摘要
为了寻求有效的流动控制方法来降低隔离段总压损失,基于非定常雷诺平均的Navier-Stokes方程,探究激光脉冲能量沉积对二维及三维隔离段流场马赫反射的控制效果。在来流马赫数分别为1.61和2.51的隔离段流场马赫反射上游,加入脉冲能量沉积,对比激励流场与基础流场。结果表明:能量沉积主要通过高温热核和其诱导的压力波两种方式对马赫反射结构施加作用,显著地影响了马赫反射结构,促使Ma_(∞)=1.61来流工况下马赫杆的高度减小,马赫反射强度减弱;Ma_(∞)=2.51来流工况下的马赫反射结构转变为稳定的正规反射,减小了总压损失。控制过程包括:(1)能量沉积产生的局部高温降低当地马赫数,减小马赫反射强度;(2)高温热核诱导的弓形波与马赫反射相互作用,马赫反射结构变形;(3)以反压形式影响马赫反射。
In order to find an effective flow control method to reduce the total pressure loss in isolator,the unsteady Reynolds averaged Navier-Stokes equations are used to simulate the control effect of laser pulse energy deposition on the Mach reflection for the two and three-dimensional isolator. The laser pulse energy deposition is introduced upstream of the Mach reflection of the flow field in isolator with incoming flow Mach numbers of 1.61and 2.51,respectively. Compared the excitation flow field with the basic flow field,results show that the energy deposition affects the Mach reflection mainlythrough the high temperature spot and its induced pressure waves,and it has a significant impact on the Mach reflection. At Mach number of 1.61,the energy deposition promotes the height of the Mach stem to reduce,and the intensity of the Mach reflection decreases accordingly. At Mach number of 2.51,the transformation of the Mach reflection into a stable regular reflection occurs,reducing the total pressure loss. The control process includes:(1)The local high temperature of the energy deposition reduces the local Mach number,thereby weakens the intensity of the Mach reflection.(2)The high temperature thermal spot induces the bow wave to interact with the Mach reflection,and the Mach reflection is deformed.(3)The energy deposition affects the Mach reflection in the form of the back-pressure.
作者
王旺
刘凡
严红
WANG Wang;LIU Fan;YAN Hong(Yangtze River Delta Research Institute,Northwestern Polytechnical University,Taicang 215400,China;Science and Technology on Space Physics Laboratory,Beijing100076,China;Shaanxi Key Laboratory of Internal Aerodynamics in Aero-Engine,Northwestern Polytechnical University,Xi’an 710072,China)
出处
《推进技术》
EI
CAS
CSCD
北大核心
2022年第10期104-118,共15页
Journal of Propulsion Technology
基金
国家自然科学基金(11672242)。
关键词
激波控制
能量沉积
马赫反射
正规反射
隔离段
数值模拟
Shock control
Energy deposition
Mach reflection
Regular reflection
Isolator
Numerical simulation
