Study of decay, spread, and shock structure of a supersonic jet issuing from a C-D nozzle with semi-circular grooves-Reference-Cited by-同舟云学术

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Study of decay, spread, and shock structure of a supersonic jet issuing from a C-D nozzle with semi-circular grooves

Published:2022-10-14 Issue:3 Volume:29 Page:327-346
ISSN:1531-8699
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Ilakkiya S.,Sridhar B. T. N.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

https://link.springer.com/content/pdf/10.1134/S0869864322030027.pdf

Reference34 articles.

1. A. Khan, R. Kumar, S.B. Verma, and C. Manisankar, Effect of cross wire tab orientation on twin jet mixing characteristics, Experimental Thermal and Fluid Science, 2018, Vol. 99, P. 344–356.

2. B.V.N. Charyulu, J. Kurain, P. Venugopalan, and V. Sriramulu, Experimental study on mixing enhancement in two-dimensional supersonic flow, Experiments in Fluids, 1998, Vol. 39, P. 340 -346.

3. D.C. McCormick and J.C. Bennett Jr., Vortical and turbulent structure of a lobed mixer free shear layer, AIAA Journal, 1994, Vol. 32, No. 9, P. 1852–1859.

4. B.B. Lyu and A.P. Dowling, An experimental study of the effects of lobed nozzles on installed jet noise, Experiments in Fluids, 2019, Vol. 60, P. 176–1–176–12.

5. K.B.M.Q. Zaman, Spreading characteristics of compressible jets from nozzles of various geometries, J. Fluid Mechanics, 1999, Vol. 383, P. 197–228.

Cited by 1 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. Manipulation of Supersonic Jet using Grooved Tabs;Journal of Applied Fluid Mechanics;2024-05-01

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