Supersonic jet mixing enhancement by 'delta-tabs'

Author:

ZAMAN B.1,REEDER M.2,SAMIMY M.2

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Ohio State University, Columbus

Publisher

American Institute of Aeronautics and Astronautics

Cited by 19 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. Flow and acoustic characteristics of convergent-divergent nozzle with and without wedges;Materials Today: Proceedings;2023-04

2. Effect of varying velocity ratio on thin lip co-flowing jet;5TH INTERNATIONAL CONFERENCE ON INNOVATIVE DESIGN, ANALYSIS & DEVELOPMENT PRACTICES IN AEROSPACE & AUTOMOTIVE ENGINEERING: I-DAD’22;2023

3. Survey on Vortex Shedding Tabs as Supersonic Jet Control;Frontiers in Physics;2022-02-01

4. Effect of tabs on transverse jet instabilities, structure, vorticity dynamics and mixing;Journal of Fluid Mechanics;2021-05-05

5. Assessment of Short Rectangular-Tab Actuation of Supersonic Jet Mixing;Actuators;2020-08-21

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