Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows-Reference-Cited by-同舟云学术

Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows

Published:2020-10 Issue: Volume:105 Page:105941
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ju Shengjun,Sun Zhenxu,Yang Guowei,Prapamonthon Prasert,Zhang Junyuan

Funder

Chinese Academy of Sciences

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

1. A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations;Huang;J. Zhejiang Univ. Sci. A,2015

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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