Journal of Flow Control, Measurement & Visualization

Volume 2, Issue 1 (January 2014)

ISSN Print: 2329-3322   ISSN Online: 2329-3330

Flow Visualization on Lateral Multiple Jet Interaction with Freestream

HTML  Download Download as PDF (Size: 2809KB)  PP. 7-11  
DOI: 10.4236/jfcmv.2014.21002    3,450 Downloads   6,377 Views  Citations

ABSTRACT

The interaction flowfield of gaseous jets ejecting from three different orifice configurations into a Mach 5 turbulent crossflow over a flat plate was investigated experimentally. These jet configurations have equal equivalent throat diameter of 6 mm and nominal exit Mach number of 3. Schlieren photography was used to visualize the spatial flow structures; meanwhile surface oil flow patterns were employed to identify the separation and reattachment regions on the flat plate. Results show the influence of the jet-to-freestream static pressure ratio and jet configurations on flow interaction characteristics.

Share and Cite:

Chen, P. , Li, S. , Luo, S. and Ni, Z. (2014) Flow Visualization on Lateral Multiple Jet Interaction with Freestream. Journal of Flow Control, Measurement & Visualization, 2, 7-11. doi: 10.4236/jfcmv.2014.21002.

Cited by

[1] Characterization of the Mixing Induced by Multiple Elevated Jets in Cross Flow
2020
[2] Dynamics of the flow field induced by multiple elevated jets in crossflow
2019
[3] Wind tunnel experiments of multijets in cross flow: Effect of the injection ratio
2019
[4] Multiple Fume Jets in Environmental Cross flows
Conference Paper, 2019
[5] Dynamics of Multiple elevated Jets in Cross flow
International Journal of Scientific Research & Engineering Technology, 2019
[6] Analysis of the impact of high temperature supersonic jets in low-thrust engines
Engineering Journal: Science and Innovation, 2018
[7] Исследование воздействий высокотемпературных сверхзвуковых струй двигателей малой тяги
2018
[8] 翼梢侧向喷流干扰特性数值模拟
2018
[9] Numerical Simulation of a Flowfield Around a Hypersonic Missile with Lateral Jets
ProQuest Dissertations Publishing, 2017

Copyright © 2024 by authors and Scientific Research Publishing Inc.

Creative Commons License

This work and the related PDF file are licensed under a Creative Commons Attribution 4.0 International License.