A summary of the NASA/Rockwell Active Flexible Wing Program is presented. Major elements of the program are presented. Key program accomplishments included single- and multiple-mode flutter suppression, load alleviation and load control during rapid roll maneuvers, and multi-input/multi-output multiple-function active controls tests above the open-loop flutter boundary.
Summary of the Active Flexible Wing Program
1992
12 pages
Report
Keine Angabe
Englisch
Aircraft , Aerodynamics , Aeronautics , Active control , Aerodynamic loads , Aeroelastic research wings , Aircraft control , Dynamic structural analysis , Flexible wings , Roll , Vibration damping , Control systems design , Flutter , Flutter analysis , Nasa programs , Vibration tests , Wind tunnel models
Summary of an Active Flexible Wing program
AIAA | 1995
|Summary of an Active Flexible Wing Program
Online Contents | 1995
|A summary of the active flexible wing program
NTRS | 1992
|A summary of the Active Flexible Wing program
NTRS | 1992
|A summary of the Active Flexible Wing program
AIAA | 1992
|