Options for aircraft noise reduction on arrival and landing

被引:12
|
作者
Filippone, Antonio [1 ]
机构
[1] Univ Manchester, Sch MACE, George Begg Bldg, Manchester M13 9PL, Lancs, England
关键词
OUTDOOR SOUND-PROPAGATION; DESIGN; MODEL;
D O I
10.1016/j.ast.2016.10.027
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper demonstrates the noise reduction potential from modified final approach and landing procedures of commercial aircraft. A conventional trajectory is compared with a steep approach with a 4.5-degree glide slope (first option), and with a displaced landing, wherein an aircraft approaching with a 3-degree slope is allowed to land with a second threshold (second option). The reference airplane is the Airbus A320-211. Examples of noise footprints are shown for generic cases of constant ground impedance. It is shown that a noise reduction of -1 EPNL reduction is possible with a 450 m landing displacement or with a 3.5 degree glide slope. Noise reduction occurs below the flight track and moderate lateral distances. It is also shown that at larger lateral distances, 200 m or above, the noise level increases compared to the reference case. The ground model has been extended to include variable impedance and actual airfields. Finally, it is shown that an Ernbraer E195 model landing on a steep trajectory has a reduced noise almost everywhere in a selected region around the airfield. (C) 2016 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:31 / 38
页数:8
相关论文
共 50 条
  • [21] Air curtains for landing gear noise reduction
    Carroll, Daniel
    Pott-Polenske, Michael
    Bennett, Gareth J.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2025, 161
  • [22] AIRCRAFT ENGINE NOISE REDUCTION.
    Conf
    NASA Special Publications, 1972, (31):
  • [23] The measurement of aircraft noise reduction in residences
    Sharp, BH
    Martin, S
    INTER-NOISE 96 - THE 1996 INTERNATIONAL CONGRESS ON NOISE CONTROL ENGINEERING, 25TH ANNIVERSARY CONGRESS - LIVERPOOL, PROCEEDINGS, BOOKS 1-6: NOISE CONTROL - THE NEXT 25 YEARS, 1996, : 2747 - 2752
  • [24] Gomolzig provides noise reduction options
    Bokulich, F
    AEROSPACE ENGINEERING, 2002, 22 (04) : 11 - 11
  • [25] METHODOLOGY FOR MULTI-AIRCRAFT MINIMUM NOISE IMPACT LANDING TRAJECTORIES
    COOK, G
    JACOBSON, ID
    CHANG, R
    MELTON, R
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1982, 18 (01) : 131 - 146
  • [26] Assessment of Noise Variability of Landing Aircraft Using Phased Microphone Array
    Snellen, Mirjam
    Merino-Martinez, Roberto
    Simons, Dick G.
    JOURNAL OF AIRCRAFT, 2017, 54 (06): : 2173 - 2183
  • [28] Control strategies for aircraft airframe noise reduction
    Li Yong
    Wang Xunnian
    Zhang Dejiu
    CHINESE JOURNAL OF AERONAUTICS, 2013, 26 (02) : 249 - 260
  • [29] A coordinated approach for aircraft and engine noise reduction
    Collin, D
    NOUVELLE REVUE AERONAUTIQUE ASTRONAUTIQUE, 1998, (02): : 133 - 135
  • [30] Airframe noise sources and reduction technologies in aircraft
    Azimi, M. (m_r_azimi1991@yahoo.com), 2012, Multi-Science Publishing Co. Ltd (43):