离器长度和扩张比对隔离器稳定性的影响。

实验】:实验通过模拟计算完成,使用的数据集为旋转爆震冲压发动机的数值模型,结果表明螺旋激波波带(SSWB)和领先激波(LSW)是隔离器内主要激波结构,临界压力比是判断隔离器能否连续稳定工作的关键参数。