Noise Transmission along Shock Waves.

[摘要] Shocks at the inlet of scramjet engines are subject to perturbations from their interaction with turbulent boundary layer. DNS results for this interaction indicate the presence of discrete vortices that interact with the shock at its foot. These studies reveal that the vortices cause oscillations of the shock. In this work we examine the propagation of disturbances along a stationary oblique shock following interaction with a two-dimensional vortex. We study the decay of disturbances along a normal shock as measured from Euler computations and compare these with the predictions of Geometrical Shock Dynamics(GSD) for long range propagation. We have incorporated two improvements into the GSD model to tackle the shock-vortex interaction problem. The wave structure of the disturbance resembles N waves, the decay of which follows a power law profile.An extension of the GSD model to predict shock surface propagation in 3-D flows is presented along with the numerical implementation.

[发布机构] University of Michigan

[效力级别] Aerospace Engineering

[关键词] Perturbations Along the Shocks Due to Vortex Interaction;Aerospace Engineering;Engineering;Aerospace Engineering