DOAJ Open Access 2021

Perceived discomfort for typical helicopter vertical sine vibrations for seated participants

Laurianne Delcor Etienne Parizet Julie Ganivet-Ouzeneau Julien Caillet

Abstrak

Vibrations contribute to helicopter’s ride comfort. This study aimed to determine the relationship between main rotor vertical excitations and discomfort. Fifty-three participants, seated on a helicopter seat fixed to a vibration test bench, evaluated the discomfort of vertical sinusoidal vibrations using a magnitude estimation procedure. Stimuli had a frequency between 15 and 30 Hz and a level between 0.32 and 3.16 m/s 2 . The average discomfort was shown related to vibration velocity using Steven’s power law, without any frequency dependence. The exponent depended on velocity and was 1.18 for higher velocities (approx. above 0.008 m/s) and 0.65 for velocities below that limit.

Topik & Kata Kunci

Control engineering systems. Automatic machinery (General) Acoustics. Sound

Penulis (4)

Laurianne Delcor

Etienne Parizet

Julie Ganivet-Ouzeneau

Julien Caillet

Format Sitasi

APA MLA BibTeX

Delcor, L., Parizet, E., Ganivet-Ouzeneau, J., Caillet, J. (2021). Perceived discomfort for typical helicopter vertical sine vibrations for seated participants. https://doi.org/10.1177/1461348420979759

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Informasi Jurnal

Tahun Terbit: 2021
Sumber Database: DOAJ
DOI: 10.1177/1461348420979759
Akses: Open Access ✓