Shock patterns in a slightly underexpanded sonic jet controlled by radial injections-Reference-Cited by-同舟云学术

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Shock patterns in a slightly underexpanded sonic jet controlled by radial injections

Published:2007-04 Issue:4 Volume:19 Page:048104
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Chauvet Nicolas,Deck Sebastien,Jacquin Laurent

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/1.2720836

Reference3 articles.

1. Effect of Tab Parameters on Near-Field Jet Plume Development

2. THE METHOD OF CHARACTERISTICS FOR PROBLEMS OF COMPRESSIBLE FLOW INVOLVING TWO INDEPENDENT VARIABLES: PART I. THE GENERAL THEORY

3. M. Holt,Numerical Methods in Fluid Dynamics, Springer Series in Computational Physics (Springer-Verlag, Berlin, 1977), pp. 80–103.

Cited by 13 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. An experimental study on supersonic jet control using shifted air tabs;Journal of Thermal Engineering;2024

2. Control of sonic jets by fluidic injection;IOP Conference Series: Materials Science and Engineering;2020-08-01

3. Study of Correctly Expanded Sonic Jet with Air Tabs;International Journal of Turbo & Jet-Engines;2020-04-24

4. Flow visualization of the jet exiting a chevron nozzle;Aeronautics and Aerospace Open Access Journal;2018-03-23

5. AR 4 elliptic jet control with limiting tab;Fluid Dynamics Research;2018-01-24

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