| 注册
首页|期刊导航|航空学报|激光转塔跨声速流动特性及气动光学效应

激光转塔跨声速流动特性及气动光学效应

谭小童 许和勇

航空学报2025,Vol.46Issue(14):144-156,13.
航空学报2025,Vol.46Issue(14):144-156,13.DOI:10.7527/S1000-6893.2024.31493

激光转塔跨声速流动特性及气动光学效应

Flow feature and aero-optical effect for laser turret in transonic flow

谭小童 1许和勇1

作者信息

  • 1. 西北工业大学 航空学院,西安 710072||飞行器基础布局全国重点实验室,西安 710072
  • 折叠

摘要

Abstract

Improved Delayed Detached Eddy Simulation(IDDES)is used to calculate the flow field around the turret in transonic flow.The ray tracing method is employed to calculate the aero-optical effect at different beam emission angles.The aero-optical effect affected by different flow structures is analyzed.The results indicate that the pressure distribution on the turret exhibits two main characteristics:a symmetric"breathing mode"and an antisymmetric"shifting mode".Their peak frequency are at 0.26-0.41 and 0.11-0.22,respectively,and these two main features exhibit coherence in the fre-quency.The drag force of the turret is primarily determined by shear layer oscillation,the lateral force is largely due to the shock wave jitter,and the axial force is influenced by both shock wave jitter and shear layer oscillation.The high-order Optical Path Difference(OPD)is relatively small with little fluctuation when the beam passes through the attached flow re-gion.However,when the beam traverses the shock wave region and the turbulent wake zone,the high-order OPD is sig-nificantly large,with the time-averaged OPD being about four times that of the attached flow region,and the peak OPD being 13 times greater than that of the attached flow.The high-order OPD of the beam passing through the shear layer and turbulent wake vortices shows similar energy ratio using Proper Orthogonal Decomposition(POD)analysis.In con-trast,the OPD energy of beams passing through the shock wave is more concentrated in the first five modes.

关键词

改进的延迟脱体涡模拟/跨声速流动/气动光学效应/本征正交分解/动力学模态分解

Key words

improved delated detached eddy simulation/transonic flow/aero-optical effect/proper orthogonal decomposition/dynamic mode decomposition

分类

航空航天

引用本文复制引用

谭小童,许和勇..激光转塔跨声速流动特性及气动光学效应[J].航空学报,2025,46(14):144-156,13.

基金项目

西北工业大学博士论文创新基金(CX2025031) Innovation Foundation for Doctor Dissertation of Northwestern Polytechnical University(CX2025031) (CX2025031)

航空学报

OA北大核心

1000-6893

访问量0
|
下载量0
段落导航相关论文