In a 1988 paper delivered at the Aerospace Technology Conference and
Exposition in Anaheim, CA, University of Kansas Professor Jan Roskam
addressed the factors and “severe and/or novel design requirements” driving
aeronautical engineers to evolve new design concepts. As background for comparison, Roskam defined a “conventional” configuration “as one with which
the designer and user community have some degree of familiarity and confidence,” adding as an example “the classical wing/fuselage/tail design used by
over 90 percent of all airplanes.” He pointed out that what engineers consider to
be unique “depends to some extent on their background,” adding that “[a]fter
being around a ‘unique’ configuration for some time, it ceases to be unique!”6
He used the Boeing B-47 Stratojet as an example.
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