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A Body-of-Revolution Implementation of the Parabolic Wave Equation With Application to Rocket Plume Attenuation Modeling

机译:抛物线方程的旋转体实现及其在火箭羽流衰减建模中的应用

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摘要

The parabolic wave equation has been used extensively to model long-range paraxial wave propagation due to its high computational efficiency. Typical radar, sonar, and communication geometries are most naturally treated using cylindrical coordinates with the radial direction chosen as the paraxial direction. Here, a method is described for modeling waves with 3-D variation propagating through an inhomogeneous body of revolution with the paraxial direction chosen to be the axis of symmetry. The technique decomposes the initial field into independent modes that are propagated in parallel using 2-D solvers. The method is benchmarked by comparison to finite-element calculations. An example application—modeling the interaction of a radio communications system with a rocket exhaust plume—is then considered.
机译:由于其高计算效率,抛物线波动方程已被广泛用于对远程近轴波传播进行建模。典型的雷达,声纳和通信几何形状最自然地使用圆柱坐标系处理,并且将径向方向选为近轴方向。在此,描述了一种方法,该方法用于建模通过非均质旋转体传播的3-D变化波,其中近轴方向被选为对称轴。该技术将初始场分解为独立的模式,这些模式使用2-D求解器并行传播。通过与有限元计算进行比较来确定该方法的基准。然后考虑一个示例应用程序-对无线电通信系统与火箭尾气羽流之间的相互作用进行建模。

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