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Mixing and combustion enhancement in a Mach 12 shape-transitioning scramjet engine

By James Barth
Topics: Scramjet, Hypersonics, Hypervelocity, Airbreathing propulsion, Boundary layer combustion, Tailored fuel injection, 0901 Aerospace Engineering
Publisher: The University of Queensland, School of Mechanical and Mining Engineering
Year: 2014
OAI identifier: oai:espace.library.uq.edu.au:UQ:345504

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