Coupled investigation on drag reduction and thermal protection mechanism induced by a novel combinational spike and multi-jet strategy in hypersonic flows-Reference-Cited by-同舟云学术

Coupled investigation on drag reduction and thermal protection mechanism induced by a novel combinational spike and multi-jet strategy in hypersonic flows

Published:2019-03 Issue: Volume:131 Page:944-964
ISSN:0017-9310
Container-title:International Journal of Heat and Mass Transfer
language:en
Short-container-title:International Journal of Heat and Mass Transfer

Author:

Zhu Liang,Li Yingkun,Gong Lunkun,Chen Xiong,Xu Jinsheng

Funder

National Nature Science Foundation of China

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference64 articles.

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2. A review of design issues specific to hypersonic flight vehicles;Sziroczak;Prog. Aerosp. Sci.,2016

3. Aerodynamic heating in transitional hypersonic boundary layers: Role of second-mode instability;Zhu;Phys. Fluids,2018

4. Numerical investigation of sweep angle effect on the supersonic flows through corners;Kharati Koopaee;J. Aerospace Eng.,2017

5. Interactions between second mode and low-frequency waves in a hypersonic boundary layer;Chen;J. Fluid Mech.,2017

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