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The development of a new model to simulate the dispersion of rocket exhaust clouds

机译:模拟火箭尾气弥散的新模型的开发

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摘要

This study presents the development of a new model named MSRED, which was designed to simulate the formation, rise, expansion, stabilisation and dispersion of rocket exhaust clouds for short-range assessment, using a three-dimensional semi-analytical solution of the advection-diffusion equation based on the ADMM method. For long-range modelling, the MSRED was built to generate a ready-to-use initial conditions file to be input to the CMAQ model, as it represents the state-of-the-art in regional and chemical transport air quality modelling. Simulations and analysis were carried out in order to evaluate the application of this integrated modelling system for different rocket launch cases and atmospheric conditions, for the Alcantara Launching Center (ALC, the Brazilian gate to the space) region. This hybrid, modern and multidisciplinary system is the basis of a modelling framework that will be employed at ALC for pre- and post-launching simulations of the environmental effects of rocket operations. (C) 2017 Elsevier Masson SAS. All rights reserved.
机译:这项研究提出了一种名为MSRED的新模型,该模型旨在使用对流的三维半解析解来模拟火箭废气云的形成,上升,扩展,稳定和弥散,以便进行短程评估。基于ADMM方法的扩散方程。对于远程建模,建立了MSRED以生成可随时使用的初始条件文件,以将其输入到CMAQ模型,因为它代表了区域和化学运输空气质量建模的最新技术。为了评估该集成建模系统在不同的火箭发射情况和大气条件下在阿尔坎塔拉发射中心(ALC,巴西通往太空的大门)区域的应用,进行了仿真和分析。这种混合,现代和多学科的系统是建模框架的基础,该模型框架将在ALC上用于火箭运行环境影响的发射前和发射后模拟。 (C)2017 Elsevier Masson SAS。版权所有。

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