Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows
Author:
Funder
Chinese Academy of Sciences
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference50 articles.
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2. Drag reduction mechanism induced by a combinational opposing jet and spike concept in supersonic flows;Huang;Acta Astronaut.,2015
3. Parametric study on the heat transfer of a blunt body with counterflowing jets in hypersonic flows;Guo;Int. J. Heat Mass Transf.,2018
4. Aerodisk effects on drag reduction for hypersonic blunt body with an ellipsoid nose;Zhong;Aerosp. Sci. Technol.,2019
5. Experimental investigations of hypersonic flow over highly blunted cones with aerospikes;Menezes;AIAA J.,2003
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