In problem 1, the flow around a blunt body subjected to the supersonic flow is solved. Problem 2 presents the shock wave reflection on the wall involving complex interaction phenomena. For both ...

A research team from Japan has developed a unified model to scale the transitional pressure development in a one-dimensional ...

At the German Aerospace Center (DLR) in Göttingen, scientists are exploring the phenomena of compressible flow mechanics in Europe’s largest and ...