scispace - formally typeset
Search or ask a question
Topic

Aircraft noise

About: Aircraft noise is a research topic. Over the lifetime, 3051 publications have been published within this topic receiving 32039 citations.


Papers
More filters
Journal ArticleDOI
TL;DR: In this paper, the authors found that fear of crashes, other forms of pollution, and proximity to the flight path are three such non-noise aspects which have spatial patterns that are closely related to the pattern of noise contours around an airport.

9 citations

Journal ArticleDOI
01 Jun 2013
TL;DR: In this article, a linear programming optimization formulation has been developed that implements a minimax performance criterion that aims to minimize the maximum cumulative noise load value occurring at any of the enforcement points.
Abstract: This article presents the development of a runway allocation planning tool that seeks to maximize the permissible number of flight operations into and out of an airport within a given annual noise budget. Although the model that underlies the planning tool is generic in nature, the tool has been customized for application to a specific airport, namely, Amsterdam airport Schiphol in the Netherlands. The noise budget regulations applicable at Schiphol stipulate limits on the annual cumulative noise loads at a large number of enforcement points arranged around the airport. To ensure an equitable distribution of the cumulative noise load at the enforcement points, an efficient allocation and distribution of the annual flight movements over available runways and routes is required that takes weather induced restrictions into account. To this end, a linear programming optimization formulation has been developed that implements a minimax performance criterion that aims to minimize the maximum cumulative noise load value occurring at any of the enforcement points. The numerical results obtained for the operational year 2005 clearly demonstrate the potential of the tool to maximize the yearly number of flight movements within the assigned noise budget.

9 citations

01 Jul 1977
TL;DR: The results of an evaluation of the effectiveness of current noise reduction technology in attaining acceptable levels of interior noise in a large (about 20,000 kg) passenger-carrying helicopter are presented in this paper.
Abstract: The results of an evaluation of the effectiveness of current noise reduction technology in attaining acceptable levels of interior noise in a large (about 20,000 kg) passenger-carrying helicopter are presented. The helicopter studied is a modified CH-53A with a specially designed, acoustically treated passenger cabin. The acoustic treatment reduced the average A-weighted interior noise levels from 115 db to 87 db. The study suggests selected improvements in the acoustic treatment which could result in additional reduction in cabin noise levels. The resulting levels would be only slightly greater than the interior noise levels of current narrow-body jet transports.

9 citations

01 Jan 1984
TL;DR: In this article, a flight and laboratory study of sidewall acoustic treatment for cabin noise control is described, where cabin noise levels were measured at six locations with three treatment configurations, and the insertion loss was defined as the reduction of interior noise associated with the addition of a treatment.
Abstract: A flight and laboratory study of sidewall acoustic treatment for cabin noise control is described. In flight, cabin noise levels were measured at six locations with three treatment configurations. Noise levels from narrow-band analysis are reduced to one-third octave format and used to calculate insertion loss, IL, defined as the reduction of interior noise associated with the addition of a treatment. Laboratory tests used a specially constructed structural panel modeled after the propeller plane section of the aircraft sidewall, and acoustic treatments representing those used in flight. Lab measured transmission loss and absorption values were combined using classical acoustic procedures to obtain a prediction of IL. Comparison with IL values measured in flight for the boundary layer component of the noise indicated general agreement.

9 citations

Journal ArticleDOI
TL;DR: In this paper, the authors describe a laboratory investigation into the concept of using a unified index for the prediction of annoyance from aircraft and traffic noise heard over periods of time, and find that at equal Leq levels traffic noise was reported to be significantly more difficult to live with than aircraft noise.

9 citations


Network Information
Related Topics (5)
Microphone
39.9K papers, 337.3K citations
75% related
Aerodynamics
33.3K papers, 460.4K citations
73% related
Wind tunnel
29.3K papers, 345.1K citations
72% related
Speech perception
12.3K papers, 545K citations
70% related
Speech processing
24.2K papers, 637K citations
66% related
Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202386
2022103
202152
202051
201980
201878