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带内埋质量超声速悬臂板的颤振特性

祁武超 俞浩洋 田素梅 刘宏亮

沈阳航空航天大学学报2024,Vol.41Issue(2):1-13,13.
沈阳航空航天大学学报2024,Vol.41Issue(2):1-13,13.DOI:10.3969/j.issn.2095-1248.2024.02.001

带内埋质量超声速悬臂板的颤振特性

Flutter characteristics of supersonic cantilever plate with embedded mass

祁武超 1俞浩洋 1田素梅 1刘宏亮1

作者信息

  • 1. 沈阳航空航天大学 辽宁省飞行器复合材料结构分析与仿真重点实验室,沈阳 110136
  • 折叠

摘要

Abstract

In order to improve the flutter velocity of a lifting surface with embedded mass,the lifting surface was simplified as a rectangular cantilever plate with concentrated mass.Based on the assumed mode method and the first-order piston theory,a flutter model was obtained,and flutter characteristics of the rectangular cantilever plate were investigated.Firstly,the structural dynamic model of the rectan-gular cantilever plate was established based on the Kirchhoff thin plate theory,and the modal properties of the plate with embedded mass were obtained using the assumed mode method;secondly,the first-or-der piston theory was introduced to approximate the modal aerodynamic force under supersonic condi-tions,and the time-domain expression of the flutter equation was obtained by substituting it into the structural dynamics model;finally,the flutter equation was transformed into the frequency domain by introducing the modal displacement in exponential form,and the flutter velocities and flutter frequen-cies were solved by the p-k method.By changing the position,mass,number,and other parameters of embedded objects,the law of their influence on the flutter characteristics of the supersonic cantilever plate were obtained.The results show that the flutter velocity of the lifting surface can be effectively in-creased by embedding small mass objects near the leading edge of the cantilever plate near the wing tip,and the flutter velocity is insensitive to the change of the embedded mass near the wing root.

关键词

颤振/内埋质量/活塞理论/假设模态法/超声速悬臂板

Key words

flutter/embedded mass/piston theory/the assumed mode method/supersonic cantilever plate

分类

航空航天

引用本文复制引用

祁武超,俞浩洋,田素梅,刘宏亮..带内埋质量超声速悬臂板的颤振特性[J].沈阳航空航天大学学报,2024,41(2):1-13,13.

基金项目

国家自然科学基金(项目编号:12002218) (项目编号:12002218)

辽宁省教育厅项目(项目编号:JYT2020034,JYT2020029) (项目编号:JYT2020034,JYT2020029)

沈阳航空航天大学学报

2095-1248

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