Evaluation of environmentally optimal descent and take-off slopes for existing and novel aircraft
Evaluation of environmentally optimal descent and take-off slopes for existing and novel aircraft
Descent and takeoff slopes of civil aircraft influence the associated noise and emissions impact around airports. Steep take-off and approach procedures are expected to reduce the noise footprint around airports whereas they could offer local air quality benefits as well. This paper appraises the optimal descent and take-off slopes in terms of noise and emissions for existing civil aircraft, as well as fora future blended wing-body (BWB) concept aircraft. The effect of the interdependencies between noise and emissions is demonstrated, whereas estimated Noise-Power-Distance (NPD) curves for the steep operations are presented. It is shown that a common optimum slope for both environmental concerns is unlikely to occur and that generally, noise benefits come to the expense of increased fuel consumption. However, it is also highlighted that new, more flexible ways of expressing the noise and emissions interdependencies may be required in order to determine optimum slopes more realistically.
European Acoustics Association, EAA
Synodinos, Athanasios
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Self, Rodney
8b96166d-fc06-48e7-8c76-ebb3874b0ef7
Torija Martinez, Antonio
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May 2018
Synodinos, Athanasios
fc4f6dd2-7200-48b4-b0bf-67a2f62dda3b
Self, Rodney
8b96166d-fc06-48e7-8c76-ebb3874b0ef7
Torija Martinez, Antonio
6dd0d982-fcd6-42b6-9148-211175fd3287
Synodinos, Athanasios, Self, Rodney and Torija Martinez, Antonio
(2018)
Evaluation of environmentally optimal descent and take-off slopes for existing and novel aircraft.
In The Euronoise 2018 Proceedings.
European Acoustics Association, EAA..
Record type:
Conference or Workshop Item
(Paper)
Abstract
Descent and takeoff slopes of civil aircraft influence the associated noise and emissions impact around airports. Steep take-off and approach procedures are expected to reduce the noise footprint around airports whereas they could offer local air quality benefits as well. This paper appraises the optimal descent and take-off slopes in terms of noise and emissions for existing civil aircraft, as well as fora future blended wing-body (BWB) concept aircraft. The effect of the interdependencies between noise and emissions is demonstrated, whereas estimated Noise-Power-Distance (NPD) curves for the steep operations are presented. It is shown that a common optimum slope for both environmental concerns is unlikely to occur and that generally, noise benefits come to the expense of increased fuel consumption. However, it is also highlighted that new, more flexible ways of expressing the noise and emissions interdependencies may be required in order to determine optimum slopes more realistically.
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Euronoise 2018
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Published date: May 2018
Venue - Dates:
11th European Congress and Exposition on Noise Control Engineering, , Crete, Greece, 2018-05-27 - 2018-05-31
Identifiers
Local EPrints ID: 421643
URI: http://eprints.soton.ac.uk/id/eprint/421643
PURE UUID: 4033b5d8-ba13-4ad9-8d40-20bc08fdc8bb
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Date deposited: 19 Jun 2018 16:30
Last modified: 30 Jul 2024 17:04
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Contributors
Author:
Athanasios Synodinos
Author:
Antonio Torija Martinez
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