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Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates

C. T. Norgren, J Howard Childs

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Key concepts: Combustor, Turbojet, Flow (mathematics), Environmental science, Aerospace engineering, Mechanics, Combustion, Engineering

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Effect of liner air-entry holes, fuel state, and combustor size on performance of an annular turbojet combustor at low pressures and high air-flow rates — Research Paper | ScholarLens