| タイトル | Modeling the Benchmark Active Control Technology Wind-Tunnel Model for Application to Flutter Suppression |
| 本文（外部サイト） | http://hdl.handle.net/2060/20040110943 |
| 著者（英） | Waszak, Martin R. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 1996-01-01 |
| 言語 | eng |
| 内容記述 | This paper describes the formulation of a model of the dynamic behavior of the Benchmark Active Controls Technology (BACT) wind-tunnel model for application to design and analysis of flutter suppression controllers. 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 paper is the development of the equations of motion from first principles using Lagrange's equations and the principle of virtual work. A numerical form of the model is generated using values for parameters obtained from both experiment and analysis. A unique aspect of the BACT wind-tunnel model is that it has upper- and lower-surface spoilers for active control. Comparisons with experimental frequency responses and other data 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 assist the design and analysis of a number of flutter suppression controllers that have been successfully implemented. |
| NASA分類 | Aircraft Design, Testing and Performance |
| レポートNO | AIAA Paper 96-3437 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
