Study on Unsymmetrical Supersonic Nozzle Flows.
Study on Unsymmetrical Supersonic Nozzle Flows.
The shape of scramjet-engine utilized for a space vehicle may be unsymmetrical in general. Supersonic flows generated in such asymmetric nozzle are very unstable due to pseudo-shock waves. To analyze the effects of the nozzle contour on the flow, three kinds of nozzle configuration were examined experimentally. The interaction of …