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Published online by Cambridge University Press: 28 July 2016
In general, the designer of an aeroplane has fixed for him the engine, the useful load, the strength factors, and the landing speed.
A weight estimate is prepared, in the process of which it would appear that the power loading, and the wing loading for the chosen section, fix themselves automatically; in practice, as we all know, the designer has a certain scope for variation of these, in addition to the choice of wing section.