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BACT Simulation User Guide (Version 7.0)This report documents the structure and operation of a simulation model of the Benchmark Active Control Technology (BACT) Wind-Tunnel Model. The BACT system was designed, built, and tested at NASA Langley Research Center as part of the Benchmark Models Program and was developed to perform wind-tunnel experiments to obtain benchmark quality data to validate computational fluid dynamics and computational aeroelasticity codes, to verify the accuracy of current aeroservoelasticity design and analysis tools, and to provide an active controls testbed for evaluating new and innovative control algorithms for flutter suppression and gust load alleviation. The BACT system has been especially valuable as a control system testbed.
Document ID
19990004130
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Waszak, Martin R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:206252
L-17678
NASA/TM-97-206252
Report Number: NAS 1.15:206252
Report Number: L-17678
Report Number: NASA/TM-97-206252
Funding Number(s)
PROJECT: RTOP 522-33-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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