Development of a CAE tool for the design of flight control and hydraulic systems, D. Scholz; aspects of integration and weight saving in hydraulic systems, G. Barrow; systems development for a supersonic civil transport aircraft, M.S. Hall; a new approach to the determination of landing gear design loads, D.F. Shiells; active structural control of an advanced fighter aircraft, S.E. Burge, et al; concerning the optimization of standby redunancy in systems, L. Wolstenholme; new avionics systems - the A330/A340, J.P. Potocki de Montalk.
