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Lateral ride quality of the B-1 aircraft subjected to a reduction of lateral static stabilityA method to evaluate the lateral ride quality of a B-1 aircraft subjected to a reduction in lateral static stability is developed. Ride quality is then found for three different relaxed static stability configurations which are augmented by yaw rate feedback to restore specified handling qualities. These cases are compared to the ride quality of the unrelaxed aircraft with the same handling qualities.
Document ID
19760019100
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hinsdale, A. J. (Purdue Univ. West Lafayette, IN, United States)
Date Acquired
September 3, 2013
Publication Date
April 10, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-148206
Report Number: NASA-CR-148206
Meeting Information
Meeting: 1976 AIAA Midwest Student Conf.
Location: Milwaukee, WI
Country: United States
Start Date: April 8, 1976
End Date: April 10, 1976
Accession Number
76N26188
Funding Number(s)
CONTRACT_GRANT: NSG-4003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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