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Shock Train Interaction in Curved Isolator by Sohel Mahmud is a document available to read on EtoBox.
This document summarizes research on the flow characteristics in a curved isolator with sidewall contraction for a hypersonic scramjet. As the backpressure downstream increases, the shock train in the isolator propagates upstream. This causes it to interact with the glancing shock wave and boundary layer vortices formed near the sidewall, creating a shock train/glancing shock/boundary layer interaction phenomenon. The shock train can be divided into two parts - a quasi-two-dimensional center part associated
- Author
- Sohel Mahmud
- Language
- EN