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Non-Spherical Particle Trajectory Modelling for Ice Crystal Conditions

机译:冰晶条件的非球形粒子轨迹建模

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Aircraft icing is a significant issue for aviation safety. In this paper, recent developments for calculating the trajectory of non-spherical particles are used to determine the trajectory and impingement of ice crystals in aircraft icing scenarios. Two models are used, each formulated from direct numerical simulations, to give the drag, lift and torque correlations for various shaped particles. Previously, within the range of Reynolds number permitted in this study, it was only possible to model the trajectory and full rotational progression of cylindrical particles. The work presented in this paper allows for analysis of a wider range of ice shapes that are commonly seen in icing conditions, capturing the dynamics and behaviours specific to ice crystals. Previous limitations relate to the in ability to account for particle rotation and the dependency of force correlations on the measure of particle sphericity - which are now overcome. The method also provides an opportunity for new analysis - the creation of catch bounds for mixed clouds of particles. The above models are applied to two geometries and compared with drag only cases for spheres and non-spherical particles as parameterized by sphericity. The analysis shows that taking the worst- and best-case scenarios provide a range of values for the catch, which can help to understand better the extent over which particles impinge. Hence a catch-limit for a mixed cloud of particles of different shaped particles and different sized particles may be easily gained. The methods are also able to capture rotations and trajectories in three dimensions. Incorporating new methods for modelling the trajectory, rotation and orientation of non-spherical particles into the modelling of aircraft icing opens new avenues for industrial analysis. In turn this may aide several areas of aircraft design related to engine design and flight instrumentation system design as well as informing the aircraft certification process.
机译:飞机结冰是航空安全的重要问题。在本文中,用于计算非球形颗粒轨迹的最新发展用于确定飞机结冰场景中冰晶的轨迹和冲击。使用两种型号,每个模型从直接数值模拟配制,以给出各种形状颗粒的拖曳,提升和扭矩相关性。以前,在本研究允许的雷诺数范围内,只有可以模拟圆柱形颗粒的轨迹和全旋转进展。在本文提出的工作允许更广泛的冰的形状,其通常见于结冰条件下,捕获动力学和行为特定于冰晶的分析。以前的限制涉及考虑粒子旋转的能力和力相关对粒子球体测量的依赖性 - 现在克服。该方法还为新分析提供了机会 - 为混合颗粒云创建捕获界。上述模型应用于两个几何形状,并与仅由球形参数化的球体和非球形颗粒的拖曳件相比。分析表明,采用最差和最佳情况的情况为捕获提供了一系列值,这有助于更好地了解粒子撞击的程度。因此,可以容易地获得不同形状颗粒和不同尺寸颗粒的颗粒的混合云的捕获限制。该方法还能够在三维中捕获旋转和轨迹。掺入用于对非球面颗粒的轨迹,旋转和定向建模的新方法,进入飞机结冰的建模开启了新的工业分析途径。反过来,这可能是与发动机设计和飞行仪表系统设计相关的飞机设计的几个领域,并通知飞机认证过程。

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