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Effect of aircraft noise on children’s cognitive performance
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
(English)In: Journal of Environmental Psychology, ISSN 0272-4944, E-ISSN 1522-9610Article in journal (Other academic) Submitted
National Category
Fluid Mechanics and Acoustics
URN: urn:nbn:se:kth:diva-7553OAI: diva2:12614
QS 20120326Available from: 2007-10-22 Created: 2007-10-22 Last updated: 2012-03-26Bibliographically approved
In thesis
1. A few aspects of aircraft noise
Open this publication in new window or tab >>A few aspects of aircraft noise
2007 (English)Licentiate thesis, comprehensive summary (Other scientific)
Abstract [en]

A few aspects of aircraft noise were evaluated. These were (i) methods of subjective evaluations, (ii) effects of equalization and (iii) the effects of cognitive aspects.

In the first paper, sorting algorithms were used instead of conventional paired comparison method in order to reduce the number of pairs in the evaluation of subjective judgments. The quick sorting algorithm method revealed more than 99% correlation coefficient with paired comparison method although the method used N*log(N) evaluations instead of N(N-1)/2.

In the second paper, equalization effects on perception were evaluated in two steps, first with stationary aircraft sounds and second with non-stationary aircraft sounds.

The first experiment examined the effects of stationary sound segments respect to three different angle positions of the aircrafts relative to the observer (78.7°, 90° & 101.3°), two different SNR conditions (sounds having original broadband plus tonal components versus control broadband sounds having no tonal components) and two different flight conditions (arrival and take-off). Subjects were asked to scale five perceptual attributes (loudness, annoyance, hardness, power and pitch) using Borg CR100 scale. The angle condition showed highly significant effects on annoyance and hardness. Maximal effects were found at an angle of 78.7°. The SNR revealed a significant impact on loudness, power and pitch.

The second experiment analyzed the effects of tonal components and the problem of appropriate equalization. The spectrum of the signals was modified in two steps (buzz-saw, isolated BPF tone). Further EPNL-equalization, A-, B-, C-, D- and spectral broadband equalizations were applied to the synthesized sounds. Annoyance, loudness, hardness and pitch in the isolated tone conditions showed significantly stronger effects than the buzz-conditions on the perceived judgments. The EPNL-equalization led to a lower degree of differentiation between the spectral conditions compared to B- and C-level equalization.

In the third paper, the effects of aircraft sounds on children’s cognitive performance were investigated. Impact of aircraft noise on children cognition was found significantly higher in reading comprehensions than in basic mathematics and problem solving tests. It seems children are very sensitive to the modifications in the aircraft noise but further studies are necessary to compliment such a finding.

Place, publisher, year, edition, pages
Stockholm: Farkost och flyg, 2007
Trita-AVE, ISSN 1651-7660 ; 2007:62
paired comparison, sorting based paired comparison, sorting algorithms, mergesort, quicksort, aircraft sound synthesis, aircraft noise, sound quality, tonal effects, angle positions, flight conditions, methods of equalization, cognition
National Category
Fluid Mechanics and Acoustics
urn:nbn:se:kth:diva-4510 (URN)
2007-11-01, S40, MWL, Teknikringen 8, Stockholm, 13:00
Available from: 2007-10-22 Created: 2007-10-22

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