Approximate Closed-Form Solution of the Differential Equation Describing Droplet Flight during Sprinkler Irrigation

IF 2.1 Q2 ENGINEERING, MULTIDISCIPLINARY Inventions Pub Date : 2024-07-10 DOI:10.3390/inventions9040073
Dario Friso
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Abstract

Sprinkler irrigation is widely used in agriculture because it allows for rational use of water. However, it can induce negative effects of soil erosion and of surface waterproofing. The scholars of these phenomena use the numerical integration of the equation of motion, but if there was an analytical solution, the study would be facilitated, and this solution could be used as software for regulating sprinklers. Therefore, in this study, the solution of the differential equation of the flight of droplets produced by sprinklers in the absence of wind was developed. The impossibility of an exact analytical solution to the ballistic problem due to the variability of the drag coefficient of the droplets is known; therefore, to find the integrals in closed form, the following were adopted: a new formula for the drag coefficient; a projection of the dynamic’s equation onto two local axes, one tangent and one normal to the trajectory and some linearization. To reduce the errors caused by the latter, the linearization coefficients and their calculation formulas were introduced through multiple non-linear regressions with respect to the jet angle and the initial droplet speed. The analytical modeling obtained, valid for jet angles from 10° to 40°, was compared to the exact numerical solution, showing, for the total travel distance, a high accuracy with a mean relative error MRE of 1.8% ± 1.4%. Even the comparison with the experimental data showed high accuracy with an MRE of 2.5% ±1.1%. These results make the analytical modeling capable of reliably calculating the travel distance, the flight time, the maximum trajectory height, the final fall angle and the ground impact speed. Since the proposed analytical modeling uses only elementary functions, it can be implemented in PLC programmable logic controllers, which could be useful for controlling water waste and erosive effects on the soil during sprinkler irrigation.
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描述喷灌过程中水滴飞行的微分方程的近似闭式解法
喷灌在农业中得到广泛应用,因为它可以合理用水。然而,它也会引起土壤侵蚀和地表防水的负面影响。研究这些现象的学者使用的是运动方程的数值积分,但如果有一个解析解,就会方便研究,而且这个解可以用作调节喷灌机的软件。因此,本研究开发了无风情况下洒水器产生的水滴飞行微分方程的解法。众所周知,由于液滴阻力系数的变化,不可能对弹道问题进行精确的分析求解;因此,为了找到封闭形式的积分,采用了以下方法:阻力系数的新公式;将动态方程投影到两个局部轴上,一个与轨迹相切,一个与轨迹法线相切,以及一些线性化方法。为了减少后者造成的误差,通过对射流角度和液滴初始速度进行多次非线性回归,引入了线性化系数及其计算公式。所获得的分析模型适用于 10° 至 40° 的喷射角,并与精确的数值解决方案进行了比较,结果表明,在总行程方面,分析模型具有很高的准确性,平均相对误差 MRE 为 1.8% ± 1.4%。与实验数据的比较也显示出较高的精度,平均相对误差为 2.5% ±1.1%。这些结果使得分析模型能够可靠地计算飞行距离、飞行时间、最大轨迹高度、最终下落角度和地面冲击速度。由于所提出的分析模型只使用了基本函数,因此可以在 PLC 可编程逻辑控制器中实现,从而有助于控制喷灌过程中的水资源浪费和对土壤的侵蚀作用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Inventions
Inventions Engineering-Engineering (all)
CiteScore
4.80
自引率
11.80%
发文量
91
审稿时长
12 weeks
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