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Publishing Language: Chinese

Spray Characteristics of Conical Atomizing Nozzles in Integrated Afterburner

Xin Xu1Bingbing Zhao1( )Li Fei2Kexuan Zou1Baoyuan Yang1
Aviation Engineering School, Air Force Engineering University, Xi’an 710038, China
Aviation Maintenance NCO School, Air Force Engineering University, Xinyang 464000, China
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Abstract

Experimental research was conducted on the fuel spray characteristics of conical atomizing nozzles in an integrated afterburner, analyzing the effects of transverse flow velocity and fuel supply pressure difference on the macroscopic and microscopic characteristics of the spray. Through LIF/Mie technology, it was found that the spray morphology of the conical atomizing nozzle was dominated by Rayleigh-Taylor and Kelvin-Helmholtz instability phenomena. The atomization effect at the top of the spray was good, but it was significantly affected by the transverse flow. Increasing the fuel supply pressure difference could increase the spray projection area and droplet velocity, but it would lead to an increase in droplet size. Increasing the transverse flow velocity to 30 m/s could reduce the droplet size to below 60 μm. In addition, although the baffle structure increased the droplet size, it broadened the spray distribution range.

CLC number: V233.7 Document code: A Article ID: 1006-8740(2026)04-0436-10

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Journal of Combustion Science and Technology
Pages 436-445

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Cite this article:
Xu X, Zhao B, Fei L, et al. Spray Characteristics of Conical Atomizing Nozzles in Integrated Afterburner. Journal of Combustion Science and Technology, 2026, 32(4): 436-445. https://doi.org/10.11715/rskxjs.R202604017

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Received: 10 March 2026
Published: 15 August 2026
© 2026 Journal of Combustion Science and Technology