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中国沙漠 ›› 2024, Vol. 44 ›› Issue (5): 254-260.DOI: 10.7522/j.issn.1000-694X.2024.00122

• • 上一篇    下一篇

基于原位风沙流观测的广冲击角的溅射函数构建

蒋缠文1,2(), 董治宝2, 罗万银3, 钱广强3, 张正偲2, 逯军峰3, 王晓艳1   

  1. 1.渭南师范学院 环境与生命科学学院/陕西省河流湿地生态与环境重点实验室,陕西 渭南 714000
    2.陕西师范大学 地理科学与旅游学院,陕西 西安 710119
    3.中国科学院西北生态环境资源研究院,甘肃 兰州 730000
  • 收稿日期:2024-08-12 修回日期:2024-09-12 出版日期:2024-09-20 发布日期:2024-10-15
  • 作者简介:蒋缠文(1984—),男,宁夏盐池人,副教授,研究方向为风沙物理学。E-mail: jiangchanwen@126.com
  • 基金资助:
    国家自然科学基金项目(41901012);中国博士后科学基金项目(2019M663615);中国科学院沙漠与沙漠化重点实验室开放课题(KLDD-2021-005);陕西省教育厅重点实验室项目(22JS017)

Constructing splash functions with a wide impact angle based on in-situ observation of aeolian sand flow

Chanwen Jiang1,2(), Zhibao Dong2, Wanyin Luo3, Guangqiang Qian3, Zhengcai Zhang2, Junfeng Lu3, Xiaoyan Wang1   

  1. 1.College of Environment and Life Sciences / Shaanxi Key Laboratory of River Wetland Ecology and Environment,Weinan Normal University,Weinan 714000,Shaanxi,China
    2.College of Geography and Tourism,Shaanxi Normal University,Xi'an 710119,China
    3.Northwest Institute of Eco-Environment and Resources,Chinese Academy of Sciences,Lanzhou 730000,China
  • Received:2024-08-12 Revised:2024-09-12 Online:2024-09-20 Published:2024-10-15

摘要:

风沙流中沙粒与床面的相互作用机理是风沙物理学研究的关键问题。由于沙粒运动的复杂性,数值模拟的研究结果通常与实际情况存在较大差异,因此,以实验手段得到的击溅函数对于理解粒-床碰撞的物理过程具有重要意义。基于饱和风沙流内气流对碰撞过程的影响可以忽略不计的共识,学者们通过大量的无风碰撞实验进行击溅函数研究。然而,由于测量技术的限制,典型冲击角度(10°)下的粒-床碰撞过程的实测数据很少。鉴于数值模拟和无风碰撞实验都表明击溅函数对冲击角度较为敏感,基于高速摄影技术在风洞内获得了松散沙床表面大量冲击角在10°左右的粒-床碰撞过程,并结合前人沙粒离心发射器(冲击角20°~50°)的实验结果,构建了涵盖广泛冲击角度的溅射函数,这些函数能够适用于前人不同实验条件的风洞实验结果,这对未来的风沙物理学研究具有重要意义。

关键词: 击溅函数, 跃移运动, 风洞实验, 粒-床碰撞过程, 高速摄影技术

Abstract:

The interaction mechanism between sand particles and the bed surface in aeolian sand flow constitutes a key issue in aeolian physics research. Owing to the complexity of sand particle movement, the research results from numerical simulation typically deviate significantly from the actual situation. Consequently, the splash functions obtained through experimental means holds great significance for understanding the physical process of particle-bed collision. Based on the consensus that the influence of airflow in saturated aeolian sand flow on the collision process can be neglected, scholars conduct splash functions research by means of a large number of windless collision experiments. However, due to limitations in measurement technology, there are scarce measured data of the particle-bed collision process under the typical impact angle of 10°. Considering that both numerical simulation and windless collision experiments indicate that the splash functions are sensitive to the impact angle, a large number of particle-bed collision processes with an impact angle around 10° on the surface of a loose sand bed are obtained in a wind tunnel by utilizing high-speed photography technology. Combined with the experimental results of predecessors' sand grain centrifugal launcher (with an impact angle ranging from 20° to 50°), the splash functions covering a wide range of impact angles are constructed. These functions can be applied to the wind tunnel experiment results of predecessors under different experimental conditions, which is of great significance for future research in aeolian physics.

Key words: splash functions, saltation movement, wind tunnel experiment, particle-bed collision process, high-speed photography technology

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