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弹道与气动力技术

立式风洞在末敏弹研制中的应用研究

  • 高宏超 ,
  • 赵养正 ,
  • 方养田
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  • 中国兵器工业第203研究所,西安 710065

高宏超(1966-),男,陕西渭南人,研究员,研究方向:火箭总体。

收稿日期: 2013-03-12

  网络出版日期: 2025-05-26

Application of Vertical Wind Tunnel in Developing Sensor Fused Munitions

  • GAO Hongchao ,
  • ZHAO Yangzheng ,
  • FANG Yangtian
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  • No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2013-03-12

  Online published: 2025-05-26

摘要

介绍在立式风洞中弹箭兵器伞弹模型动态参数测量的实验方法、图像采集与处理,并采用该视频测量技术测量了两种不同的伞弹模型的扫描角和转速。实验结果显示:该实验系统测试伞弹系统的动态状态参数与外场试验基本一致,可在一定程度上满足伞弹系统实验要求;另外如果转速曲线具有较稳定的周期性变化,伞弹系统就会出现较好的运转稳定性。

本文引用格式

高宏超 , 赵养正 , 方养田 . 立式风洞在末敏弹研制中的应用研究[J]. 弹箭与制导学报, 2013 , 33(5) : 138 -140 . DOI: 10.15892/j.cnki.djzdxb.2013.05.040

Abstract

This paper focuses onexperiment method, image collection and processing for measuring dynamic parameters of model of sensor fused munitions with parachute in vertical wind tunnel. The video measurement technology was used to measure scanning angle and spin rate of two different sensor fused munitions. The measurement result shows that the measured dynamic parameters of model of sensor fused munitions are identical with that achieved in field test. In certain degree, the method can satisfy the scanning angle and spin rate test requirements of sensor fused munitions. In addition, if the spin curve possesses a stable periodic change, the sensor fused munitions with parachute will possess better spin stability.

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