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Record Details

Record 16 of 3265
Helicopter crew/passenger vibration sensitivity -
Offline Availability: Go to Request Form
Author and Affiliation:
Gabel, R.(Boeing Co., Philadelphia, PA, United States)
Reed, D. A.(Boeing Co., Philadelphia, PA, United States)
Abstract: Helicopter crew and passenger vibration sensitivity are presented. Pilot subjective ratings are established for discrete frequencies and the impact of combinations of harmonic frequencies is examined. A passenger long term comfort level and a short term limit are defined for discrete frequencies and compared with pilot ratings. The results show reasonable agreement between pilot and passenger. Subjective comfort levels obtained for mixed frequency environments clearly demonstrate the need for a multi-frequency criterion.
Publication Date: Oct 01, 1972
Document ID:
19730001292
(Acquired Nov 22, 1995)
Accession Number: 73N10019
Subject Category: BIOSCIENCES
Document Type: Conference Paper
Publication Information: NASA. Langley Res. Center Symp. on Vehicle Ride Quality; p 143-153
Publisher Information: United States
Financial Sponsor: NASA; United States
Organization Source: Boeing Co.; Vertol Div.; Philadelphia, PA, United States
Description: 11p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: No Copyright
NASA Terms: HELICOPTERS; HUMAN FACTORS ENGINEERING; HUMAN REACTIONS; VIBRATION EFFECTS; VIBRATION PERCEPTION; ENVIRONMENTAL TESTS; PHYSIOLOGICAL EFFECTS; PSYCHOLOGICAL EFFECTS
Imprint And Other Notes: In NASA. Langley Res. Center Symp. on Vehicle Ride Quality p 143-153 (SEE N73-10012 01-02)
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