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中文核心期刊

高速多体分离风洞实验研究进展

PROGRESS IN EXPERIMENTAL RESEARCH ON HIGH-SPEED MULTI-BODY SEPARATION IN WIND TUNNEL

  • 摘要: 高速多体分离力学问题是航空航天领域中的核心基础问题, 它涉及到在超声速/高超声速条件下多个物体分离的多物理强相互作用过程, 如高速多体飞行器级间分离、抛撒分离, 空间碎片/陨石(群)进入大气层等. 高速多体分离研究区别于单体绕流问题, 高速流动产生的激波、压缩/膨胀波、分离涡等流体力学现象与分离体产生动态耦合, 这种复杂非定常动力学过程是多体分离研究的核心挑战之一. 理论预测与数值模拟面对高动态、强耦合的高速非定常多体分离过程存在一定的局限性, 因此准确、可靠的地面实验模拟尤为重要. 本文系统回顾了高速多体分离相关的实验技术与应用研究, 主要包括静态实验、准定常实验、动态分离实验技术与测量方法等; 梳理总结了高速多体分离中复杂流动物理现象与机制; 此外, 深入剖析了当前高速多体分离实验技术的局限性和挑战性, 并对多体分离实验技术的未来发展方向进行了展望. 高速多体分离风洞实验的核心挑战在于多体之间的非线性气动干扰、非定常流动与高动态运动的强耦合问题, 风洞实验模拟亟需解决的关键技术包括毫秒级的动态实验测量、多体姿轨精确模拟与气动载荷高精度预测等. 本文期望对多体分离风洞实验基础研究提供一些有意义的启示, 推动我国空天高速多体飞行器装备发展.

     

    Abstract: The high-speed multi-body separation mechanics problem is a core fundamental issue in the aerospace field. It involves the multi-physical strong interaction processes of multi-body separating under supersonic/hypersonic conditions, such as high-speed multi-body vehicles stage separation, dispersal separation, and the entry of space debris/meteorites (groups) into the atmosphere. The research on high-speed multi-body separation differs from the flow-around issues of single-body. The fluid mechanics phenomena generated by high-speed flow, such as shock waves, compression/expansion waves, and separated vortices, dynamically couple with the separated bodies. This complex unsteady dynamic process is one of the core challenges in the study of multi-body separation. Theoretical predictions and numerical simulations face certain limitations in dealing with highly dynamic, strongly coupled high-speed unsteady multi-body separation processes, making accurate and reliable ground experimental simulations particularly important. This paper provides a systematic review of the wind tunnel experimental techniques and application research on high-speed multi-body separation problems, mainly including static experiments, quasi-steady experiments, and dynamic separation experimental techniques and measurement methods. Secondly, it summarizes the complex flow phenomena and physics of experiments on high-speed multi-body separation. Furthermore, it systematically analyzes the limitations and challenges of current high-speed multi-body separation experimental techniques and outlines the future development direction of multi-body separation experiments. The core scientific issue in high-speed multi-body separation wind tunnel experiments lies in the nonlinear aerodynamic interference, unsteady flow, and motion coupling among multiple bodies. The key technologies that urgently need to be addressed in wind tunnel experimental simulation include millisecond-level dynamic experimental technology, precise simulation of multi-body poses, and aerodynamic load prediction, etc. It is expected to provide some meaningful insights into the basic experimental research of multi-body separation and promote the development of China's aerospace high-speed multi-body vehicle equipment.

     

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