确定人体气动鼻阻力系数的理论模型和自然模型的可能性

Nosova Yana, Oleg Avrunin, Shushliapina Nataliia, Ibrahim Younouss Abdelhamid, Alofie Bander Ali Saleh
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引用次数: 0

摘要

本文对计算机头气动阻力系数的数学模型和全尺寸模型进行了比较分析。根据3D打印获得的全尺寸模型的实验测试结果,可以通过获得相应给定气流流速下的压降值总损失来计算气动前端阻力系数的值。在这种情况下,气动鼻阻力系数值之间的差异不超过15%,其原因是与计算鼻腔气动模型的方法有关的方法误差,特别是不可能考虑到所有局部干扰及其相互影响,以及实验测试中全尺寸模型的空气通道塑料表面的特性
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Possibilities Theoretical And Natural Models For Determining The Coefficient Of Human Aerodynamic Nose Resistance
This paper presents a comparative analysis of mathematical and full-scale models in determining the aerodynamic nose drag coefficient. According to the results of experimental tests of a full-scale model obtained by 3D printing, it is possible to calculate the value of the aerodynamic nose drag coefficient by obtaining the pressure drop values total losses for the corresponding given air flow rates. The discrepancy between the values of the aerodynamic nose drag coefficients in this case did not exceed 15% and is explained by methodological errors associated with the approaches in calculating the aerodynamic model of the nasal cavity, in particular, the impossibility of taking into account all local disturbances and their mutual influence, and the properties of the plastic surface of the air channels of the full-scale model during experimental tests
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