Once again on the supersonic flow separation near a corner
Once again on the supersonic flow separation near a corner
Laminar boundary-layer separation in the supersonic flow past a corner point on a rigid body contour, also termed the compression ramp, is considered based on the viscousāinviscid interaction concept. The ātriple-deck modelā is used to describe the interaction process. The governing equations of the interaction may be formally derived from ā¦