Interaction of Boundary Layer with Shock Wave in Unsymmetrical Supersonic Nozzle.
Interaction of Boundary Layer with Shock Wave in Unsymmetrical Supersonic Nozzle.
The study of unsymmetrical nozzle flow is important not only for basic research in gas dynamics but also for mechanical applications. In the present study, six kinds of unsymmetrical nozzles which had different divergence angles and wall lengths were used to analyze the effect of the nozzle configuration and Mach …