Experimental and Numerical Investigations of Shock-Wave Boundary Layer Interactions in a Highly Loaded Transonic Compressor Cascade
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
https://link.springer.com/content/pdf/10.1007/s11630-023-1929-1.pdf
Reference37 articles.
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3. Ferri A., Experimental results with airfoils tested in the high-speed tunnel at Guidonia. 1940, NACA-TM-946.
4. Dolling D.S., Fifty years of shock-wave/boundary-layer interaction research: what next? AIAA Journal, 2001, 39(8): 1517–1531.
5. Schreiber H.A., Starken H., Experimental cascade analysis of a transonic compressor rotor blade section. Journal of Engineering for Gas Turbines and Power-Transactions of the Asme, 1984, 106(2): 288–294.
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1. Numerical study of shock wave boundary layer interaction flows using a novel turbulence model;Physics of Fluids;2024-05-01
2. Aerodynamic Optimization and Mechanism Investigation on Performance Improvements in a Transonic Compressor Cascade;Machines;2023-02-07
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