Dynamic Mode Decomposition of Turbulent Combustion Process in DLR Scramjet Combustor-Reference-Cited by-同舟云学术

Dynamic Mode Decomposition of Turbulent Combustion Process in DLR Scramjet Combustor

Published:2017-09 Issue:5 Volume:30 Page:04017034
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Li Qing¹,Wang Zhenguo²

Affiliation:

1. Associate Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China (corresponding author).

2. Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000747

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4. Finite Rate Chemistry Large-Eddy Simulation of Self-Ignition in Supersonic Combustion Ramjet

5. LES of supersonic combustion in a scramjet engine model

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