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Active controls for transportsIt is shown that the integration of active controls into advanced commercial transport designs yields increased efficiency (by as much as 12%), reduced fuel consumption, and improved safety. These conclusions are based on a NASA development program considering various design configurations, wind tunnel tests (e.g., tests of static and dynamic control effects, aerodynamic loads, flutter tests, and active flutter suppression system tests), and extensive flight testing.
Document ID
19780034111
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Taylor, L. W., Jr.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Publication Information
Publication: Aviation Engineering and Maintenance
Volume: 1
Subject Category
Aircraft Stability And Control
Accession Number
78A18020
Distribution Limits
Public
Copyright
Other

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