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Aircraft pass-by noise on ground modelled with the SAFT-program

机译:使用SAFT程序建模的飞机地面噪声

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SAFT (Simulation of atmosphere and Air traffic For a quieter environmenT) is the name of a simulation tool for aircraft noise propagation that has been developed at CIT, Chalmers and KTH since the end of 2016. It is funded through CSA - Centre for Sustainable Aviation at KTH. Already in its current state SAFT enables aircraft pass-by noise estimations of several kinds. The set of computational approaches stretches from the most complex "full-simulation" ones, involving directivity, time-and frequency dependent individual (jet, fan, flaps,...) noise sources as well as sound propagation through a refractive atmosphere, down to the more old-fashioned "integrated" computational methods such as given in ECAC doc.29. Special attention has been paid to making the tool user-friendly and fast to run. Even in the case with a refractive atmosphere model SAFT runs at rather short CPU-times thanks to a new concept of a Transmission Loss interpolation matrix. The typical result from SAFT-runs is either a noise-contour map (LA_(max), SEL(A) or other metric) or the noise level time history in selected ground points (for simulation computations only). Other features involves possibilities to plot AdB-contours from "any possible" model-, parameter- or aircraft procedure variation. E.g. comparison of results such as from ECAC doc.29 vs "full-simulation", aircraft A vs aircraft B, weather condition X vs weather Y, different absorption models, different engine, airframe or procedure modifications etc. In a planned effort noise-source data in SAFT is to be extended with measured aircraft pass-by noise, time-correlated with FDR or/and trajectory data from the Opensky database.
机译:SAFT(模拟大气和空中交通以实现更安静的环境)是自2016年底以来由CIT,Chalmers和KTH开发的飞机噪声传播模拟工具的名称。该工具由CSA-可持续航空中心资助在KTH。在目前的状态下,SAFT已经可以估算几种飞机的通过噪声。计算方法集从最复杂的“完全模拟”方法扩展而来,涉及方向性,与时间和频率相关的个体(喷射,风扇,襟翼等)噪声源以及通过折射大气传播的声音,向下到更老式的“集成”计算方法,例如ECAC doc.29中给出的方法。已经特别注意使该工具易于使用和快速运行。由于采用了传输损耗插值矩阵这一新概念,即使在折射大气层模型的情况下,SAFT仍可以在很短的CPU时间上运行。 SAFT运行的典型结果是噪声轮廓图(LA_(max),SEL(A)或其他度量)或选定地面点的噪声水平时间历史记录(仅用于模拟计算)。其他功能包括从“任何可能的”模型,参数或飞机程序变化绘制AdB轮廓的可能性。例如。比较结果,例如ECAC doc.29与“完全模拟”,飞机A与飞机B,天气条件X与天气Y,不同的吸收模型,不同的发动机,机身或程序修改等结果。 SAFT中的数据将通过与FDR或/和Opensky数据库中的轨迹数据在时间上相关的实测飞机通过噪声进行扩展。

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