Aircraft Loading and Structural Layout (Aerospace Series by Denis Howe

By Denis Howe

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Experience enables this to be achieved without the necessity of specific reference to the loading requirement% However, the more detailed layout of the components of the airframe and, especially, the initial sizing of the individual members, can only be undertaken in conjunction with a detailed reference to the loading requirements. For the present purposes this phase of the total aircraft design process is taken to be the definition of the configuration of the primary structural members and their preliminary sizing; the description 'structural layout' is taken to cover both aspects of this procedure.

Form the starting point for the preliminary structural design. It must be pointed out that, since these requirements are based on past experience, it is also necessary to consider the introduction of special new requirements in those cases where the concept of the aircraft is in any way unconventional. The interpretation andapplication of the structural design requirements may be defined as loading actions analysis. A knowledge of the basic aerodynamic and inertial characteristics of the design is essential to enable the loading analysis to be undertaken and it is presumed that these data have been derived during the conceptual design and analysis phases.

There is also likely to be a variability in materials and construction due to the use of production methods such as welding. For these reasons the technique of probabilistic design was extensively developed by offshore structures and ship designers. More recently it has been realized that a guided weapon system consists of many components, Aircraft loading a n d structural layout most of which have to be designed on a statistical basis, and the airframe can he included in this. The concept has been applied to the design of military aircraft in the United Kingdom and it is accepted as one way of demonstrating compliance with structural design requirements.

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