Drag and heat flux reduction mechanism induced by the combinational forward-facing cavity and pulsed counterflowing jet configuration in supersonic flows.

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Bibliographic Details
Title: Drag and heat flux reduction mechanism induced by the combinational forward-facing cavity and pulsed counterflowing jet configuration in supersonic flows.
Authors: Zhang, Rui-rui1 (AUTHOR), Dong, Min-zhou1,2 (AUTHOR) dongminzhou@nwpu.edu.cn, Huang, Wei1 (AUTHOR) gladrain2001@163.com, Li, Shi-bin3 (AUTHOR), Du, Zhao-bo1 (AUTHOR), Liao, Jun4 (AUTHOR)
Source: Acta Astronautica. Jul2019, Vol. 160, p62-75. 14p.
Database: Academic Search Ultimate
Description
ISSN:00945765
DOI:10.1016/j.actaastro.2019.04.026