Experimental work on the aerodynamics of integrated slender wings for supersonic flight

This paper reviews an extensive programme of experimental work which was aimed at the production of integrated slender wings which had volume distributions and cross-section shapes compatible with the requirements of a supersonic transport aircraft. The wings were also to be cambered so that they were trimmed at the cruise condition about a centre of gravity position located at the aerodynamic centre position at the approach condition; furthermore the camber was to be chosen so that the drag was as low as possible. The main work was carried out about 20 years ago, but the involvement in specific design applications resulted in no overall account of the programme being published, although a number of reports on individual wings, or groups of wings, have appeared. This paper reviews the whole programme from the initial tests on very simple delta wings with diamond cross-sections to the final tests on realistic shapes which achieved almost all of the design requirements.