In the illustration, aeroelastic modeling and optimization design of wings, tails, and full aircrafts are presented, and both metal and composite materials are taken into account.

Also due to the features,the design and manufacture of the aeroelastic model are difficult although the kind of models are effective to investigate responses of the structures under strong wind actions,and thus has been seldom used in practical application.

Based on the mechanism and equation of wind vibration control,wind-induced vibration control for transmission tower model with suspended mass pendulums was performed by using a full aeroelastic model test.

It is very difficult to design and manufacture aeroelastic models of space structures.

The Role of Research on Servoaeroelasticity in Design of UAV;

A New Interface Mapping and Marching Method for Aeroelasticity;

A new interface mapping method for aeroelasticity;

Unsteady Aerodynamics and Aeroelastic Analysis Based on Volterra-Series;

High-fidelity analysis tool of both aerodynamics and structures were permitted to carry out aeroelastic analysis on these sample design scenarios.

The unsteady aerodynamics space-state model is constructed by means of feature system realization algorithm and applied to aeroelastic calculation.