Aerodynamic heating in transitional hypersonic boundary layers: Role of second-mode instability-Reference-Cited by-同舟云学术

Aerodynamic heating in transitional hypersonic boundary layers: Role of second-mode instability

Published:2018-01 Issue:1 Volume:30 Page:011701
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Zhu Yiding¹^ORCID,Chen Xi¹,Wu Jiezhi¹,Chen Shiyi¹^ORCID,Lee Cunbiao¹,Gad-el-Hak Mohamed²^ORCID

Affiliation:

1. State Key Laboratory for Turbulence and Complex Systems, Collaborative Innovation Center for Advanced Aero-Engine, Peking University, Beijing 100871, China

2. Department of Mechanical and Nuclear Engineering, Virginia Commonwealth University, Richmond, Virginia 23284, USA

Funder

National Natural Science Foundation of China

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5005529

Reference15 articles.

1. Transition and Stability of High-Speed Boundary Layers

2. Transition in hypersonic boundary layers

3. Transition in Hypersonic Boundary Layers: Role of Dilatational Waves

4. Breakdown mechanisms and heat transfer overshoot in hypersonic zero pressure gradient boundary layers

5. Direct numerical simulation of transition in a sharp cone boundary layer at Mach 6: fundamental breakdown

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