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Flight-Configuration-Based Analysis of Emissions and Noise Interdependencies
Chalmers Univ Technol, Fluid Dynam Div, Dept Mech & Maritime Sci, S-41296 Gothenburg, Sweden..
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0001-9902-6216
2025 (English)In: Journal of Aircraft, ISSN 0021-8669, E-ISSN 1533-3868, p. 1-13Article in journal (Refereed) Epub ahead of print
Abstract [en]

A unique series of flyover tests was conducted during the pandemic to study how variations commonly found in standard approach procedures primarily affect the noise level on the ground. The pandemic created unique conditions as the reduced air traffic provided the opportunity to perform these tests and collect noise measurements that are almost clear from background noise. The tests were performed with two A321neo aircraft one morning in April 2021 at Arlanda Airport, Stockholm. This work takes advantage of this database to develop an understanding of the influence of variations in configuration, speed, and altitude on the environmental impact. Interdependencies between noise, CO2, and non-CO2 emissions are closely studied, and the significant findings are presented and discussed. It is shown that, for early configurations, before landing gear deployment, there is a substantial tradeoff between CO2 and non-CO2 emissions, and careful consideration of the latter should be taken to avoid areas of critically low idle power. Noise in these configurations is mainly affected by the impact of the aircraft-microphone distance on the measurements. For the configurations that follow, CO2 emissions become more relevant as the fuel flow increases due to the increase in drag, which also results in an increased noise level that, in these configurations, shows a significant dependency on aircraft speed with an increase of 1 dB for every 10 knots. Based on these findings, some actions are proposed to minimize the impact of each configuration.

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics (AIAA) , 2025. p. 1-13
Keywords [en]
Aircraft Components and Structure, Indicated Airspeed, Energy Economics, Flight Data Recorder, International Civil Aviation Organization, Aerospace Manufacturers, Aircraft Navigation Systems, Sound Pressure Level, Acoustic Properties, Aircraft Stability and Control
National Category
Vehicle and Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-360774DOI: 10.2514/1.C037531ISI: 001424960800003OAI: oai:DiVA.org:kth-360774DiVA, id: diva2:1941860
Note

QC 20250303

Available from: 2025-03-03 Created: 2025-03-03 Last updated: 2025-03-03Bibliographically approved

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Johansson, AndersOtero, Evelyn

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