Determination of the inviscid, incompressible flow due to a thin, two-dimensional aerofoil moving with varying incidence and forward speed requires the solution of an integral equation. This report examines the case of ...
Methods recently developed for estimating distributions and intensities of sonic bangs are described. They are applied to several interesting flight manoeuvres and the results discussed in detail. The effect on sonic-bang ...
The supersonic flow over bodies for which the surface boundary condition may be satisfied on a circular cylinder is considered. The method is based on the linearised small-perturbation theory of supersonic flow. The ...