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地面对双轨超声速火箭橇的气动特性影响研究

王方元 林晓辉 余元元 董凌锋 郑达仁 许常悦

航空科学技术2024,Vol.35Issue(4):31-39,9.
航空科学技术2024,Vol.35Issue(4):31-39,9.DOI:10.19452/j.issn1007-5453.2024.04.005

地面对双轨超声速火箭橇的气动特性影响研究

Effect of Ground on Aerodynamic Performance of a Double-track Supersonic Rocket-sled

王方元 1林晓辉 2余元元 3董凌锋 2郑达仁 2许常悦1

作者信息

  • 1. 南京航空航天大学 飞行器环境控制与生命保障工业与信息化部重点实验室,江苏 南京 210016||航空防护救生技术航空科技重点实验室,湖北 襄阳 441003
  • 2. 南京航空航天大学 飞行器环境控制与生命保障工业与信息化部重点实验室,江苏 南京 210016
  • 3. 航空工业航宇救生装备有限公司,湖北 襄阳 441003
  • 折叠

摘要

Abstract

The aerodynamic characteristics of the rocket sled are significantly influenced by the ground as the rocket sled moves along the track.To analyze the flow field and force characteristics of the double-track rocket sled,changes in the flow field,time-averaged force and their characteristics in both time and frequency domain are investigated using scale adaptive simulation(SAS)and the dynamic mesh method at a Ma 2.The results show that the reflection of shock waves and compression waves on the ground facilities could lead to 6 extra high-pressure areas on the lower surface of the double-track rocket sled,and 4 of them could change with different reflection positions.The ground environment causes the time-average lift to increase by 9.6 times.The pressure signal and instantaneous aerodynamic force indicate strict periodic oscillation at the same frequency,the amplitude of the lift oscillation is 28.6% of the lift showing a lower drag oscillation.The present findings would contribute to the drag and vibration reduction of the double-track rocket sled.

关键词

双轨火箭橇/超声速流动/SAS/动网格/气动特性

Key words

double-track rocket sled/supersonic flow/SAS/dynamic mesh/aerodynamic characteristics

分类

航空航天

引用本文复制引用

王方元,林晓辉,余元元,董凌锋,郑达仁,许常悦..地面对双轨超声速火箭橇的气动特性影响研究[J].航空科学技术,2024,35(4):31-39,9.

基金项目

航空科学基金(20200029052001,20220029052002) Aeronautical Science Foundation of China(20200029052001,20220029052002)39 (20200029052001,20220029052002)

航空科学技术

1007-5453

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