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非规则砂尘颗粒三分量气动力特性试验方法OA

Experimental Method for Three-Component Aerodynamic Characteristics of Irregular Sand Particles

中文摘要英文摘要

近年来,惯性粒子分离器内砂尘颗粒的运动特性备受关注,颗粒气动力特性是理解其运动规律的基础.常见的沉降试验在姿态控制、测量维度与雷诺数调控方面存在系统性局限,难以满足非规则颗粒三分量力的测量需求.为此,基于典型砂尘颗粒抽象模型,采用六分量天平测量阻力、升力与侧向力.通过调节颗粒模型安装姿态设定来流角,结合磁驱滑块系统驱动模型在静置甘油-水溶液中匀速运动,模拟等效来流,开展多组三分量力测量试验.结果表明,阻力系数主要受雷诺数与球形度影响:随雷诺数增加,阻力系数持续下降;在相同雷诺数下,低球形度颗粒阻力显著高于高球形度颗粒,且差异在高雷诺数区更为明显.来流角的影响表现出明显的形状依赖性,低球形度颗粒对角度变化更为敏感.相同角度条件下,侧滑角引发更强的三维绕流结构,其对阻力与侧向力的增强效应明显强于攻角.最后,基于试验数据拟合了同时考虑雷诺数、球形度与来流角的阻力系数函数关系式,为多变量建模提供数据基础与方法支持.

In recent years,the motion characteristics of sand particles within inertial particle separators have received widespread attention.The aerodynamic properties of particles serve as the basis for understanding their migration behav-ior.Conventional settling experiments,commonly employed in studies of particle aerodynamic characteristics,exhibit inherent limitations in orientation control,force measurement dimensionality,and Reynolds number regulation,render-ing them inadequate for precise characterization of the three-component aerodynamic forces acting on irregular sand par-ticles.To overcome these constraints,this study employs a set of representative abstract models of irregular sand par-ticles and conducts direct force measurements using a six-component balance to capture drag,lift,and sideway forces.A magnetically driven slider system is utilized to propel the force measurement system and particle models through a qui-escent glycerol-water solution at constant velocity,thereby simulating an equivalent uniform inflow.A series of three-component force measurement experiments are conducted under varying equivalent inflow conditions to obtain the hy-drodynamic forces acting on particles in liquid.The results indicate that the drag coefficient is primarily influenced by both the Reynolds number and the sphericity.Specifically,the drag coefficient decreases consistently with increasing Reynolds number;at a fixed Reynolds number,particles with lower sphericity exhibit significantly higher drag coeffi-cients than those with higher sphericity,with this difference becoming more significant in the high-Reynolds-number re-gime.The influence of inflow angle on aerodynamic forces exhibits a notable dependence on particle shape.Particles with lower sphericity exhibit greater variations in drag coefficient with changes in inflow angle,revealing a more no-table aerodynamic dependence on angular variation.Under identical angular conditions,sideslip angle produces a stron-ger enhancement in both drag and sideway force than angle of attack.Finally,a drag coefficient correlation is developed based on the experimental data,incorporating Reynolds number,sphericity,angle of attack,and sideslip angle,provid-ing fundamental data and methodological support for multi-variable drag modeling.

刘祥琪;谭慧俊;张悦;孙姝;何小明;郑高杰

南京航空航天大学能源与动力学院,江苏 南京 210016南京航空航天大学能源与动力学院,江苏 南京 210016南京航空航天大学能源与动力学院,江苏 南京 210016南京航空航天大学民航学院,江苏 南京 210016南京航空航天大学能源与动力学院,江苏 南京 210016南京航空航天大学能源与动力学院,江苏 南京 210016

航空航天

砂尘颗粒非规则气动力特性六分量天平雷诺数球形度攻角侧滑角

sand particlesirregularaerodynamic characteristicssix-component balanceReynolds numbersphericityangle of attacksideslip angle

《海军航空大学学报》 2026 (3)

495-507,13

两机项目:国家重大科技专项(J2019-Ⅱ-0014-0035)

10.7682/j.issn.2097-1427.2026.03.008

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