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阻力伞及气囊气动特性风洞试验技术研究
引用本文:杨贤文,廖翼兵,张德宇,刘伟,师建元,白本奇.阻力伞及气囊气动特性风洞试验技术研究[J].流体力学实验与测量,2007,21(4):49-52.
作者姓名:杨贤文  廖翼兵  张德宇  刘伟  师建元  白本奇
作者单位:[1]中国空气动力研究与发展中心,四川绵阳621000 [2]航宇救生装备有限公司,湖北襄樊441003 [3]中国航天科工集团第十七研究所,北京100038
基金项目:在本项试验技术研究中,与航字救生装备有限公司联合开展了开伞试验技术研究,与航天科工集团第十七研究所联合开展了气囊模型气动特性试验技术研究,对他们的支持表示感谢.
摘    要:对阻力伞、气囊等柔性减速器进行了风洞试验研究。采用高速摄像清晰地记录了阻力伞在M=1.0条件下的开伞过程、气囊在M=6.0条件下充气过程的外形变化,准确地测得了气囊在M=6.0条件下充气过程的阻力时间历程,且气囊充气过程外形变化的时间历程与阻力时间历程相符。此外,对阻力伞高速风洞试验的堵塞度影响进行了研究。结果表明,通过研究,为柔性减速器的气动特性测试建立了新的试验技术。

关 键 词:降落伞  气囊  风洞试验
文章编号:1672-9897(2007)04-0049-04
收稿时间:2007-01-24
修稿时间:2007-08-13

Wind-tunnel studies on the aerodynamics of drag parachutes and airbags
YANG Xian-wen, LIAO Yi-bing, ZHANG De-yu, LIU Wei, SHI Jian-yuan, BAI Ben-qi.Wind-tunnel studies on the aerodynamics of drag parachutes and airbags[J].Experiments and Measurements in Fluid Mechanics,2007,21(4):49-52.
Authors:YANG Xian-wen  LIAO Yi-bing  ZHANG De-yu  LIU Wei  SHI Jian-yuan  BAI Ben-qi
Abstract:Wind-tunnel experiments have been performed to study the aerodynamics of flexible decelerators such as drag parachutes and airbags. The deployment process of a drag parachute at M = 1.0 and the deformation of an airbag during the inflation at M = 6.0 were recorded using high-speed camera. The time history of the drag was shown to match the shape change of the airbag very well. The blockage effects of the drag parachute have been also studied. Test results show that new techniques developed in the present studies can be successfully used in studying the aerodynamics of flexible decelerators.
Keywords:drag parachute  airbag  wind tunnel test
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