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A “swallowtail” cavity for the supersonic combustor was proposed to serve as an efficient flame holder for scramjets by enhancing the mass exchange between the cavity and the main flow. A numerical study on the “swallowtail” cavity was conducted by solving the three-dimensional Reynolds-averaged Navier–Stokes equations implemented with a k–ε turbulence model in a multi-block mesh. Turbulence model...
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