Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp-Reference-Cited by-同舟云学术

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Experimental and numerical investigation of shock wave/boundary layer interactions induced by curved back-swept compression ramp

Published:2023-11 Issue: Volume:142 Page:108639
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chen Liang^ORCID,Zhang Yue,Xue Hong-chao^ORCID,Tan Hui-jun,Wang Zi-yun^ORCID,Yu Hang

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference36 articles.

1. How much compression should a scramjet inlet do?;Smart;AIAA J.,2012

2. Busemann inlet for hypersonic speeds;Mölder;J. Spacecr. Rockets,1966

3. Cross section controllable hypersonic inlet design using streamline-tracing and osculating axisymmetric concepts;You,2007

4. Streamline tracing: technique for designing hypersonic vehicles;Billig;J. Propuls. Power,2000

5. Design of modular shape-transition inlets for a conical hypersonic vehicle;Rowan;J. Propuls. Power,2013

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The Effects of Compression Direction on the Performance of a Two-Dimensional Inlet Mounted on the Aft Body;Applied Sciences;2024-06-20

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