NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of tactile vibration on annoyance to synthesized propfan noiseDesign information that maximizes passenger comfort for propfan aircraft is presented. Predicted noise and vibration environments and the resultant passenger acceptability were studied. The effect of high frequency tactile vibration (i.e., greater than 30 Hz) on passenger reactions was analyzed. Passenger reactions to a wide range of noise with and without tactile vibration was studied. The passenger ride quality simulator was employed using subjects who evaluated either synthesized propeller noises only, or these noises combined with seat/arm vibration. The noises ranging from 80-100 dB consisted of a turbulent boundary layer noise with a factorial combination of five blade passage frequencies (50-200 Hz), two harmonic rolloffs, and three tone/noise ratios. It is indicated that passenger reaction (annoyance) to noise is not significantly changed in the presence of tactile vibration.
Document ID
19820010992
Document Type
Conference Paper
Authors
Clevenson, S. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1981
Subject Category
BEHAVIORAL SCIENCES
Report/Patent Number
NASA-TM-83258
Meeting Information
Meeting of the Acoust. Soc. of Am.(Miami Beach, FL)
Funding Number(s)
PROJECT: RTOP 505-35-13-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

NameType 19820010992.pdf STI