Nonweiler, T.2012-09-112012-09-111953-10http://dspace.lib.cranfield.ac.uk/handle/1826/7564An expression is deduced for the wave drag of a fully tapered swept wing of arbitrary section in the convenient form of a double integral involving the variation of wing-surface slope. It is concluded, in the general case, that the drag may best be computed by numerical integration, the method for which will be the subject of a further report. Continues …enReport