The paper sets out to summarise the properties of the flow in a local supersonic, two-dimensional, steady potential flow region. Starting from the results of the theory of characteristics, the concept of wave strength is ...
This note presents curves of a number of parameters which frequently Occur in calculations of the performance of conical centrebody intakes at supersonic speeds and full mass flow. These parameters follow directly from the ...
An untapered, sweptback wing of aspect ratio 4, sweepback 25 degrees and section 12% thick (R.A.E. 104 with 1% camber, a = 0.6) was tested in the R.A.E. Hqh Speed Tunnel. The pressure distribution was measured at the ...