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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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 |
_version_ |
1721515353168674816 |