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Performance of a 48-module swirl-can turbojet combustor segment at high temperatures using ASTM-A1 fuel

Title:Performance of a 48-module swirl-can turbojet combustor segment at high temperatures using ASTM-A1 fuel
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Note:National Aeronautics and Space Administration ;, 1969
  
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Subject:Aircraft gas-turbines -- Combustion chambers -- Testing
Subject:Airplanes -- Turbojet engines -- Combustion -- Equipment and supplies -- Testing
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