Flame propagation involved in vortices of supersonic mixing layers laden with droplets: Effects of ambient pressure and spray equivalence ratio-Reference-Cited by-同舟云学术

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Flame propagation involved in vortices of supersonic mixing layers laden with droplets: Effects of ambient pressure and spray equivalence ratio

Published:2018-10 Issue:10 Volume:30 Page:106107
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Ren Zhaoxin¹,Wang Bing²,Zhao Dan³^ORCID,Zheng Longxi¹^ORCID

Affiliation:

1. School of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China

2. School of Aerospace Engineering, Tsinghua University, Beijing 1000084, China

3. Department of Mechanical Engineering, College of Engineering University of Canterbury, Private Bag 4800, Christchurch 8140, New Zealand

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/10.1063/1.5049840

Reference58 articles.

1. Shock Wave—Turbulence Interactions

2. Large-Eddy Simulation of Shock-Turbulence Interaction

3. Direct Numerical Simulation of a Reflected-Shock-Wave/Turbulent-Boundary-Layer Interaction

4. Direct Numerical Simulation Database for Impinging Shock Wave/Turbulent Boundary-Layer Interaction

5. Reynolds- and Mach-number effects in canonical shock–turbulence interaction

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