Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles
Author:
Funder
Science Foundation of National University of Defense Technology
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
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2. Separation flow control by the gas injection contrary supersonic stream;Bazyma;AIAA J.,2006
3. Numerical investigation of a jet from a blunt body opposing a supersonic flow;Chen;J. Fluid Mech.,2011
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