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Publishing Language: Chinese | Open Access

Key aerodynamic issues and development tendency of internal weapons bay of advanced fighters

Xin JIN1,4Dangguo YANG2,3( )Guangping CAI1Jifei WU3Laiwu XU3Fusheng LIU2,3
Chengdu Aircraft Design & Research Institute, Aviation Industry Corporation of China, Chengdu 610091, China
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China
High Speed Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
School of Aerospace Engineering, Tsinghua University, Beijing 100084, China
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Abstract

Internal weapons bay can considerably improve the overall aerodynamic performance of advanced fighters. However, during the bomb dropping, the structural vibration and aerodynamic noise induced by flow fields around internal weapons bay will significantly undermine fighters' safety. This paper first briefly introduces the development of internal weapons bay and summarizes related research regarding cavity-flow-induced vibrations and aerodynamic noise. Later, design requirements for internal weapons bay are proposed based on a systematic analysis of the complex cavity flows related to internal weapons bay. At last, critical technical difficulties and some future research directions are discussed after a thorough study of flow mechanism, numerical simulation methods, wind test techniques, and control strategies for fluid-structure-noise coupled systems. This paper is helpful to the understanding of vital aerodynamic issues related to internal weapons bay. It also provides research directions to the cavity-flow-induced noise and vibrations.

CLC number: V211.5 Document code: A

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Acta Aerodynamica Sinica
Pages 152-159

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Cite this article:
JIN X, YANG D, CAI G, et al. Key aerodynamic issues and development tendency of internal weapons bay of advanced fighters. Acta Aerodynamica Sinica, 2022, 40(3): 152-159. https://doi.org/10.7638/kqdlxxb-2022.0060

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Received: 23 March 2022
Revised: 19 April 2022
Published: 30 May 2022
© The journal of Acta Aerodynamica Sinica.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).