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NASA TN D-7881

Title:NASA TN D-7881
Alternate title:Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine. I, Design and performance of a solid blade configuration
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Note:National Aeronautics and Space Administration ;, 1975
  
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Subject:Axial flow
Subject:Gas-turbines
Subject:Turbines -- Cooling
Subject:Turbines -- Testing -- Performance
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