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Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Active Control Design ApplicationsThis report describes the formulation of a model of the dynamic behavior of the Benchmark Active Controls Technology (BACT) wind tunnel model for active control design and analysis applications. The model is formed by combining the equations of motion for the BACT wind tunnel model with actuator models and a model of wind tunnel turbulence. The primary focus of this report is the development of the equations of motion from first principles by using Lagrange's equations and the principle of virtual work. A numerical form of the model is generated by making use of parameters obtained from both experiment and analysis. Comparisons between experimental and analytical data obtained from the numerical model show excellent agreement and suggest that simple coefficient-based aerodynamics are sufficient to accurately characterize the aeroelastic response of the BACT wind tunnel model. The equations of motion developed herein have been used to aid in the design and analysis of a number of flutter suppression controllers that have been successfully implemented.
Document ID
19980203955
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Waszak, Martin R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1998
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.60:206270
NASA/TP-1998-206270
L-17625
Report Number: NAS 1.60:206270
Report Number: NASA/TP-1998-206270
Report Number: L-17625
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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