Three-dimensional reconstruction of incident shock/boundary layer interaction using background-oriented schlieren
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference12 articles.
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2. Pseudo-shock waves and their interactions in high-speed intakes;Gnani;Prog. Aero. Sci.,2016
3. Flow control of swept shock-wave/boundary-layer interaction using plasma actuators;Deshpande;J. Spacecraft Rockets,2018
4. Experimental investigation of an incident shock-induced interaction near an expansion corner;Sathianarayanan;J. Spacecraft Rockets,2017
5. Interactions between shock waves and turbulent boundary layers;Green;Prog. Aero. Sci.,1970
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