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Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor

Title:Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor
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Note:National Aeronautics and Space Administration, 1959
  
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Subject:Aerodynamics
Subject:Compressors -- Blades
Subject:Pressure
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