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achieved actuator aerodynamic Airbus Industrie aircraft airframe AMRAeS analysis angle application assessment aviation BAC One-Eleven blade British Aerospace camber CEng Chairman Coanda coefficient components composite composite materials configuration control system cost crack damage detection display drag dynamic effects eigenvalue engine equations factor failure fatigue fibre Figure finite element flapping flight flow Fluid Mechanics flying FRAeS frequency fuel function gust helicopter Illustrated improved increase input inspection integrity load London Mach number manoeuvre manufacturing materials matrix mechanical ment method MRAeS NASA ONERA TP operation paper performance pilot pitch Politecnico di Milano power spectral density President pressure problems programme RAeS ratio reduced rotor Royal Aeronautical Society Secretary shown in Fig simulation speed static strength stress structural surface techniques tion turbulence variable varicam vector velocity weight Weybridge wing