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We show that the Tandem-Hole injector gave superior performance than the Single-Hole injector for same fuel flow rate in a Scramjet Combustor
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This page is a summary of: Penetration and Combustion Studies of Tandem Liquid Jets in Supersonic Crossflow, Journal of Propulsion and Power, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b38047.
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