An engineering flight simulator used as a multi-purpose teaching and research tool
Sequential use of conceptual MDO and panel sizing methods for aircraft wing design
Smart internal vibration suppressor for a helicopter blade - a feasibility study
A smart internal vibration suppressor for a helicopter blade a feasibility study
Application of a Learning Control Algorithm to a Rotor Blade Tab
Unsteady aerodynamic loads on an aerofoil with deflecting tab
The use of smooth bending moment modes in helicopter rotor blade vibration studies