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Direct numerical simulation of supersonic internal flow in a model scramjet combustor under a non-reactive condition (2023)

First Author: Fang J

Attributed to: UK Turbulence Consortium funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1063/5.0137884

Publication URI: http://dx.doi.org/10.1063/5.0137884

Type: Journal Article/Review

Parent Publication: Physics of Fluids

Issue: 2