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Combined effect of noise and vibration on passenger acceptanceAn extensive research program conducted at NASA Langley Research Center to develop a comprehensive model of passenger comfort response to combined noise and vibration environments has been completed. This model was developed for use in the prediction and/or assessment of vehicle ride quality and as a ride quality design tool. The model has the unique capability to transform individual elements of vehicle interior noise and vibration into subjective units and combining the subjective units to produce a total subjective discomfort index as well as the other useful subjective indices. This paper summarizes the basic approach used in the development of the NASA ride comfort model, presents some of the more fundamental results obtained, describes several application of the model to operational vehicles, and discusses a portable, self-contained ride quality meter system that is a direct hardware/software implementation of the NASA comfort algorithm.
Document ID
19840026090
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leatherwood, J. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Behavioral Sciences
Report/Patent Number
NAS 1.15:86284
NASA-TM-86284
Report Number: NAS 1.15:86284
Report Number: NASA-TM-86284
Meeting Information
Meeting: Meeting of the Acoustical Society of America
Location: Minneapolis, MN
Country: United States
Start Date: October 8, 1984
End Date: October 12, 1984
Accession Number
84N34161
Funding Number(s)
PROJECT: RTOP 141-20-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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