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Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5

Title:Effect of casing treatment on overall performance of axial-flow transonic fan stage with pressure ratio of 1.75 and tip solidity of 1.5
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Note:National Aeronautics and Space Administration ;, 1977
  
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Subject:Aerodynamics, Transonic
Subject:Aircraft gas-turbines
Subject:Axial flow compressors
Subject:Impellers
Subject:Turbomachines -- Blades
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