This is inevitably an iterative procedure which consists of alternative phases of synthesis and analysis. Many compromises are inevitable. Aerodynamic performance has to be matched access the operating speed range, blended with power plant characteristics, yield satisfactory control and stability and at the same time not unduly penalise structural considerations and the consequent mass penalties. The integration of advanced flying control systems with the aerodynamic and structural design is a unique and vital procedure. At the same time as the technical aspects of the design are under consideration it is essential to allow for manufacturing considerations. The whole design process must make use of the most advanced tools available in computer aided design and manufacturing. There are a number of excellent texts which cover many of the various facets of initial aircraft design. Some concentrate on one or two of the implied disciplines to the detriment of the others. Although some include consideration of the initial, synthesis, phase of the design the usual emphasis is on analytical methods. Certain of these texts are also restricted, implicitly or explicitly, to particular classes of aircraft.
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