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Tests and analyses applicable to passenger ride quality of large transport aircraftA test program was undertaken to determine airline passenger reaction to vibration environments that might be encountered in a supersonic transport or other large commercial jet aircraft. The principal problem addressed was to determine accelerations of vertical and lateral vibration that people find objectionable. Further questions experimentally posed were: (1) what is the relationship between human reactions to vertical and lateral vibration, (2) to single- and combined-frequency vibration, and (3) to single- and combined-axis vibration? Interest was confined to reactions to vibration in the frequency range of 0.20 to 7.0 Hz, a range typical of the vibration environment of a large airplane. Results indicated an increasing sensitivity to vertical vibration as frequency was increased from 1.0 to 7.0 Hz. Subjects were found most sensitive to lateral vibration in the 1.0 to 3.0 Hz range. There was a nearly linear decrease in sensitivity as frequency of lateral vibration was increased from 3.0 to 7.0 Hz.
Document ID
19730001290
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Holloway, R. B.
(Boeing Co. Wichita, KS, United States)
Brumaghin, S. H.
(Boeing Co. Wichita, KS, United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1972
Publication Information
Publication: NASA. Langley Res. Center Symp. on Vehicle Ride Quality
Subject Category
Aircraft
Accession Number
73N10017
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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