An outline of the Active Flexible Wing (AFW) project that was meant to serve as an introduction to an entire session of the Computational Control Workshop is presented. Following background information on the project is a description of the AFW wind tunnel model and results from the initial wind tunnel test of the AFW model under the current project. Emphasis is on major project accomplishments. The AFW project is an effort to demonstrate aeroelastic control through the application of digital controls technology. Active flutter suppression and active control of maneuver loads during high speed rolling maneuvers are examined.
An overview of the active flexible wing program
1991-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
AIAA | 1995
|Editorial: Active Flexible Wing Program
Online Contents | 1995
|Summary of an Active Flexible Wing Program
Online Contents | 1995
|Summary of an Active Flexible Wing program
AIAA | 1995
|Summary of the Active Flexible Wing Program
NTIS | 1992
|