Control mechanism of micro vortex generator and secondary recirculation jet combination in the shock wave/boundary layer interaction
Author:
Funder
National Key Research and Development Program of China
National Natural Science Foundation of China
Natural Science Foundation of Hunan Province
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference55 articles.
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3. Effect of wave wall strut fuel injector on shock wave development and mixing enhancement of fuel and air for a scramjet combustor;Kummitha;Journal of Computational Design and Engineering,2021
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