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ResearcherID: G-5224-2017

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Education and qualifications (1)

National University of Defense Technology: Changsha, Hunan, CN

2010-09-01 to present | PHD (Science and Technology on Scramjet Laboratory)
Education
Source: Self-asserted source
Shibin Li

Works (6)

Drag and heat reduction mechanism of the porous opposing jet for variable blunt hypersonic vehicles

International Journal of Heat and Mass Transfer
2018-11 | Journal article
DOI: 10.1016/j.ijheatmasstransfer.2018.06.054
Contributors: Shibin Li; Wei Huang; Jing Lei; Zhenguo Wang
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Crossref

Variable Mach number design approach for a parallel waverider with a wide-speed range based on the osculating cone theory

Acta Astronautica
2018-06 | Journal article
DOI: 10.1016/j.actaastro.2018.04.008
Contributors: Zhen-tao Zhao; Wei Huang; Shi-Bin Li; Tian-Tian Zhang; Li Yan
Source: check_circle
Crossref

Design and investigation on variable Mach number waverider for a wide-speed range

Aerospace Science and Technology
2018-05 | Journal article
DOI: 10.1016/j.ast.2018.01.044
Contributors: Shibin Li; Zhenguo Wang; Wei Huang; Jing Lei; Shenren Xu
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Crossref

Numerical investigation of drag and heat flux reduction mechanism of the pulsed counterflowing jet on a blunt body in supersonic flows

Acta Astronautica
2018-05 | Journal article
DOI: 10.1016/j.actaastro.2018.02.040
Contributors: Rui-rui Zhang; Wei Huang; Li Yan; Lang-quan Li; Shi-bin Li; R. Moradi
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Crossref

A design approach of wide-speed-range vehicles based on the cone-derived theory

Aerospace Science and Technology
2017-12 | Journal article
DOI: 10.1016/j.ast.2017.09.010
Contributors: Tian-tian Zhang; Zhen-guo Wang; Wei Huang; Shi-bin Li
Source: check_circle
Crossref

Effect of the injector configuration for opposing jet on the drag and heat reduction

Aerospace Science and Technology
2016-04 | Journal article
DOI: 10.1016/j.ast.2016.01.014
Contributors: Shi-bin Li; Zhen-guo Wang; Wei Huang; Jun Liu
Source: check_circle
Crossref
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