What is it about?
The effect of boundary layer transition on the shock dynamics of transonic fans of turbofans or jet engines at altitude conditions is investigated. An experiment using high speed Schlieren is used, as well as a numerical investigation with large eddy simulations (LES).
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This page is a summary of: Effect of Transition on Self-Sustained Shock Oscillations in Highly Loaded Transonic Rotors, AIAA Journal, June 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063378.
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