Experimental investigation of cold ejecting characteristics and primary-secondary flow interaction in a strut-jet RBCC flowpath

IF 2.6 3区 工程技术 Q2 ENGINEERING, MECHANICAL
Feiteng Luo , Dahao Yao , Xinke Li , Zhenming Qu , Wenjuan Chen , Yaosong Long , Qiang Cheng , Zixue Luo
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引用次数: 0

Abstract

Based on a typical strut-jet Rocket-Based Combined Cycle (RBCC) engine’s characteristic flow channel model, extensive cold jet entrainment experiments were carried out over a broad range of conditions, involving different ejector inlet configurations and strut-jet configurations. The study has provided an understanding of the entrainment air intake characteristics, as well as the interaction features and patterns between the primary and secondary flows. The research findings indicate that as the mass rate of primary flow and total pressure ratio increase, the Mach number of the secondary flow gradually increases, and the flow rate increases to a certain maximum value, while the entrainment ratio continues to decrease monotonically. Dimensional analysis shows that increasing the contraction ratio and contraction angle of the ejector inlet configuration can enhance the entrainment capability of the primary flow at low total pressure ratios, but the impact is smaller at high total pressure ratios. The strut-jet configuration with a single rectangular nozzle has a stronger entrainment capability compared to the configuration with a double circular nozzle. It can increase the mass flux ratio by 10% to 40% under the same mass rate of primary flow and nozzle throat area, and the structure with a wavy groove at the trailing edge of the strut is conducive to enhancing the entrainment capability. As the total pressure ratio between the primary and secondary flows increases, the velocity ratio and convective Mach number show a decreasing trend, while the static pressure ratio and density ratio increase. Ejector inlet configurations with a larger contraction ratio and double circular nozzle configurations lead to higher velocity ratios and convective Mach numbers, but lower static pressure and density ratios. These variations in parameter gradients determine the primary-secondary flow interaction processes and characteristics from the initial state perspective.
支柱-射流RBCC流道冷射特性及一次-二次流相互作用实验研究
基于典型的柱喷联合循环(RBCC)发动机的特征流道模型,在广泛的条件下进行了大量的冷射流夹带实验,包括不同的引射入口配置和柱喷配置。研究提供了对夹带进气特征的理解,以及一次流和二次流之间的相互作用特征和模式。研究结果表明,随着一次流质量率和总压比的增大,二次流马赫数逐渐增大,流量增大到一定最大值,而夹带比继续单调减小。量纲分析表明,在低总压比下,增加引射入口结构的收缩比和收缩角可以增强一次流的带气能力,但在高总压比下影响较小。单矩形喷嘴的支杆射流结构比双圆形喷嘴的支杆射流结构具有更强的夹带能力。在一次流质量率和喷管喉道面积相同的情况下,可使质量通量比提高10% ~ 40%,支板尾缘带波浪形槽的结构有利于增强夹带能力。随着一次流和二次流总压比的增大,速度比和对流马赫数呈减小趋势,而静压比和密度比呈增大趋势。较大收缩比的引射入口配置和双圆形喷管配置可以提高速度比和对流马赫数,但降低静压和密度比。这些参数梯度的变化从初始状态的角度决定了一次-二次流相互作用的过程和特征。
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来源期刊
International Journal of Heat and Fluid Flow
International Journal of Heat and Fluid Flow 工程技术-工程:机械
CiteScore
5.00
自引率
7.70%
发文量
131
审稿时长
33 days
期刊介绍: The International Journal of Heat and Fluid Flow welcomes high-quality original contributions on experimental, computational, and physical aspects of convective heat transfer and fluid dynamics relevant to engineering or the environment, including multiphase and microscale flows. Papers reporting the application of these disciplines to design and development, with emphasis on new technological fields, are also welcomed. Some of these new fields include microscale electronic and mechanical systems; medical and biological systems; and thermal and flow control in both the internal and external environment.
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