Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation

Aircraft performance and noise database together with operational weights (depending on flight distances) and operational procedures (including low noise procedures) significantly influence results of noise exposure contour maps assessment in conditions of real atmosphere. Current recommendations of...

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Bibliographic Details
Main Authors: Oleksandr Zaporozhets, Larisa Levchenko
Format: Article
Language:English
Published: MDPI AG 2021-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/8/5/121
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spelling doaj-73442353545a477197719945ec21d0932021-04-21T23:06:01ZengMDPI AGAerospace2226-43102021-04-01812112110.3390/aerospace8050121Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event CalculationOleksandr Zaporozhets0Larisa Levchenko1Scientific-Research Department, National Aviation University, 03058 Kyiv, UkraineDepartment of Automation of Designing of Energy Processes and Systems, National Technical University “KPI”, 03056 Kyiv, UkraineAircraft performance and noise database together with operational weights (depending on flight distances) and operational procedures (including low noise procedures) significantly influence results of noise exposure contour maps assessment in conditions of real atmosphere. Current recommendations of the Standard SAE-AIR1845A allow the definition of flight profiles via solutions of balanced motion equations. However, differences are still supervised between the measured sound level data and calculated ones, especially in assessing the single flight noise events. Some of them are well explained by differences between balanced flight parameters (thrust and velocity first of all) and monitored ones by the traffic control system. Statistical data were gathered to make more general view on these differences and some proposal to use them in calculations has been proven. Besides, the real meteorological parameters provide inhomogeneous atmosphere conditions always, which are quite different from the main assumptions of the SAE-AIR1845A, stipulating inaccuracies of sound level calculations.https://www.mdpi.com/2226-4310/8/5/121aircraftnoiseperformancesingle eventsound levelcalculation model
collection DOAJ
language English
format Article
sources DOAJ
author Oleksandr Zaporozhets
Larisa Levchenko
spellingShingle Oleksandr Zaporozhets
Larisa Levchenko
Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
Aerospace
aircraft
noise
performance
single event
sound level
calculation model
author_facet Oleksandr Zaporozhets
Larisa Levchenko
author_sort Oleksandr Zaporozhets
title Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
title_short Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
title_full Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
title_fullStr Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
title_full_unstemmed Accuracy of Noise-Power-Distance Definition on Results of Single Aircraft Noise Event Calculation
title_sort accuracy of noise-power-distance definition on results of single aircraft noise event calculation
publisher MDPI AG
series Aerospace
issn 2226-4310
publishDate 2021-04-01
description Aircraft performance and noise database together with operational weights (depending on flight distances) and operational procedures (including low noise procedures) significantly influence results of noise exposure contour maps assessment in conditions of real atmosphere. Current recommendations of the Standard SAE-AIR1845A allow the definition of flight profiles via solutions of balanced motion equations. However, differences are still supervised between the measured sound level data and calculated ones, especially in assessing the single flight noise events. Some of them are well explained by differences between balanced flight parameters (thrust and velocity first of all) and monitored ones by the traffic control system. Statistical data were gathered to make more general view on these differences and some proposal to use them in calculations has been proven. Besides, the real meteorological parameters provide inhomogeneous atmosphere conditions always, which are quite different from the main assumptions of the SAE-AIR1845A, stipulating inaccuracies of sound level calculations.
topic aircraft
noise
performance
single event
sound level
calculation model
url https://www.mdpi.com/2226-4310/8/5/121
work_keys_str_mv AT oleksandrzaporozhets accuracyofnoisepowerdistancedefinitiononresultsofsingleaircraftnoiseeventcalculation
AT larisalevchenko accuracyofnoisepowerdistancedefinitiononresultsofsingleaircraftnoiseeventcalculation
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