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NASA/FRC wake turbulence flight test program: Ride quality aspectsTo determine how much the ride quality of the Shuttle Carrier (Boeing 747) Aircraft is affected at various spoiler settings, the PEMS II (Portable Environmental Measuring System) was used to measure onboard motion during a test flight October 15, 1975. The PEMS II measures acceleration in the vertical, transverse and longitudinal directions as well as angular rates of pitch, roll, and yaw. The data acquired by this instrument, combined with an airline passenger comfort model, gives an indication of how passengers would react to the motion induced by flying in a vortex alleviation configuration.
Document ID
19760003952
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Deptula, D. A.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
ESS-4032-104-75
NASA-CR-145700
MEMO-403225
Report Number: ESS-4032-104-75
Report Number: NASA-CR-145700
Report Number: MEMO-403225
Accession Number
76N11040
Funding Number(s)
CONTRACT_GRANT: NGR-47-005-181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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