Effect of Co-Flow on Near Field Shock Structure

Author:

Srinivasarao T.1,Lovaraju P.1,Rathakrishnan E.2

Affiliation:

1. Department of Mechanical Engineering, Lakireddy Balireddy College of Engineering, Mylavaram, India

2. Department of Aerospace Engineering, IIT Kanpur, Kanpur, India

Abstract

This paper presents the experimental results of underexpanded jets delivered from a central nozzle surrounded by a co-flow. The co-flow is found to be effective in elongating the supersonic core length of the central jet, at all levels of underexpansion. However, the expansion level of the central jet dictates the elongation caused by the co-flow.

Publisher

ASME International

Subject

Mechanical Engineering

Cited by 16 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Effect of increasing bypass ratio on supersonic co-flowing jet with finite lip thickness;International Journal of Heat and Fluid Flow;2024-07

2. Influence of orifice thickness on the flow field of co-flow jets;Journal of Physics: Conference Series;2023-05-01

3. Supersonic jet mixing in the presence of two annular co-flow streams;International Journal of Turbo & Jet-Engines;2023-02-28

4. Mach number variation in subsonic co-flowing jets;5TH INTERNATIONAL CONFERENCE ON INNOVATIVE DESIGN, ANALYSIS & DEVELOPMENT PRACTICES IN AEROSPACE & AUTOMOTIVE ENGINEERING: I-DAD’22;2023

5. On the influence of co-flow on the shocks and vortex rings in the starting phases of under-expanded jets;Physics of Fluids;2022-07

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