Calculated and measured pressure-distributions at subsonic speeds on a non-lifting wing, mounted on a body

Pressure measurements on a non-lifting 55 swept wing-body combination have been performed at subsonic speeds in the 2.00x1.60 m2 high speed windtunnel (HST) of the National Aerorpace Laboratory ITLR, Amsterdam. The model for there tests has been made available by the Royal Aircraft Establishment at Farnborough. The results of these measurements...