Flame stabilization enhancement by microjet-based virtual shock wave generators in a supersonic combustor-Reference-Cited by-同舟云学术

Flame stabilization enhancement by microjet-based virtual shock wave generators in a supersonic combustor

Published:2021-01-01 Issue:1 Volume:33 Page:016104
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

An Bin¹,Wang Zhenguo¹,Sun Mingbo¹^ORCID

Affiliation:

1. Science and Technology on Scramjet Laboratory, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

Funder

China Scholarship Council

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/10.1063/5.0031825

Reference26 articles.

1. Fundamental Studies of Cavity-Based Flameholder Concepts for Supersonic Combustors

2. Scramjet Fuels Autoignition Study

3. A shock tube study of ignition delay in the combustion of ethylene

4. Role of jet spacing and strut geometry on the formation of large scale structures and mixing characteristics

5. Mixing in nearwall regions downstream of a sonic jet in a supersonic crossflow at Mach 2.7

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