This report comprises two papers presented to the Sub-Committee on Aeroelasticity. One gives an exposition of the ground vibration testing of aircraft with active control systems. The other presents a method of performing and interpreting dynamic tests on non-linear systems, such as control surface actuators. (Author)
Non-Linear Aeroelastic Analyses and Testing
1981
44 pages
Report
Keine Angabe
Englisch
Avionics , Aircraft , Aeroelasticity , Structural analysis , Flight control systems , Eigenvalues , Nonlinear analysis , Dynamic loads , Transfer functions , Coupling(Interaction) , Mathematical models , Hydraulic servomechanisms , Hydraulic actuators , NATO , Harmonic analysis , Vibration , Control surfaces , Foreign technology , NATO furnished , Eigen modes