Numerical study of supersonic turbulent boundary layer combustion with pressure gradient
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Published:2020-12
Issue:
Volume:107
Page:106246
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ISSN:1270-9638
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Container-title:Aerospace Science and Technology
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language:en
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Short-container-title:Aerospace Science and Technology
Author:
Zhang Pu,
Xu Jinglei,
Cui WeiORCID
Subject
Aerospace Engineering
Cited by
8 articles.
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