Abstract:
The improved performance of aircraft during the past decade has resulted
in the need for new design and production techniques. Particular examples are
integral construction and the use of sandwich panels. Although these processes
are costly, especially when applied to titanium and steel construction, their use
is likely to be necessary, at least to some extent. on many supersonic aircraft.
The supersonic airliner is no exception to this and the paper discusses the design
aspects of this type of aircraft which have a bearing on production problems. It
is concluded that more research aimed at reducing the cost of sophisticated forms
of construction is required.
