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A summary of the active flexible wing programA summary of the NASA/Rockwell Active Flexible Wing Program is presented. Major elements of the program are presented. Key program accomplishments included single- and multiple-mode flutter suppression, load alleviation and load control during rapid roll maneuvers, and multi-input/multi-output multiple-function active controls tests above the open-loop flutter boundary.
Document ID
19920022020
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Perry, Boyd, III
(NASA Langley Research Center Hampton, VA, United States)
Cole, Stanley R.
(NASA Langley Research Center Hampton, VA, United States)
Miller, Gerald D.
(Rockwell International Corp. Los Angeles, CA., United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:107655
NASA-TM-107655
Report Number: NAS 1.15:107655
Report Number: NASA-TM-107655
Meeting Information
Meeting: AIAA Dynamic Specialists'' Conference
Location: Dallas, TX
Country: United States
Start Date: April 16, 1992
End Date: April 17, 1992
Accession Number
92N31264
Funding Number(s)
PROJECT: RTOP 505-63-50-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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